Page 1

Maintenance Schedule for

B737-700

Hamburg International Revision No. 19 dated Jul 23/08 List of Effective Pages

please enter the number and date of this revision into „Record of Revision List“. Chapter / Section

Pages

Issue date

List of Eff. Pages Approval Sheet Record of Revision Record of Eff. Temp. Rev.

Page 1 of 1 Page 1 of 1 Page 1 - 2 Page 1 of 1

Jul 23/08 Jul 23/08 Jul 23/08 Jul 23/08

Table of Contents

Page 1 - 3

Jul 23/08

Introduction Highlights Item Revision Highlights

Page 1 - 2 Page 1 - 23

Jul 23/08 Jul 23/08

ATA Break-Down

Page 1 - 5

Jul 23/08

List of Effective Items

Page 1 - 7

Jul 23/08

Introduction

Page 1 - 28

Jul 23/08

Nat. and Internat. Special Requirements

Page 1 of 1

Jul 23/08

Aircraft Zones

Page 1 - 11

Jul 23/08

Items

see List of Eff. Items

Jul 23/08

Explanation Component Maintenance Section Page 1 - 6 Items Component Maintenance Section

see List of Eff. Items

Jul 23/08

Jul 23/08

Please note that Revision 19 dated Jul 23/08 of Maintenance Schedule for 737-6/-7/-8 A/C of Hamburg International is a complete issue.

Lufthansa Technik Form 30835-95 (HAM TB 3) Printed in the Federal Republic of Germany

Customer Engineering FRA WE Page 1 of 1


Maintenance Schedule for

B737-700

Hamburg International Revision No. 19 dated Jul 23/08 Record of Revision List Revision No.

Revision Date

Approval Date

Mar 24/99

Apr 26/99

1

Aug 02/99

Sep 02/99

2

Oct 27/99

Nov 22/99

3

Apr 13/00

Apr 26/00

4

Jan 11/01

Mar 09/01

5

Jun 12/01

Jul 31/01

6

Dec 11/01

Jan 11/02

7

Jun 26/02

Aug 28/02

8

Oct 17/02

Nov 28/02

9

Dec 18/02

Jan 14/03

10

Apr 29/03

May 22/03

11

Jun 13/03

Jun 24/03

12

Dec 02/03

Jan 16/04

13

Jun 03/04

Jul 15/04

14

Mar 18/05

Apr 26/05

15

Nov 30/05

Jan 16/06

16

Apr 25/06

May 10/06

17

Sep 05/06

Oct 10/06

18

Mar 22/07

Aug 06/07

19

Jul 23/08

First Issue

Lufthansa Technik Form 30839-95 (HAM TB 3) Printed in the Federal Republic of Germany

Revision No.

Revision Date

Approval Date

Customer Engineering FRA WE

Page 1 of 2


Maintenance Schedule for

B737-700

Hamburg International Revision No. 19 dated Jul 23/08 Record of Revision List Revision No. First Issue

Revision Date

Date incorp. / Sign

Revision No.

Revision Date

Date incorp. / Sign

Mar 24/99

1

Aug 02/99

2

Oct 27/99

3

Apr 13/00

4

Jan11/01

5

Jun 12/01

6

Dec 11/01

7

Jun 26/02

8

Oct 17/02

9

Dec 18/02

10

Apr 29/03

11

Jun 13/03

12

Dec 02/03

13

Jun 03/04

14

Mar 18/04

15

Nov 30/05

16

Apr 25/06

17

Sep 05/06

18

Mar 22/07

19

Jul 23/08

Lufthansa Technik Form 30839-95 (HAM TB 3) Printed in the Federal Republic of Germany

Customer Engineering FRA WE

Page 2 of 2


Maintenance Schedule for

B737-700

Hamburg International Revision No. 19 dated Jul 23/08 Record of Eff. Temporary Revision List Temp. Rev. No.

Date

Approval Date

Lufthansa Technik Form 30839-95 (HAM TB 3) Printed in the Federal Republic of Germany

Temp. Rev. No.

Date

Approval Date

Customer Engineering FRA WE

Page 1 of 1


MAINTENANCE SCHEDULE

HHI

737-6

TABLE OF CONTENTS HIGHLIGHTS ATA BREAK DOWN LIST OF EFFECTIVE ITEMS INTRODUCTION 1

GENERAL .................................................................................................................................................................................................................1 1.1 Validity .................................................................................................................................................................................................................1 1.2 Responsibilities.....................................................................................................................................................................................................2 1.3 Average Utilization...............................................................................................................................................................................................2 1.4 Operator’s Statement ............................................................................................................................................................................................3 1.5 Authority Approval...............................................................................................................................................................................................4 1.6 Explanation of Regulation ....................................................................................................................................................................................4 1.6.1 Flight Program ..............................................................................................................................................................................................4 1.6.2 Normal Standard Flight Time ........................................................................................................................................................................5 1.6.3 Maintenance Station ......................................................................................................................................................................................5 1.7 Revision Procedure...............................................................................................................................................................................................5 1.8 Reliability Monitoring Program ...........................................................................................................................................................................6 1.8.1 Aircraft Reliability Monitoring ......................................................................................................................................................................6 1.8.2 Engine Condition Monitoring ........................................................................................................................................................................7 1.8.3 Component Reliability Monitoring ................................................................................................................................................................7 1.9 Reference Documents...........................................................................................................................................................................................7

2

MAINTENANCE PROGRAM ................................................................................................................................................................................8 2.1 2.2

Line Maintenance .................................................................................................................................................................................................8 Base Maintenance.................................................................................................................................................................................................9

Date: 23-jul-2008

TABLE OF CONTENTS

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HHI

737-6

2.3 Time Controlled Maintenance ..............................................................................................................................................................................9 2.4 Zonal Inspection Program.....................................................................................................................................................................................9 2.4.1 Enhanced Zonal Analysis Procedure (EZAP)..............................................................................................................................................10 2.5 Structure Program...............................................................................................................................................................................................10 2.6 (Not used) ...........................................................................................................................................................................................................10 2.7 Corrosion Prevention and Control Program (CPCP)..........................................................................................................................................10 2.8 Identification of Type Certification and MRB Requirements ............................................................................................................................11 2.8.1 MSI, SSI, AWL and CMR .............................................................................................................................................................................11 2.9 Component Maintenance Program .....................................................................................................................................................................12 2.10 Inspection Techniques.....................................................................................................................................................................................12 2.11 Task Codes ......................................................................................................................................................................................................15 2.12 (Not used) ........................................................................................................................................................................................................17 2.13 Parking, Storage and Return to Service ..........................................................................................................................................................17 2.13.1 Parking .....................................................................................................................................................................................................17 2.13.2 Storage......................................................................................................................................................................................................17 2.13.3 Return to Service ......................................................................................................................................................................................18 2.13.4 Special Regulations for Parked or Stored Aircraft ..................................................................................................................................18 2.14 Authority Requirements ..................................................................................................................................................................................18 2.14.1 Approval of Maintenance Schedule by Authority .....................................................................................................................................18 2.14.2 Interval Escalation Procedure..................................................................................................................................................................19 2.14.3 Permitted Variations to Task Frequencies ...............................................................................................................................................19 2.15 (Not used) ........................................................................................................................................................................................................20 2.16 (Not used) ........................................................................................................................................................................................................20 2.17 (Not used) ........................................................................................................................................................................................................20 2.18 Maintenance Requirements for Specific Aircraft Operations .........................................................................................................................20 2.18.1 MNPS Maintenance Procedures ..............................................................................................................................................................20 2.18.2 RVSM (Reduced Vertical Separation Minimum) Capability ....................................................................................................................20 2.18.3 CAT II / CAT III Operation ......................................................................................................................................................................20 3

FORMAT LAYOUT DESCRIPTION AND DEFINITION OF TERMS..........................................................................................................21 3.1 3.2

Revision Column ................................................................................................................................................................................................21 ITEM Column.....................................................................................................................................................................................................21

Date: 23-Jul-2008

TABLE OF CONTENTS

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MAINTENANCE SCHEDULE

HHI 3.3 3.4 3.5 3.6 3.7 3.8 3.9 3.10 3.11 3.12 3.13 3.14 4

DESCRIPTION Column ....................................................................................................................................................................................22 ZONE Column....................................................................................................................................................................................................23 ACCESS Column ...............................................................................................................................................................................................23 STRUCTURE Column .......................................................................................................................................................................................23 REFERENCES Column .....................................................................................................................................................................................24 THRESHOLD/INTERVAL Column..................................................................................................................................................................25 TASK Column ....................................................................................................................................................................................................25 EFFECTIVITY Column..................................................................................................................................................................................25 BY Column......................................................................................................................................................................................................25 REP Column....................................................................................................................................................................................................26 LEV Column ...................................................................................................................................................................................................26 ITEM REVISION DATE Column ..................................................................................................................................................................26

WEIGHING .............................................................................................................................................................................................................27 4.1 4.2 4.3

5

737-6

Weighing Periods................................................................................................................................................................................................27 Weighing Procedure ...........................................................................................................................................................................................27 Weighing Results................................................................................................................................................................................................27

AIRCRAFT ..............................................................................................................................................................................................................28

NATIONAL AND INTERNATIONAL SPECIAL REQUIREMENTS AIRCRAFT ZONES ITEMS EXPLANATION COMPONENT MAINTENANCE SECTION (Page 1-6) ITEMS COMPONENT MAINTENANCE SECTION

Date: 23-Jul-2008

TABLE OF CONTENTS

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MAINTENANCE SCHEDULE

HHI

737-6

Introduction Highlights General: Note “Which ever comes first” has been deleted from Items as it is explained within Chapter 2.1.

Chapter 1.3

Average Utilization

Relation between utilization and Flight Length Sensitive Thresholds from MPD Section 9 added (Already introduced with TR 001/07)

Chapter 1.7Revision Procedure Revision Procedure revised (Already introduced with TR001/07)

Chapter 1.9Reference Documents Documents revised and added

Chapter 2.4.1 Enhanced Zonal Analysis Procedure (EZAP) Chapter added based on MPD/MRB

Chapter 2.10

Inspection Techniques

Fuel Airworthiness Limitation CDCCL description added.

Chapter 2.18

Maintenance Requirements for Specific Aircraft Operations

Chapter added

Chapter 2.18.1

MNPS Maintenance Procedures

Chapter added

Chapter 2.18.2

RVSM (Reduced Vertical Separation Minimum) Capability

Chapter added

Date: 23-Jul-2008

HIGHLIGHTS

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MAINTENANCE SCHEDULE

HHI

Chapter 2.18.3

737-6

CAT II / CAT III Operation

Chapter added

Chapter 3.7Reference column Examples revised

Chapter 5 Aircraft D-AKIA,AHID,AHIE and AHIF phased out.

Date: 23-Jul-2008

HIGHLIGHTS

Page 2 of 2


HHI

MAINTENANCE SCHEDULE

737-6

Item Revision Highlights ITEM

DATE

05111- 00000

23-jul-08

TYPING ERROR IN NOTE (I) CORRECTED.

05145- 00000

23-jul-08

REFERENCES REVISED.

05195- 00000

23-jul-08

ACCESS PANELS REVISED ACCORDING TO MRB REV SEP 2007.

23-jul-08

REFERENCES REVISED EDITORIALLY.

05210- 01000

23-jul-08

AMM REFERENCE ADDED.

05553- 01000

23-jul-08

REFERENCES REVISED.

05560- 00000

23-jul-08

REFERENCES REVISED.

05571- 02000

23-jul-08

REFERENCES REVISED.

05841- 01000

23-jul-08

INTERVAL REVISED FROM 4800 CYC/18 MTH TO 4800 CYC/24 MTH AS AGREED AT THE OCT 2006 ISC MEETING ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)

05900- 20290

23-jul-08

MPD JUN.08 OEM TASK 20-290-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.

05900- 20300

23-jul-08

MPD JUN.08 OEM TASK 20-300-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.

05900- 20310

23-jul-08

MPD JUN.08 OEM TASK 20-310-00:

Date: 23-jul-08

REVISION

HIGHLIGHTS

Page 1 of 23


HHI

MAINTENANCE SCHEDULE ITEM

DATE

737-6

REVISION ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.

05900- 20320

23-jul-08

MPD JUN.08 OEM TASK 20-320-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.

05900- 20330

23-jul-08

MPD JUN.08 OEM TASK 20-330-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.

05900- 20340

23-jul-08

MPD JUN.08 OEM TASK 20-340-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.

05900- 20350

23-jul-08

MPD JUN.08 OEM TASK 20-350-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.

05900- 20360

23-jul-08

MPD JUN.08 OEM TASK 20-360-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.

Date: 23-jul-08

HIGHLIGHTS

Page 2 of 23


HHI

MAINTENANCE SCHEDULE ITEM

DATE

REVISION

05900- 20370

23-jul-08

MPD JUN.08 OEM TASK 20-370-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.

05900- 20380

23-jul-08

MPD JUN.08 OEM TASK 20-380-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.

05900- 20390

23-jul-08

MPD JUN.08 OEM TASK 20-390-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.

05900- 20400

23-jul-08

MPD JUN.08 OEM TASK 20-400-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.

05900- 20410

23-jul-08

MPD JUN.08 OEM TASK 20-410-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.

05900- 20420

23-jul-08

MPD JUN.08 OEM TASK 20-420-00:

Date: 23-jul-08

HIGHLIGHTS

737-6

Page 3 of 23


HHI

MAINTENANCE SCHEDULE ITEM

DATE

737-6

REVISION ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.

05900- 20430

23-jul-08

MPD JUN.08 OEM TASK 20-430-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.

05900- 20440

23-jul-08

MPD JUN.08 OEM TASK 20-440-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.

05900- 20450

23-jul-08

MPD JUN.08 OEM TASK 20-450-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.

05900- 20460

23-jul-08

MPD JUN.08 OEM TASK 20-460-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.

05900- 20470

23-jul-08

MPD JUN.08 OEM TASK 20-470-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.

Date: 23-jul-08

HIGHLIGHTS

Page 4 of 23


HHI

MAINTENANCE SCHEDULE ITEM

DATE

REVISION

05900- 20480

23-jul-08

MPD JUN.08 OEM TASK 20-480-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.

05900- 20490

23-jul-08

MPD JUN.08 OEM TASK 20-490-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.

05900- 20500

23-jul-08

MPD JUN.08 OEM TASK 20-500-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.

05900- 20510

23-jul-08

MPD JUN.08 OEM TASK 20-510-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.

05900- 20520

23-jul-08

MPD JUN.08 OEM TASK 20-520-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.

05900- 20530

23-jul-08

MPD JUN.08 OEM TASK 20-530-00:

Date: 23-jul-08

HIGHLIGHTS

737-6

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HHI

MAINTENANCE SCHEDULE ITEM

DATE

737-6

REVISION ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.

05900- 20540

23-jul-08

MPD JUN.08 OEM TASK 20-540-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.

05900- 20550

23-jul-08

MPD JUN.08 OEM TASK 20-550-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.

05900- 20560

23-jul-08

MPD JUN.08 OEM TASK 20-560-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.

05900- 20570

23-jul-08

MPD JUN.08 OEM TASK 20-570-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.

05900- 20580

23-jul-08

MPD JUN.08 OEM TASK 20-580-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.

Date: 23-jul-08

HIGHLIGHTS

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HHI

MAINTENANCE SCHEDULE ITEM

DATE

REVISION

05900- 20590

23-jul-08

MPD JUN.08 OEM TASK 20-590-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.

05900- 20600

23-jul-08

MPD JUN.08 OEM TASK 20-600-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.

05900- 20610

23-jul-08

MPD JUN.08 OEM TASK 20-610-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.

05900- 20620

23-jul-08

MPD JUN.08 OEM TASK 20-620-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.

081000 01000

23-jul-08

REFERENCE REVISED.

233011 00000

23-jul-08

REVISED AMM REFERENCE.

250000 09001

23-jul-08

ITEM DELETED DUE TO NON-APPLICABILITY.

254008 00000

23-jul-08

EDITORIAL CORRECTION OF ITEM DESCRIPTION.

256401 71000

23-jul-08

AMTOSS REFERENCE 25-64-00-71 DELETED AND CORRECT AMM REFERENCES ADDED.

Date: 23-jul-08

HIGHLIGHTS

737-6

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HHI

MAINTENANCE SCHEDULE ITEM

DATE

REVISION

256601 40000

23-jul-08

ITEM DLELETED; COVERD BY CMS-ITEMS CM2566 000010 AND CM2566 00020.

270000 00000

23-jul-08

SB REFERENCE REVISED DUE TO RELEASE OF SB REVISION 1.

270000 12000

23-jul-08

MPD FEB.08 REVISED ACCESS PANEL TO ADD 334JB, 344JB AND DELETE 315A, 333BB, 333EB, 334AB, 334BB, 343BB, 343EB, 344AB, 344BB. ACCESS PANEL WAS REVISED TO REFLECT APPLICABLE ACCESS REQUIREMENT.

23-jul-08

REFERENCES REVISED.

270000 25000

23-jul-08

MPD JUN.08 REVISED ACCESS NOTE. ACCESS NOTE WAS REVISED FROM "FORWARD CARGO COMPARTMENT CEILING PANELS" TO "FORWARD CARGO COMPARTMENT CEILING PANELS OR FLOOR PANELS BETWEEN B.S.396 TO B.S. 540". REVISION TO ADD "FLOOR PANELS BETWEEN B.S.396 TO B.S. 540" WAS APPROVED BY OCTOBER 2006 ISC.

270000 32000

23-jul-08

MPD FEB.08 REVISED ACCESS PANEL TO ADD 211A, 211B. ACCESS PANEL WAS REVISED TO ADD ACCESS PANELS 211A AND 211B FOR THE INSPECTION OF CABLE WITHIN PILOTS CONTROL QUADRANT. REVISED TASK DESCRIPTION. TASK DESCRIPTION WAS REVISED TO CORRECT THE WING CENTER SECTION STATION FROM "BS 520 TO 727" TO "BS 520 TO 667.75" AND TO INCLUDE "CABLE WITHIN PILOTS CONTROL QUADRANT" WHICH WAS PROVIDED IN THE TASK CARD 27-230-00-02. ADDED ACCESS NOTE. ACCESS NOTE WAS ADDED TO REFLECT THE APPROPRIATE ACCESS REQUIREMENT.

23-jul-08

REFERENCES REVISED.

23-jul-08

MPD JUN.08 ADDED TASK. TASK WAS ADDED AFTER REVIEWING THE ORIGINAL MSG-3 ANALYSIS FOR ACCOUNTABILITY ALL TASKS. THE ADDITION OF THE TASK WAS APPROVED BY 2006 ISC.

270000 35000

Date: 23-jul-08

HIGHLIGHTS

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DATE

REVISION

272100 03000

23-jul-08

MPD OCT.07 REVISED ZONE TO ADD 117, 211, 212 AND DELETE 134. ZONE WAS REVISED TO ADD THE REQUIRED ZONE 117,211 AND 212 AREA WHERE THE TASK PROCEDURE IS PERFORMED. AFTER REVIEWING THE TASK PROCEDURE, ZONE 134 WERE DETERMINED AS BEING NOT REQUIRED FOR THE TASK. REVISED ACCESS PANEL TO ADD 117A. ACCESS PANEL 117A WAS ADDED AS THE AMM TASK PROCEDURE REQUIRES ACCESSING INTO EE COMPARTMENT.

23-jul-08

ZONE 133 DELETED ACCORDING TO MRB REV SEP 2007.

273101 75000

23-jul-08

SB 737-55A1082 DELETED FROM EFFECTIVITY NOTE AS THIS SB IS NOT RELATED TO THIS MS ITEM.

273134 21500

23-jul-08

MPD JUN.08 REVISED ACCESS PANEL TO ADD 334PT, 344PT. ACCESS WAS REVISED TO REFLECT CORRECT ACCESS REQUIREMENT FOR THIS TASK.

23-jul-08

SB 737-55A1082 DELETED FROM EFFECTIVITY NOTE AS THIS SB IS NOT RELATED TO THIS MS ITEM.

274181 01000

23-jul-08

SB 737-27A1277 R1 ADDED AS A REFERENCE. THIS SB CONTAINS A REQUIREMENT FOR OVERHAUL OF THE HORIZONTAL STABILIZER TRIM ACTUATOR.

274181 21000

23-jul-08

INTERVAL REVISED TO HAVE THE SAME INTERVAL LIKE THE LUBRICATION TASK MS 270000 00000 AS RECOMMENDED BY BOEING IN SB. SB REFERENCE REVISED DUE TO RELEASE OF SB REVISION 1.

275106 21000

23-jul-08

EDITORIAL REVISION OF REFERENCES.

23-jul-08

MPD OCT.07 OEM TASK 27-166-00: REVISED ZONE TO DELETE 112, 117, 118. ZONE WAS REVISED BY DELETING 112,117 AND 118 BECAUSE THE ACTUAL WORKING ZONE IS INSIDE THE FLIGHT

Date: 23-jul-08

HIGHLIGHTS

737-6

Page 9 of 23


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DATE

737-6

REVISION DECK WHOSE ZONE IS DEFINED BY ZONES 211 AND 212. REVISED ACCESS PANEL TO ADD 211A, 211B. ACCESS PANEL WAS REVISED TO ADD 211A AND 211B WHICH ARE ACCESS TO THE INSIDE OF CONTROL STAND. DELETED ACCESS NOTE. "EXTENDED FLAPS" WAS DELETED FROM ACCESS NOTE BECAUSE EXTENSION OF FLAP IS NOT NECESSARY TO PERFORM THE DETAIL INSPECTION OF FLAP LEVER SENSOR WHICH IS LOCATED IN THE CONTROL STAND IN THE FLIGHT DECK.

276100 21000

23-jul-08

MPD JUN.08 ADDED TASK. TASK WAS ADDED AFTER REVIEWING THE ORIGINAL MSG-3 ANALYSIS FOR ACCOUNTABILITY OF ALL TASKS. THE ADDITION OF THE TASK WAS APPROVED BY 2006 ISC.

276200 21000

23-jul-08

REFERENCES EDITORIALLY REVISED.

280000 06000

23-jul-08

ACCESS PANELS UPDATED ACCORDING TO MPD. (ISSUED WITH TR001/07)

23-jul-08

FAILURE EFFECT CATEGORY "9" ADDED AND DESCRIPTION REVISED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)

280000 76000

23-jul-08

FAILURE EFFECT CATEGORY "9" ADDED AND DESCRIPTION REVISED, INTERVAL CHANGED FROM 5 YRS TO 6 YRS ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)

281100 01000

23-jul-08

NEW CMR MAR 08 REVISION, ITEM UPDATED.

281331 20000

23-jul-08

NEW TASK ADDED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)

281341 21000

23-jul-08

NEW TASK ADDED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)

282111 20000

23-jul-08

NEW TASK ADDED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)

Date: 23-jul-08

HIGHLIGHTS

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DATE

282151 20000

23-jul-08

NEW TASK ADDED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)

282200 20000

23-jul-08

MPD OCT.07 REVISED AIRPLANE NOTE. AIRPLANE NOTE WAS REVISED BY ADDING THE WORD "TASK" TO CLARIFY THE INTENT OF THE TASK.

282200 21000

23-jul-08

MPD OCT.07 REVISED AIRPLANE NOTE. AIRPLANE NOTE WAS REVISED BY ADDING THE WORD "TASK" TO CLARIFY THE INTENT OF THE TASK.

282211 20000

23-jul-08

NEW TASK ADDED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)

282211 72000

23-jul-08

NEW ITEM ACCORDING ALI 28-AWL-24.

282502 20000

23-jul-08

NEW TASK ADDED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)

284100 01000

23-jul-08

DESCRIPTION REVISED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)

284100 28000

23-jul-08

NEW TASK ADDED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)

284100 29000

23-jul-08

NEW TASK ADDED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)

23-jul-08

TASK UPDATED ACCORDING TO 28-AWL-03.

291104 20000

23-jul-08

NEW TASK ADDED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)

292100 70000

23-jul-08

INTERVAL TRANSFERRED FROM NOTE (I) TO INTERVAL COLUMN.

320000 31000

23-jul-08

DESCRIPTION REVISED.

320000 63000

23-jul-08

MPD JUN.08

Date: 23-jul-08

737-6

REVISION

HIGHLIGHTS

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DATE

737-6

REVISION REVISED ACCESS NOTE. ACCESS NOT WAS REVISED FROM "FORWARD CARGO COMPARTMENT CEILING PANELS" TO "FORWARD CARGO COMPARTMENT CEILING PANELS OR FLOOR PANELS BETWEEN B.S.396 TO B.S. 540". REVISION TO ADD "FLOOR PANELS BETWEEN B.S.396 TO B.S. 540" WAS APPROVED BY OCTOBER 2006 ISC.

320000 64000

23-jul-08

MPD JUN.08 REVISED ACCESS NOTE. ACCESS NOT WAS REVISED FROM "FORWARD CARGO COMPARTMENT CEILING PANELS" TO "FORWARD CARGO COMPARTMENT CEILING PANELS OR FLOOR PANELS BETWEEN B.S.396 TO B.S. 540". REVISION TO ADD "FLOOR PANELS BETWEEN B.S.396 TO B.S. 540" WAS APPROVED BY OCTOBER 2006 ISC.

320000 65000

23-jul-08

MPD JUN.08 REVISED ACCESS NOTE. ACCESS NOT WAS REVISED FROM "FORWARD CARGO COMPARTMENT CEILING PANELS" TO "FORWARD CARGO COMPARTMENT CEILING PANELS OR FLOOR PANELS BETWEEN B.S.396 TO B.S. 540". REVISION TO ADD "FLOOR PANELS BETWEEN B.S.396 TO B.S. 540" WAS APPROVED BY OCTOBER 2006 ISC.

320000 66000

23-jul-08

MPD JUN.08 REVISED ACCESS NOTE. ACCESS NOT WAS REVISED FROM "FORWARD CARGO COMPARTMENT CEILING PANELS" TO "FORWARD CARGO COMPARTMENT CEILING PANELS OR FLOOR PANELS BETWEEN B.S.396 TO B.S. 540". REVISION TO ADD "FLOOR PANELS BETWEEN B.S.396 TO B.S. 540" WAS APPROVED BY OCTOBER 2006 ISC.

320000 67000

23-jul-08

MPD JUN.08 REVISED ACCESS NOTE. ACCESS NOT WAS REVISED FROM "FORWARD CARGO COMPARTMENT CEILING PANELS" TO "FORWARD CARGO COMPARTMENT CEILING PANELS OR FLOOR PANELS BETWEEN B.S.396 TO

Date: 23-jul-08

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DATE

737-6

REVISION B.S. 540". REVISION TO ADD "FLOOR PANELS BETWEEN B.S.396 TO B.S. 540" WAS APPROVED BY OCTOBER 2006 ISC.

320000 68000

23-jul-08

MPD FEB.08 REVISED TASK PROCEDURE. TASK PROCEDURE WAS REVISED TO ADD AMM TASKS 32-31-22-211-801, 20-20-31-200-801, 20-20-31-200-802 AND 20-20-31-200-805 TO INSPECT LANDING GEAR CONTROL LEVER CABLE.

322171 20000

23-jul-08

MPD FEB.08 ADDED TASK. TASK WAS ADDED AFTER REVIEWING THE MSG-3 ANALYSIS TO ADDRESS SERVICE RELATED ISSUE ON NOSE LANDING GEAR AXLE. TASK ADDITION WAS APPROVED BY THE ISC CHAIR AND FAA MRB CHAIR.

324500 70000

23-jul-08

MPD JUN.08 REVISED FROM INSPECTION - DETAILED TO VISUAL CHECK. TASK WAS REVISED FROM "E3" TO "E1" AFTER REVIEWING THE ORIGINAL MSG-3 ANALYSIS TASK DESCRIPTION. THE ORIGINAL MSG-3 ANALYSIS IDENTIFIED THE TASK AS A VISUAL CHECK. REVISED TASK DESCRIPTION. TASK DESCRIPTION WAS REVISED FROM DETAILED INSPECTION TO VISUALLY CHECK AFTER REVIEWING THE ORIGINAL MSG-3 ANALYSIS TASK DESCRIPTION. THE ORIGINAL MSG-3 ANALYSIS IDENTIFIED THE TASK AS A VISUAL CHECK.

345300 73000

23-jul-08

AMM REFERENCE CORRECTED.

346002 00001

23-jul-08

AMM REFERENCE CORRECTED.

491611 10000

23-jul-08

AMM REFERENCES UPDATED.

491611 11000

23-jul-08

AMM REFERENCE CORRECTED.

493011 40000

23-jul-08

INTERVAL IN NOTE (I) CORRECTED.

494151 20000

23-jul-08

ZONE ADDED.

496100 90000

23-jul-08

REFERENCE "SERVICE EXPERIENCE" ADDED.

Date: 23-jul-08

HIGHLIGHTS

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DATE

498111 20100

23-jul-08

AMM REFERENCE CORRECTED.

499111 00000

23-jul-08

AMM REFERENCE CORRECTED.

524800 02000

23-jul-08

ACCESS PANEL CORRECTED.

526000 00000

23-jul-08

NEW ITEM ADDED ON CUSTOMER REQUEST.

526000 01000

23-jul-08

NEW ITEM ADDED ON CUSTOMER REQUEST.

526050 21000

23-jul-08

NEW ITEM ADDED ON CUSTOMER REQUEST.

527000 05000

23-jul-08

MPD FEB.08 REVISED TASK DESCRIPTION. TASK DESCRIPTION WAS REVISED FROM "THE THREE POSITION ROTARY SWITCH IN THE P5 PANEL" TO "THE THREE POSITION ROTARY SWITCH IN THE P8 PANEL" TO INDICATE THE APPROPRIATE LOCATION OF THE THREE POSITION ROTARY SWITCH.

527000 07000

23-jul-08

AMM REFERENCE ADDED.

527001 00000

23-jul-08

DELETED INTERVAL 16000 CYC DUE TO NON-APPLICABILITY AND ADJUSTED DESCRIPTION NOTE.

527001 02000

23-jul-08

DELETED INTERVAL 16000 CYC DUE TO NON-APPLICABILITY AND ADJUSTED DESCRIPTION NOTE.

23-jul-08

MPD FEB.08 REVISED TASK PROCEDURE. REVISED TASK PROCEDURE BY ADDING AIRCRAFT MAINTENANCE MANUAL (AMM) PROCEDURE 51-05-01-210-803 (CORROSION PREVENTION CONTROL PROGRAM (CPCP) BASIC STEPS PROCEDURE), TO REFLECT CORRECT CPCP REQUIREMENTS FOR THIS TASK.

23-jul-08

DELETED INTERVAL 16000 CYC DUE TO NON-APPLICABILITY AND ADJUSTED DESCRIPTION NOTE.

23-jul-08

MPD FEB.08

527001 04000

Date: 23-jul-08

737-6

REVISION

HIGHLIGHTS

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DATE

737-6

REVISION REVISED TASK PROCEDURE. REVISED TASK PROCEDURE BY ADDING AIRCRAFT MAINTENANCE MANUAL (AMM) PROCEDURE 51-05-01-210-803 (CORROSION PREVENTION CONTROL PROGRAM (CPCP) BASIC STEPS PROCEDURE), TO REFLECT CORRECT CPCP REQUIREMENTS FOR THIS TASK.

530900 01000

23-jul-08

ACCESS NOTE REVISED ACCORDING TO MRB REV SEP 2007.

530900 05000

23-jul-08

DESCRIPTION REVISED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)

530900 08000

23-jul-08

ACCESS NOTE REVISED ACCORDING TO MRB REV SEP 2007.

530900 10000

23-jul-08

ACCESS NOTE REVISED ACCORDING TO MRB REV SEP 2007.

530900 11000

23-jul-08

ACCESS NOTE REVISED ACCORDING TO MRB REV SEP 2007.

530900 13000

23-jul-08

ACCESS NOTE REVISED ACCORDING TO MRB REV SEP 2007.

531500 01000

23-jul-08

AMM-REFERENCES ADDED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)

531500 02000

23-jul-08

AMM-REFERENCES ADDED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)

531500 04000

23-jul-08

MPD OCT.07 AMM REFERENCE ADDED.

544000 00000

23-jul-08

INTERVAL REVISED FROM 9000 CYC/30 MTH TO 9000 CYC/36 MTH AS AGREED AT THE OCT 2006 ISC MEETING ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)

544000 06000

23-jul-08

ITEM SPLITTED TO LEFT SIDE AND RIGHT SIDE SEPERATELY. RIGHT SIDE IS COVERED BY NEW MS-ITEM 544000 06100 (MPD 54-020-02).

544000 06100

23-jul-08

SPLITTED MS ITEM 544000 06000 IN TWO SEPARATE ITEMS (LEFT STRUT AND RIGHT STRUT).

Date: 23-jul-08

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DATE

737-6

REVISION THIS NEW ITEM COVERS THE RIGHT ENGINE STRUT. THE EXISTING ITEM COVERS THE LEFT STRUT. REASON: TASK TO BE PERFORMED AT ENGINE CHANGE, WHICH TYPICALLY OCCURS ONLY ON ONE SIDE AT THE SAME TIME.

552000 03000

23-jul-08

DELETED NOTE (E) DUE TO NON-APPLICABILITY.

553000 00000

23-jul-08

REFERENCES EDITORIALLY REVISED.

553000 02000

23-jul-08

REFERENCES EDITORIALLY REVISED.

561100 02000

23-jul-08

DESCRIPTION REVISED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)

561100 03000

23-jul-08

NEW ITEM ADDED DUE TO AD REQUIREMENT OF INSPECTIONS ACCORDING TO SB 737-56A1022.

571000 03000

23-jul-08

DESCRIPTION REVISED ACCORDING TO MPD.

571400 02000

23-jul-08

ACCESS PANELS REVISED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)

571400 04000

23-jul-08

ENTERED CALCULATED THRESHOLD/INTERVAL ACC. MPD SECTION 9 FLS AND DTR 57-20-03. (ISSUED WITH TR001/07)

23-jul-08

NOTE (E) DELETED AND NOTE (I) REVISED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)

23-jul-08

ENTERED CALCULATED THRESHOLD/INTERVAL ACC. MPD SECTION 9 FLS AND DTR 57-20-03. (ISSUED WITH TR001/07)

23-jul-08

NOTE (E) DELETED AND NOTE (I) REVISED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)

23-jul-08

ENTERED CALCULATED THRESHOLD/INTERVAL ACC. MPD SECTION 9 FLS AND DTR 57-20-03. (ISSUED WITH TR001/07)

571400 05000

571400 05500

Date: 23-jul-08

HIGHLIGHTS

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DATE

REVISION

23-jul-08

NOTE (E) DELETED AND NOTE (I) REVISED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)

23-jul-08

ENTERED CALCULATED THRESHOLD/INTERVAL ACC. MPD SECTION 9 FLS AND DTR 57-20-09. (ISSUED WITH TR001/07)

23-jul-08

NOTE (E) DELETED AND NOTE (I) REVISED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)

572200 00000

23-jul-08

MPD OCT.07 OEM TASK 57-270-01: REVISED ACCESS PANEL TO ADD 572CB, 572CT. ACCESS WAS REVISED TO REFLECT CORRECT ACCESS REQUIREMENTS FOR THIS TASK BY ADDING 572CB AND 572CT. OEM TASK 57-270-02: REVISED ACCESS PANEL TO ADD 651GB AND DELETE 653AT. ACCESS WAS REVISED TO REFLECT CORRECT ACCESS REQUIREMENTS FOR THIS TASK BY ADDING 651GB AND DELETING 653AT.

573100 00000

23-jul-08

ACCESS PANELS REVISED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)

23-jul-08

EDITORIAL CORRECTION OF ITEM DESCRIPTION AND REFERENCES.

573200 01000

23-jul-08

INTERVAL REVISED FROM 9000 CYC/30 MTH TO 9000 CYC/36 MTH AS AGREED AT THE OCT 2006 ISC MEETING ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)

573500 00000

23-jul-08

INTERVAL REVISED FROM 9000 CYC/30 MTH TO 9000 CYC/36 MTH AS AGREED AT THE OCT 2006 ISC MEETING ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)

711102 20000

23-jul-08

AMM REFERENCE ADDED.

717100 20000

23-jul-08

AMM REFERENCE ADDED.

571400 07000

Date: 23-jul-08

737-6

HIGHLIGHTS

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DATE

720000 20000

23-jul-08

AMM REFERENCE ADDED.

720000 20200

23-jul-08

AMM REFERENCE ADDED.

720000 20300

23-jul-08

AMM REFERENCE ADDED.

720000 20400

23-jul-08

AMM REFERENCES CORRECTED.

720011 01200

23-jul-08

AMM REFERENCE ADDED.

720021 00200

23-jul-08

AMM REFERENCE ADDED.

722000 21000

23-jul-08

AMM REFERENCE ADDED.

722304 20000

23-jul-08

AMM REFERENCE ADDED.

722304 21000

23-jul-08

AMM REFERENCE ADDED.

725000 20000

23-jul-08

AMM REFERENCE ADDED.

731102 00000

23-jul-08

AMM REFERENCES ADDED.

732100 74000

23-jul-08

AMM REFERENCE ADDED.

742101 20000

23-jul-08

AMM REFERENCE ADDED.

742102 20000

23-jul-08

AMM REFERENCE ADDED.

781100 21000

23-jul-08

AMM REFERENCE ADDED.

783100 70000

23-jul-08

AMM REFERENCE ADDED.

783100 71000

23-jul-08

AMM REFERENCE ADDED.

783106 20000

23-jul-08

AMM REFERENCE ADDED.

783107 90000

23-jul-08

AMM REFERENCE ADDED.

783112 20000

23-jul-08

AMM REFERENCE ADDED.

783112 21000

23-jul-08

AMM REFERENCE ADDED.

783123 20000

23-jul-08

AMM REFERENCE ADDED.

Date: 23-jul-08

737-6

REVISION

HIGHLIGHTS

Page 18 of 23


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MAINTENANCE SCHEDULE ITEM

DATE

790000 20000

23-jul-08

AMM REFERENCE ADDED.

790000 20500

23-jul-08

AMM REFERENCE CORRECTED.

792103 00000

23-jul-08

AMM REFERENCES ADDED.

792106 00000

23-jul-08

AMM REFERENCES ADDED.

801101 20000

23-jul-08

AMM REFERENCE ADDED.

CM2132 00000

23-jul-08

MPD REFERENCES ADDED.

CM2324 00000

23-jul-08

DESCRIPTION AND TASK CODE REVISED AND NOTE ADDED TO COVER SHOP REQUIREMENTS.

CM2371 00010

23-jul-08

NOTE (M) ADDED.

CM2560 00020

23-jul-08

INTERVAL CORRECTED AND NOTE REVISED.

CM2560 00021

23-jul-08

INTERVAL CORRECTED AND NOTE REVISED.

CM2560 00030

23-jul-08

INTERVAL CORRECTED AND NOTE REVISED.

23-jul-08

MPD REFERENCE ADDED.

23-jul-08

PARTNUMBER FOR CHILD LIFE VEST CORRECTED.

CM2560 00031

23-jul-08

INTERVAL CORRECTED AND NOTE REVISED.

CM2566 00010

23-jul-08

REFERENCES ADDED.

CM2740 00020

23-jul-08

SB ADDED AS A REFERENCE. IN SB THERE IS A REQUIREMENT FOR OVERHAUL OF THE HORIZONTAL STABILIZER TRIM ACTUATOR.

CM2900 00020

23-jul-08

MPD JUN.08 OEM TASK REFERENCE 29-290-00 ADDED.

CM2999 00030

23-jul-08

MPD REFERENCE ADDED.

CM3211 00010

23-jul-08

MPD JUN.08 OEM TASK 32-040-01:32-040-02

Date: 23-jul-08

737-6

REVISION

HIGHLIGHTS

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DATE

737-6

REVISION REVISED INTERVAL. TASK INTERVAL WAS REVISED FROM 18000FC TO 21000FC. THE ESCALATION WAS CONCURRED BY BOEING ENGINEERING AFTER REVIEWING LANDING GEAR DIMENSIONAL DATA COLLECTED DURING LANDING GEAR OVERHAUL. THE INTERVAL ESCALATION WAS ALSO APPROVED BY MRB /CHAIRMAN AND ISC CHAIRPERSON.

CM3211 00020

23-jul-08

MPD JUN.08 OEM TASK 32-040-01: 32-040-02 REVISED INTERVAL. TASK INTERVAL WAS REVISED FROM 18000FC TO 21000FC. THE ESCALATION WAS CONCURRED BY BOEING ENGINEERING AFTER REVIEWING LANDING GEAR DIMENSIONAL DATA COLLECTED DURING LANDING GEAR OVERHAUL. THE INTERVAL ESCALATION WAS ALSO APPROVED BY MRB /CHAIRMAN AND ISC CHAIRPERSON.

CM3211 00030

23-jul-08

MPD JUN.08 OEM TASK 32-040-01: 32-040-02 REVISED INTERVAL. TASK INTERVAL WAS REVISED FROM 18000FC TO 21000FC. THE ESCALATION WAS CONCURRED BY BOEING ENGINEERING AFTER REVIEWING LANDING GEAR DIMENSIONAL DATA COLLECTED DURING LANDING GEAR OVERHAUL. THE INTERVAL ESCALATION WAS ALSO APPROVED BY MRB /CHAIRMAN AND ISC CHAIRPERSON.

CM3211 00040

23-jul-08

MPD JUN.08 OEM TASK 32-040-01: 32-040-02 REVISED INTERVAL. TASK INTERVAL WAS REVISED FROM 18000FC TO 21000FC. THE ESCALATION WAS CONCURRED BY BOEING ENGINEERING AFTER REVIEWING LANDING GEAR DIMENSIONAL DATA COLLECTED DURING LANDING GEAR OVERHAUL. THE INTERVAL ESCALATION WAS ALSO APPROVED BY MRB /CHAIRMAN AND ISC CHAIRPERSON.

CM3211 00050

23-jul-08

MPD JUN.08 OEM TASK 32-040-01: 32-040-02

Date: 23-jul-08

HIGHLIGHTS

Page 20 of 23


HHI

MAINTENANCE SCHEDULE ITEM

DATE

737-6

REVISION REVISED INTERVAL. TASK INTERVAL WAS REVISED FROM 18000FC TO 21000FC. THE ESCALATION WAS CONCURRED BY BOEING ENGINEERING AFTER REVIEWING LANDING GEAR DIMENSIONAL DATA COLLECTED DURING LANDING GEAR OVERHAUL. THE INTERVAL ESCALATION WAS ALSO APPROVED BY MRB /CHAIRMAN AND ISC CHAIRPERSON.

CM3211 00060

23-jul-08

MPD JUN.08 OEM TASK 32-040-01: 32-040-02 REVISED INTERVAL. TASK INTERVAL WAS REVISED FROM 18000FC TO 21000FC. THE ESCALATION WAS CONCURRED BY BOEING ENGINEERING AFTER REVIEWING LANDING GEAR DIMENSIONAL DATA COLLECTED DURING LANDING GEAR OVERHAUL. THE INTERVAL ESCALATION WAS ALSO APPROVED BY MRB /CHAIRMAN AND ISC CHAIRPERSON.

CM3211 00070

23-jul-08

MPD JUN.08 OEM TASK 32-040-01: 32-040-02 REVISED INTERVAL. TASK INTERVAL WAS REVISED FROM 18000FC TO 21000FC. THE ESCALATION WAS CONCURRED BY BOEING ENGINEERING AFTER REVIEWING LANDING GEAR DIMENSIONAL DATA COLLECTED DURING LANDING GEAR OVERHAUL. THE INTERVAL ESCALATION WAS ALSO APPROVED BY MRB /CHAIRMAN AND ISC CHAIRPERSON.

CM3211 00080

23-jul-08

MPD JUN.08 OEM TASK 32-040-01: 32-040-02 REVISED INTERVAL. TASK INTERVAL WAS REVISED FROM 18000FC TO 21000FC. THE ESCALATION WAS CONCURRED BY BOEING ENGINEERING AFTER REVIEWING LANDING GEAR DIMENSIONAL DATA COLLECTED DURING LANDING GEAR OVERHAUL. THE INTERVAL ESCALATION WAS ALSO APPROVED BY MRB /CHAIRMAN AND ISC CHAIRPERSON.

CM3211 00090

23-jul-08

MPD JUN.08 OEM TASK 32-040-01:

Date: 23-jul-08

HIGHLIGHTS

Page 21 of 23


HHI

MAINTENANCE SCHEDULE ITEM

DATE

737-6

REVISION REVISED INTERVAL. TASK INTERVAL WAS REVISED FROM 18000FC TO 21000FC. THE ESCALATION WAS CONCURRED BY BOEING ENGINEERING AFTER REVIEWING LANDING GEAR DIMENSIONAL DATA COLLECTED DURING LANDING GEAR OVERHAUL. THE INTERVAL ESCALATION WAS ALSO APPROVED BY MRB /CHAIRMAN AND ISC CHAIRPERSON.

CM3211 00100

23-jul-08

MPD JUN.08 OEM TASK 32-040-01: 32-040-02 REVISED INTERVAL. TASK INTERVAL WAS REVISED FROM 18000FC TO 21000FC. THE ESCALATION WAS CONCURRED BY BOEING ENGINEERING AFTER REVIEWING LANDING GEAR DIMENSIONAL DATA COLLECTED DURING LANDING GEAR OVERHAUL. THE INTERVAL ESCALATION WAS ALSO APPROVED BY MRB /CHAIRMAN AND ISC CHAIRPERSON.

CM3351 00010

23-jul-08

TASK CODE REVISED.

CM3453 00010

23-jul-08

NEW ITEM ADDED TO COVER NFL REQUIREMENT.

CM3531 00010

23-jul-08

DESCRIPTION TEXT CHANGED.

CM4900 01010

23-jul-08

MPD REFERENCE ADDED.

CM4900 01020

23-jul-08

MPD JUN.08 OEM TASK 49-062-00 REFERENCE ADDED.

CM4900 01030

23-jul-08

MPD JUN.08 OEM TASK 49-072-00 REFERENCE ADDED.

CM4900 01040

23-jul-08

MPD JUN.08 OEM TASK 49-082-00 REFERENCE ADDED.

CM7200 20010

23-jul-08

EDITORIAL CORRECTION OF INTERVAL.

CM7200 20060

23-jul-08

P/N ADDED IN CORRESPONDENCE TO ESM 05-11-02 REVISION.

CM7200 20070

23-jul-08

P/N CORRECTED IN CORRESPONDENCE TO ESM 05-11-02 REVISION.

Date: 23-jul-08

HIGHLIGHTS

Page 22 of 23


HHI

MAINTENANCE SCHEDULE ITEM

DATE

REVISION

CM7200 20080

23-jul-08

INTERVAL INFORMATION TRANSFERED FROM NOTE TO INTERVAL COLUMN. NOTE DELETED.

23-jul-08

P/N ADDED IN CORRESPONDENCE TO ESM 05-11-02 REVISION.

CM7200 20090

23-jul-08

P/N ADDED IN CORRESPONDENCE TO ESM 05-11-03 REVISION.

CM7200 20100

23-jul-08

P/N ADDED IN CORRESPONDENCE TO ESM 05-11-03 REVISION.

CM7200 20110

23-jul-08

INTERVAL CHANGED IN CORRESPONDANCE WITH ESM 05-11-03 REVISION TR 05-0091.

23-jul-08

INTERVAL INFORMATION TRANSFERED FROM NOTE TO INTERVAL COLUMN. NOTE DELETED.

23-jul-08

P/N ADDED IN ACCORDANCE WITH ESM 05-11-03.

CM7200 20120

23-jul-08

NOTE DELETED AND P/N CORRECTED. P/N 1498M45P07 COVERD WITH NEW MS ITEM.

CM7200 20210

23-jul-08

P/N ADDED IN ACCORDANCE WITH ESM 05-12-04.

CM7200 20230

23-jul-08

AAR REFERENCES UPDATED.

CM7200 20240

23-jul-08

NEW ITEM TO COVER P/N 1498M45P07.

Date: 23-jul-08

HIGHLIGHTS

737-6

Page 23 of 23


HHI

737-6

MAINTENANCE SCHEDULE ATA Break-Down

ATA

DEFINITION

ATA

DEFINITION

05 10

ZONE 100 FUSELAGE -LOWER HALF-

05 50

LEFT WING / RIGHT WING

05 11

BODY STA 130 TO STA 360

05 51

05 12

BODY STA 360 TO STA 540

05 13

BODY STA 540 TO STA 727

WING LEADING EDGE - FORWARD OF FRONT SPAR INBOARD OF NACELLE STRUT - INCLUDING NACELLE GAP COVER AREA

05 14

BODY STA 727 TO 1016

05 52

WING LEADING EDGE - FORWARD OF FRONT SPAR OUTBOARD OF NACELLE STRUT

05 19

WING TO BODY FAIRINGS

05 53

05 20

FUSELAGE - UPPER HALF -

WING INSPAR AREA (FUEL TANKS) - INBOARD OF WING RIB 22 - WS 643.50

05 21

FLIGHT COMPARTMENT BODY STA 178 TO STA 259.5

05 54

WING TRAILING EDGE FLAP TRACK FAIRINGS

05 22

PASSENGER COMPARTMENT BODY STA 259.5 TO STA 360

05 55

WING TRAILING EDGE - AFT OF REAR SPAR - INBOARD OF OUTBOARD TRAILING EDGE FLAP

05 23

PASSENGER COMPARTMENT BODY STA 360 TO STA 663.75

05 56

05 24

PASSENGER COMPARTMENT BODY STA 663.75 TO STA 1016

WING TRAILING EDGE - AFT OF REAR SPAR OUTBOARD OF INBOARD TRAILING EDGE FLAP INBOARD OF FIXED TRAILING EDGE

05 57

FIXED TRAILING EDGE - OUTBOARD OF OUTBOARD FLAP - INBOARD OF WING TIP WBL 658.17

05 30

ZONE 300-EMPENNAGE AND SECTION 48

05 31

FUSELAGE STA 1016 TO 1217

05 70

LANDING GEAR

05 32

FIN AND RUDDER

05 71

NOSE LANDING GEAR & DOORS

05 33

HORIZONTAL STABILIZER & ELEVATOR LEFT

05 73

LEFT MAIN LANDING GEAR & L.G. DOORS

05 40

POWER PLANTS & NACELLE STRUTS

05 80

ZONE 800- PASSENGER AND CARGO DOORS

05 41

NO. 1 POWERPLANT+ L/H NACELLE STRUT

05 82

DOORS, LOWER HALF FUSELAGE, L/H

05 43

LEFT NACELLE STRUT -

05 83

DOORS, UPPER HALF FUSELAGE, L/H

05 84

DOORS, UPPER HALF FUSELAGE, R/H

Date: 23-jul-08

ATA Break-Down

Page 1 of 5


HHI

737-6

MAINTENANCE SCHEDULE

ATA

DEFINITION

ATA

DEFINITION

05 90

EZAP

25 40

LAVATORIES

08 10

WEIGHING

25 52

CARCO COMPARTMENT LINING

21 25

RECIRCULATION SYSTEM

25 61

21 27

EQUIPMENT COOLING SYSTEM

ESCAPE STRAPS AND LANYARDS AND ESCAPE SLIDES (DOOR MOUNTED)

21 31

CABIN PRESSURE CONTROL SYSTEM

25 62

OVER-WATER SURVIVAL EQUIPMENT (OPTIONAL)

21 32

CABIN PRESSURE RELIEF

25 64

DETACHABLE EMERGENCY EQUIPMENT

21 33

CABIN PRESSURE INDICATION AND WARNING SYSTEM

25 66

DOOR-MOUNTED ESCAPE SYSTEM

25 71

ACCESSORY COMPARTMENTS

21 51

AIR COOLING SYSTEM

26 00

FIRE EXTINGUISHING SYSTEM

21 61

ZONE TEMPERATURE CONTROL AND INDICATION

26 14

LAVATORY SMOKE DETECTION

23 24

EMERGENCY LOCATOR TRANSMITTER

26 15

APU FIRE DETECTION SYSTEM

23 30

PASSENGER ADDRESS (PA) AND ENTERTAINMENT SYSTEM

26 20

FIRE EXTINGUISHING SYSTEM

26 23

EXTINGUISHING SYSTEM - CARGO COMPARTMENT

23 60

STATIC DISCHARGER

26 24

23 71

VOICE RECORDING SYSTEM

LAVATORY WASTE COMPARTMENT FIRE EXTINGUISHING

24 00

GENERAL

26 25

PORTABLE FIRE EXTINGUISHER

24 11

AC GENERATOR DRIVE SYSTEM

27 00

GENERAL

24 31

DC GENERATION SYSTEM

27 11

AILERON AND FLAPERON CONTROL SYSTEM

24 34

STANDBY POWER SYSTEM

27 21

RUDDER CONTROL SYSTEM

25 00

EQUIPMENT / FURNISHINGS

27 31

ELEVATOR CONTROL SYSTEM

25 11

FLIGHT COMPARTMENT SEATS

27 32

STALL WARNING

25 22

PASSENGER COMPARTMENT SEATS

27 41

HORIZONTAL STABILIZER CONTROL SYSTEM

25 25

CABIN ATTENDANT SEATS

27 51

FLAP/SLAT SYSTEM

Date: 23-jul-08

ATA Break-Down

Page 2 of 5


HHI

737-6

MAINTENANCE SCHEDULE

ATA

DEFINITION

ATA

DEFINITION

27 61

SPOILER AND SPEEDBRAKE CONTROL SYSTEM

32 11

MAIN LANDING GEAR SHOCK STRUT

27 62

AUTO SPEEDBRAKE CONTROL

32 21

NOSE LANDING GEAR SHOCK STRUT

27 81

LEADING EDGE SLAT SYSTEM

32 31

LANDING GEAR CONTROL SYSTEM

27 83

LEADING EDGE AUTOSLAT SYSTEM

32 32

MAIN LANDING GEAR EXTENSION AND RETRACTION

28 00

FUEL

32 34

NOSE LANDING GEAR EXTENSION AND RETRACTION

28 11

FUEL TANKS

32 35

LANDING GEAR ALTERNATE EXTENSION SYSTEM

28 13

FUEL VENT SYSTEM

32 41

BRAKE CONTROL SYSTEM

28 21

PRESSURE FUELING SYSTEM

32 44

PARKING BRAKE SYSTEM

28 22

ENGINE FUEL FEED SYSTEM

32 45

WHEELS, BRAKES, AND TIRES

28 25

APU FUEL FEED SYSTEM

32 51

NOSE GEAR STEERING SYSTEM

28 41

FUEL QUANTITY INDICATING SYSTEM (FQIS)

32 61

LANDING GEAR POSITION INDICATING AND WARNING

29 00

HYDRAULIC POWER

33 51

EMERGENCY LIGHTS

29 11

MAIN HYDRAULIC POWER SYSTEM

34 11

STATIC AND TOTAL AIR PRESSURE SYSTEM

29 18

GROUND SERVICING SYSTEM

34 24

STANDBY MAGNETIC COMPASS

29 21

STANDBY HYDRAULIC SYSTEM

34 53

AIR TRAFFIC CONTROL SYSTEM

29 22

POWER TRANSFER SYSTEM

34 60

FLIGHT MANAGEMENT COMPUTING

29 32

HYDRAULIC FLUID TEMPERATURE INDICATING SYSTEM

35 00

GENERAL

35 12

FLIGHT CREW OXYGEN SYSTEM

31 31

FLIGHT DATA RECORDER SYSTEM

35 21

PASSENGER / LLAR OXYGEN SYSTEM-CHEMICAL

31 51

CENTRAL WARNING SYSTEMS

35 22

PASSENGER OXYGEN SYSTEM-GASEOUS

31 62

COMMON DISPLAY SYSTEM

35 31

PORTABLE OXYGEN EQUIPMENT

32 00

GENERAL

36 14

APU BLEED SYSTEM

Date: 23-jul-08

ATA Break-Down

Page 3 of 5


HHI

737-6

MAINTENANCE SCHEDULE

ATA

DEFINITION

ATA

DEFINITION

38 11

STORAGE AND DISTRIBUTION

52 49

ACCESS AND BLOWOUT DOOR

38 32

VACUUM WASTE SYSTEM

52 60

AIR STAIRS

38 33

WASTE TANK QUANTITY INDICATION

52 70

COCKPIT DOOR

38 42

WATER TANK PRESSURIZATION SYSTEM

52 71

DOOR WARNING SYSTEM

49 00

AUXILIARY POWER UNIT (APU) - GENERAL

53 09

BODY UPPER

49 11

APU - SYSTEM

53 13

TAIL SECTION

49 13

APU MOUNTS

53 15

NOSE AND MAIN LANDING GEAR WHEEL WELL

49 15

APU AIR INTAKE SYSTEM

53 30

FUSELAGE EXTERIOR

49 16

APU DRAINS

53 51

WING-TO-BODY FAIRING

49 17

APU INSULATION PANELS

53 81

49 30

APU FUEL SYSTEM

UNDERFLOOR NOSE COMPARTMENT AND ELECTRONIC EQUIPMENT COMPARTMENT

49 41

IGNITION / STARTING

53 82

FORWARD CARGO COMPARTMENT

49 61

APU CONTROLS

53 84

AIR CONDITIONING COMPARTMENT LH AND RH

49 81

EXHAUST

53 85

AFT CARGO COMPARTMENT

49 91

APU EDUCTOR SYSTEM

54 30

PYLON-SKIN

52 11

PASSENGER ENTRY DOOR

54 40

ATTACHMENT FITTINGS

52 12

FORWARD AND AFT SERVICE DOORS

55 10

STABILIZER- HORIZONTAL

52 13

AFT ENTRY DOOR

55 20

52 22

EMERGENCY EXIT DOOR

ELEVATOR, HINGE SUPPORT AND BALANCE MECHANISM

52 31

CARGO DOOR

55 30

VERTICAL STABILIZER

52 48

EQUIPMENT COMPARTMENT EXTERIOR DOORS

55 40

RUDDER

56 11

FLIGHT COMPARTMENT WINDOWS

57 10

INTERSPAR WING

Date: 23-jul-08

ATA Break-Down

Page 4 of 5


HHI

737-6

MAINTENANCE SCHEDULE

ATA

DEFINITION

ATA

DEFINITION

57 12

FRONT AND REAR SPAR

74 21

IGNITION LEADS

57 14

CENTER WING BOX

78 11

TURBINE EXHAUST SYSTEM

57 15

MAIN LANDING GEAR TRUNNION SUPPORT BEAM

78 31

THRUST REVERSER SYSTEM ( HARDWARE)

57 21

LEADING EDGE

79 00

ENGINE OIL GENERAL

57 22

TRAILING EDGE

79 21

ENGINE OIL FILTER

57 31

WING UPPER SURFACE

80 11

STARTER

57 32

WING LOWER SURFACE

CM 21

AIR CONDITIONING

57 35

WING FITTINGS

CM 23

COMMUNICATIONS

57 52

TRAILING EDGE FLAPS

CM 24

ELECTRICAL POWER

57 54

SLATS

CM 25

EQUIPMENT/ FURNISHING

57 55

SPOILER

CM 26

FIRE PROTECTION

71 11

INLET COWL

CM 27

FLIGHT CONTROLS

71 71

ENGINE DRAINS

CM 28

FUEL

72 00

ENGINE

CM 29

HYDRAULIC POWER

72 20

FAN SECTION

CM 31

INSTRUMENTS

72 21

SPINNER CONE

CM 32

LANDING GEAR

72 23

THRUST MOUNT FITTINGS

CM 33

AIRCRAFT LIGHTING SYSTEM

72 30

COMPRESSOR SECTION

CM 34

NAVIGATION

72 50

TURBINE SECTION

CM 35

OXYGEN

72 60

ACCESSORY DRIVE SECTION

CM 36

PNEUMATIC

73 11

FUEL FILTER

CM 49

AUXILIARY POWER

73 21

FUEL CONTROL SYSTEM

CM 72

ENGINE

Date: 23-jul-08

ATA Break-Down

Page 5 of 5


HHI

737-6

MAINTENANCE SCHEDULE LIST OF EFFECTIVE ITEMS

05100- 00000 05100- 01000 05110- 00000 05110- 01000 05110- 02000 05111- 00000 05112- 00000 05120- 00000 05120- 01000 05120- 02000 05120- 03000 05120- 04000 05122- 00000 05130- 00000 05130- 01000 05130- 02000 05139- 00000 05141- 00000 05141- 01000 05141- 02000 05141- 03000 05142- 00000 05143- 00000 05145- 00000 05190- 00000 05191- 00000 05192- 00000 05194- 00000 05194- 01000 05195- 00000 Date: 23-jul-08

03-jun-04 22-mar-07 03-jun-04 03-jun-04 03-jun-04 23-jul-08 03-jun-04 22-mar-07 18-mar-05 18-mar-05 18-mar-05 03-jun-04 22-mar-07 18-mar-05 18-mar-05 03-jun-04 22-mar-07 22-mar-07 03-jun-04 18-mar-05 18-mar-05 22-mar-07 18-mar-05 23-jul-08 22-mar-07 03-jun-04 03-jun-04 03-jun-04 03-jun-04 23-jul-08

05200- 00000 05210- 00000 05210- 01000 05210- 02000 05220- 00000 05220- 01000 05220- 02000 05221- 00000 05222- 00000 05230- 00000 05230- 01000 05230- 02000 05230- 03000 05240- 00000 05240- 01000 05240- 02000 05240- 03000 05241- 00000 05242- 00000 05300- 00000 05300- 01000 05310- 00000 05310- 01000 05310- 02000 05310- 03000 05310- 04000 05321- 00000 05322- 00000 05322- 01000 05322- 02000

03-jun-04 03-jun-04 23-jul-08 03-jun-04 03-jun-04 22-mar-07 03-jun-04 22-mar-07 22-mar-07 03-jun-04 22-mar-07 05-sep-06 05-sep-06 22-mar-07 22-mar-07 22-mar-07 22-mar-07 22-mar-07 22-mar-07 22-mar-07 13-apr-00 22-mar-07 22-mar-07 22-mar-07 03-jun-04 03-jun-04 03-jun-04 22-mar-07 03-jun-04 03-jun-04

05323- 00000 05323- 01000 05324- 00000 05324- 01000 05325- 00000 05326- 00000 05331- 00000 05332- 00000 05332- 01000 05333- 00000 05333- 01000 05334- 00000 05335- 00000 05400- 00000 05410- 00000 05410- 01000 05410- 02000 05410- 03000 05411- 00000 05431- 00000 05432- 00000 05433- 00000 05434- 00000 05500- 00000 05500- 01000 05511- 00000 05511- 01000 05512- 00000 05512- 01000 05520- 00000

LIST OF EFFECTIVE ITEMS

22-mar-07 03-jun-04 22-mar-07 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 18-mar-05 22-mar-07 22-mar-07 22-mar-07 03-jun-04 03-jun-04 22-mar-07 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 05-sep-06 03-jun-04 03-jun-04 22-mar-07 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04

05521- 00000 05521- 01000 05526- 00000 05526- 01000 05531- 00000 05531- 01000 05532- 00000 05532- 01000 05533- 00000 05533- 01000 05534- 00000 05541- 00000 05542- 00000 05542- 01000 05543- 00000 05543- 01000 05544- 00000 05544- 01000 05551- 00000 05551- 01000 05552- 00000 05553- 00000 05553- 01000 05560- 00000 05561- 00000 05567- 00000 05571- 00000 05571- 01000 05571- 02000 05572- 00000

03-jun-04 03-jun-04 03-jun-04 25-apr-06 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 18-mar-05 03-jun-04 18-mar-05 03-jun-04 18-mar-05 03-jun-04 18-mar-05 03-jun-04 25-apr-06 03-jun-04 03-jun-04 23-jul-08 23-jul-08 03-jun-04 03-jun-04 03-jun-04 03-jun-04 23-jul-08 03-jun-04 Page 1 of 8


HHI 05700- 00000 05710- 00000 05730- 00000 05730- 01000 05800- 00000 05800- 01000 05821- 00000 05821- 01000 05822- 00000 05822- 01000 05831- 00000 05831- 01000 05833- 00000 05833- 01000 05834- 00000 05834- 01000 05841- 00000 05841- 01000 05843- 00000 05843- 01000 05844- 00000 05844- 01000 05900- 20290 05900- 20300 05900- 20310 05900- 20320 05900- 20330 05900- 20340 05900- 20350 05900- 20360 05900- 20370 05900- 20380 Date: 23-jul-08

737-6

MAINTENANCE SCHEDULE 03-jun-04 22-mar-07 22-mar-07 18-mar-05 22-mar-07 03-jun-04 22-mar-07 03-jun-04 22-mar-07 03-jun-04 22-mar-07 03-jun-04 03-jun-04 03-jun-04 22-mar-07 03-jun-04 22-mar-07 23-jul-08 03-jun-04 03-jun-04 22-mar-07 22-mar-07 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08

05900- 20390 05900- 20400 05900- 20410 05900- 20420 05900- 20430 05900- 20440 05900- 20450 05900- 20460 05900- 20470 05900- 20480 05900- 20490 05900- 20500 05900- 20510 05900- 20520 05900- 20530 05900- 20540 05900- 20550 05900- 20560 05900- 20570 05900- 20580 05900- 20590 05900- 20600 05900- 20610 05900- 20620 081000 01000 212502 40000 212503 00000 212700 70000 212700 71000 212700 89000 212701 00000 213100 71000

23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 18-mar-05 30-nov-05 03-jun-04 18-mar-05 03-jun-04 18-mar-05 18-mar-05

213203 70000 213300 00000 215103 00000 215105 40000 216106 10000 232400 00000 233011 00000 236000 76000 237100 71000 237100 73000 237121 00000 240000 01000 240000 02000 240000 03000 240000 04000 240000 05000 240000 06000 240000 07000 240000 08000 240000 09000 240000 09100 240000 10000 240000 11000 240000 13000 240000 14000 240000 15000 240000 16000 240000 18000 241141 00000 241161 20000 243141 72000 243400 71200

LIST OF EFFECTIVE ITEMS

03-jun-04 18-mar-05 03-jun-04 18-mar-05 25-apr-06 18-mar-05 23-jul-08 03-jun-04 18-mar-05 03-jun-04 03-jun-04 25-apr-06 18-mar-05 18-mar-05 05-sep-06 05-sep-06 22-mar-07 22-mar-07 05-sep-06 05-sep-06 22-mar-07 05-sep-06 05-sep-06 05-sep-06 18-mar-05 03-jun-04 05-sep-06 03-jun-04 25-apr-06 25-apr-06 03-jun-04 03-jun-04

250000 01000 250000 04001 250000 05001 250000 06001 250000 08001 250000 09001 250000 13001 250000 14001 250000 15001 250000 22000 251100 20000 251100 20100 251111 20000 252200 20000 252200 71000 252200 71100 252512 20000 252512 71000 252512 71200 254008 00000 255200 20000 255200 20100 255200 21000 256110 20000 256110 71000 256110 71100 256299 00001 256400 21000 256400 71100 256400 71200 256401 21000 256401 71000

23-jul-08 11-dec-01 11-dec-01 03-jun-04 11-dec-01 23-jul-08 11-dec-01 11-dec-01 11-dec-01 11-dec-01 22-mar-07 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 23-jul-08 03-jun-04 18-mar-05 22-mar-07 05-sep-06 05-sep-06 03-jun-04 23-jul-08 03-jun-04 30-nov-05 30-nov-05 03-jun-04 23-jul-08 Page 2 of 8


HHI 256402 90000 256403 20000 256404 90000 256405 90000 256600 71000 256601 00000 256601 20000 256601 40000 257100 21000 260000 01000 261400 73000 261401 10000 261500 71000 262000 01000 262000 02000 262000 21000 262001 72000 262001 72100 262001 72200 262001 73000 262002 21000 262003 21000 262300 00650 262300 01000 262300 02000 262300 03000 262300 04000 262300 05000 262401 00000 262401 01000 262401 90000 262500 01000 Date: 23-jul-08

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MAINTENANCE SCHEDULE 30-nov-05 22-mar-07 23-jul-08 23-jul-08 30-nov-05 22-mar-07 03-jun-04 23-jul-08 03-jun-04 13-apr-00 18-mar-05 18-mar-05 22-mar-07 03-jun-04 03-jun-04 25-apr-06 18-mar-05 03-jun-04 03-jun-04 05-sep-06 03-jun-04 03-jun-04 05-sep-06 05-sep-06 05-sep-06 05-sep-06 22-mar-07 05-sep-06 25-apr-06 25-apr-06 03-jun-04 03-jun-04

270000 00000 270000 01000 270000 02000 270000 03000 270000 04000 270000 05000 270000 06000 270000 07000 270000 08000 270000 09000 270000 10000 270000 11000 270000 12000 270000 13000 270000 14000 270000 15000 270000 16000 270000 17000 270000 18000 270000 19000 270000 20000 270000 21000 270000 22000 270000 25000 270000 32000 270000 35000 271100 21000 271100 21100 271100 71000 271100 71100 271100 73000 271100 82000

23-jul-08 03-jun-04 03-jun-04 03-jun-04 22-mar-07 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 18-mar-05 18-mar-05 23-jul-08 03-jun-04 03-jun-04 03-jun-04 03-jun-04 22-mar-07 03-jun-04 03-jun-04 18-mar-05 18-mar-05 23-jul-08 23-jul-08 23-jul-08 23-jul-08 03-jun-04 03-jun-04 18-mar-05 03-jun-04 22-mar-07 18-mar-05

271101 70000 271101 70100 271101 71000 271101 72000 271131 21000 271131 22000 271161 21000 272100 03000 272100 60000 272100 65000 272100 80000 272100 85000 272100 86000 272100 87000 272101 70000 272102 70000 272103 70000 272124 21000 272124 22000 272151 21000 272161 21000 272171 00000 272182 00000 273100 01000 273100 70000 273100 71000 273100 72000 273100 73000 273100 82000 273101 70000 273101 75000 273102 01000

LIST OF EFFECTIVE ITEMS

18-mar-05 03-jun-04 03-jun-04 30-nov-05 03-jun-04 29-apr-03 18-mar-05 23-jul-08 29-apr-03 18-mar-05 03-jun-04 25-apr-06 05-sep-06 05-sep-06 18-mar-05 18-mar-05 03-jun-04 03-jun-04 18-mar-05 18-mar-05 05-sep-06 03-jun-04 03-jun-04 18-mar-05 18-mar-05 18-mar-05 03-jun-04 18-mar-05 03-jun-04 18-mar-05 23-jul-08 03-jun-04

273111 00000 273114 21000 273114 21100 273114 22000 273117 20000 273120 00000 273134 21000 273134 21500 273161 21000 273164 90000 273200 71000 274100 70000 274101 70000 274102 70000 274103 70000 274141 21000 274181 00000 274181 01000 274181 21000 274191 70000 274197 70000 275100 21000 275100 71000 275100 72000 275100 73000 275100 74000 275100 74100 275101 21000 275101 74000 275106 21000 275132 22000 276100 21000

03-jun-04 18-mar-05 30-nov-05 03-jun-04 18-mar-05 18-mar-05 18-mar-05 23-jul-08 18-mar-05 18-mar-05 18-mar-05 18-mar-05 18-mar-05 18-mar-05 18-mar-05 18-mar-05 05-sep-06 23-jul-08 23-jul-08 18-mar-05 18-mar-05 22-mar-07 03-jun-04 03-jun-04 18-mar-05 03-jun-04 03-jun-04 03-jun-04 18-mar-05 23-jul-08 03-jun-04 23-jul-08 Page 3 of 8


HHI 276100 71000 276100 72000 276100 73000 276100 82000 276101 82000 276200 21000 276201 21000 276201 82000 276202 82000 278100 21000 278100 70000 278100 71000 278100 86000 278300 71000 280000 03000 280000 04000 280000 05000 280000 06000 280000 76000 281100 01000 281100 21000 281331 10000 281331 20000 281341 20000 281341 21000 282111 20000 282151 20000 282200 20000 282200 21000 282200 71000 282200 72000 282200 72100 Date: 23-jul-08

737-6

MAINTENANCE SCHEDULE 22-mar-07 30-nov-05 30-nov-05 03-jun-04 03-jun-04 23-jul-08 18-mar-05 05-sep-06 18-mar-05 18-mar-05 25-apr-06 18-mar-05 18-mar-05 03-jun-04 11-dec-01 11-dec-01 11-dec-01 23-jul-08 23-jul-08 23-jul-08 03-jun-04 03-jun-04 23-jul-08 03-jun-04 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 05-sep-06 03-jun-04 18-mar-05

282211 20000 282211 72000 282213 20000 282214 00000 282502 20000 282505 79000 284100 01000 284100 28000 284100 29000 284100 71000 290000 01000 290000 01100 290000 06000 290011 01000 291100 20000 291100 30000 291102 00000 291103 00000 291104 20000 291121 00000 291141 00000 291151 00000 291161 00000 291171 40000 291811 00000 292100 60000 292100 61000 292100 70000 292141 00000 292151 00000 292200 73000 292201 71000

23-jul-08 23-jul-08 18-mar-05 03-jun-04 23-jul-08 03-jun-04 23-jul-08 23-jul-08 23-jul-08 03-jun-04 11-dec-01 11-dec-01 03-jun-04 18-mar-05 25-apr-06 22-mar-07 30-nov-05 25-apr-06 23-jul-08 03-jun-04 18-mar-05 25-apr-06 18-mar-05 03-jun-04 03-jun-04 22-mar-07 30-nov-05 23-jul-08 22-mar-07 22-mar-07 03-jun-04 22-mar-07

292221 02000 293200 73000 313100 97000 313109 70000 315100 73000 315100 74000 315101 73000 315102 73000 316200 00000 320000 01000 320000 03000 320000 04000 320000 05000 320000 08000 320000 09000 320000 11000 320000 21000 320000 31000 320000 41000 320000 60000 320000 61000 320000 62000 320000 63000 320000 64000 320000 65000 320000 66000 320000 67000 320000 68000 320010 00000 321100 01000 321100 40000 321100 50000

LIST OF EFFECTIVE ITEMS

22-mar-07 03-jun-04 18-mar-05 03-jun-04 18-mar-05 18-mar-05 18-mar-05 18-mar-05 22-mar-07 22-mar-07 22-mar-07 25-apr-06 22-mar-07 03-jun-04 22-mar-07 24-mar-99 24-mar-99 23-jul-08 24-mar-99 22-mar-07 22-mar-07 18-mar-05 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 03-jun-04 22-mar-07 22-mar-07 05-sep-06

322100 00000 322100 21000 322100 22000 322100 60000 322110 00100 322110 00200 322110 10000 322171 20000 323100 00000 323151 20000 323171 40000 323221 00000 323400 70000 323500 73000 324100 71000 324100 72000 324131 00000 324141 70000 324181 00000 324400 79000 324411 00000 324500 70000 324511 40000 324521 00000 325121 00000 326100 71000 335100 72000 335103 96000 335105 96000 341100 17000 341100 79000 341101 17000

22-mar-07 22-mar-07 22-mar-07 03-jun-04 22-mar-07 05-sep-06 03-jun-04 23-jul-08 25-apr-06 22-mar-07 03-jun-04 05-sep-06 25-apr-06 25-apr-06 18-mar-05 03-jun-04 22-mar-07 03-jun-04 22-mar-07 22-mar-07 22-mar-07 23-jul-08 03-jun-04 03-jun-04 22-mar-07 30-nov-05 03-jun-04 03-jun-04 03-jun-04 18-mar-05 03-jun-04 22-mar-07 Page 4 of 8


HHI 341101 20000 341102 20000 342400 02000 345300 73000 346002 00001 350000 01000 350000 02000 350000 04000 350000 05000 350000 06000 350000 09000 351200 70000 351200 70001 351200 71000 352101 00000 352101 01000 352200 70000 352231 21000 353100 71000 361400 00000 381106 00000 381106 10000 381106 20000 383200 10000 383202 00100 383203 00000 383205 96000 383300 74000 384210 96000 490011 10000 491111 40000 491311 20000 Date: 23-jul-08

737-6

MAINTENANCE SCHEDULE 18-mar-05 18-mar-05 29-apr-03 23-jul-08 23-jul-08 11-dec-01 11-dec-01 03-jun-04 11-dec-01 11-dec-01 18-dec-02 05-sep-06 03-jun-04 25-apr-06 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 22-mar-07 03-jun-04 18-mar-05 22-mar-07 05-sep-06 18-mar-05 22-mar-07 03-jun-04 03-jun-04 03-jun-04 23-jul-08 03-jun-04 03-jun-04

491511 20000 491522 00000 491611 10000 491611 11000 491611 19900 491711 20000 493011 40000 493021 00000 494151 20000 496100 70000 496100 90000 498111 20000 498111 20100 498111 20200 499111 00000 499113 20000 499141 20000 499171 20000 499171 21000 521100 00000 521100 01000 521100 02000 521100 03000 521100 04000 521100 05000 521100 06000 521100 09000 521100 09100 521100 09200 521200 00000 521200 00500 521200 01000

03-jun-04 03-jun-04 23-jul-08 23-jul-08 18-mar-05 03-jun-04 23-jul-08 03-jun-04 23-jul-08 30-nov-05 23-jul-08 03-jun-04 23-jul-08 03-jun-04 23-jul-08 03-jun-04 03-jun-04 03-jun-04 22-mar-07 03-jun-04 30-nov-05 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 30-nov-05

521200 01500 521200 02000 521200 02500 521200 03000 521200 03500 521200 04000 521200 05000 521200 06000 521300 00000 521300 01000 521300 02000 521300 03000 521300 04000 521300 05000 521300 06000 522200 00000 522200 01000 522200 02000 522200 03000 522200 04000 522200 05000 522200 06000 522200 07000 522200 07500 523100 00000 523100 00500 523100 01000 523100 01500 523100 02000 523100 03000 523100 05000 523100 06000

LIST OF EFFECTIVE ITEMS

30-nov-05 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 30-nov-05 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 18-mar-05 03-jun-04 03-jun-04 03-jun-04 18-mar-05 18-mar-05 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04

524800 00000 524800 02000 524800 03000 524800 04000 524800 07000 524900 00000 524900 01000 524900 02000 526000 00000 526000 01000 526050 21000 527000 00000 527000 01000 527000 02000 527000 03000 527000 04000 527000 05000 527000 07000 527001 00000 527001 01000 527001 02000 527001 04000 527100 00000 530900 00000 530900 01000 530900 02000 530900 03000 530900 04000 530900 05000 530900 06000 530900 07000 530900 08000

03-jun-04 23-jul-08 05-sep-06 05-sep-06 03-jun-04 03-jun-04 03-jun-04 03-jun-04 23-jul-08 23-jul-08 23-jul-08 30-nov-05 03-jun-04 03-jun-04 03-jun-04 03-jun-04 23-jul-08 23-jul-08 23-jul-08 03-jun-04 23-jul-08 23-jul-08 03-jun-04 18-mar-05 23-jul-08 03-jun-04 03-jun-04 03-jun-04 23-jul-08 03-jun-04 03-jun-04 23-jul-08 Page 5 of 8


HHI 530900 09000 530900 10000 530900 11000 530900 12000 530900 13000 530900 14000 530900 15000 530900 16000 531300 00000 531300 01000 531300 02000 531500 00000 531500 01000 531500 02000 531500 03000 531500 04000 533000 00000 533000 01000 533000 02000 533000 03000 533000 04000 533000 05000 533000 06000 535100 00000 538100 00000 538100 01000 538100 02000 538200 00000 538200 01000 538200 02000 538200 03000 538200 04000 Date: 23-jul-08

737-6

MAINTENANCE SCHEDULE 03-jun-04 23-jul-08 23-jul-08 03-jun-04 23-jul-08 03-jun-04 03-jun-04 03-jun-04 03-jun-04 22-mar-07 03-jun-04 03-jun-04 23-jul-08 23-jul-08 03-jun-04 23-jul-08 03-jun-04 03-jun-04 03-jun-04 05-sep-06 18-mar-05 05-sep-06 03-jun-04 03-jun-04 18-mar-05 03-jun-04 03-jun-04 18-mar-05 03-jun-04 05-sep-06 03-jun-04 03-jun-04

538400 00000 538500 00000 538500 01000 538500 02000 538500 03000 538500 04000 543000 00000 543000 01000 543001 00000 543002 00000 544000 00000 544000 01000 544000 02000 544000 03000 544000 04000 544000 05000 544000 06000 544000 06100 551000 00000 551000 01000 551000 02000 551000 03000 551000 05000 551000 06000 551000 07000 552000 00000 552000 01000 552000 03000 553000 00000 553000 01000 553000 02000 554000 00000

03-jun-04 18-mar-05 03-jun-04 05-sep-06 03-jun-04 03-jun-04 25-apr-06 25-apr-06 30-nov-05 30-nov-05 23-jul-08 03-jun-04 25-apr-06 05-sep-06 25-apr-06 03-jun-04 23-jul-08 23-jul-08 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 23-jul-08 23-jul-08 03-jun-04 23-jul-08 03-jun-04

561100 00000 561100 01000 561100 02000 561100 03000 571000 00000 571000 01000 571000 02000 571000 03000 571000 04000 571000 05000 571200 00000 571400 00000 571400 01000 571400 02000 571400 03000 571400 04000 571400 05000 571400 05500 571400 07000 571500 00000 572100 00000 572200 00000 573100 00000 573100 02000 573200 01000 573200 02000 573200 03000 573200 04000 573200 05000 573500 00000 575200 00000 575200 01000

LIST OF EFFECTIVE ITEMS

03-jun-04 03-jun-04 23-jul-08 23-jul-08 25-apr-06 25-apr-06 25-apr-06 23-jul-08 03-jun-04 03-jun-04 03-jun-04 25-apr-06 05-sep-06 23-jul-08 05-sep-06 23-jul-08 23-jul-08 23-jul-08 23-jul-08 25-apr-06 03-jun-04 23-jul-08 23-jul-08 25-apr-06 23-jul-08 25-apr-06 25-apr-06 25-apr-06 25-apr-06 23-jul-08 25-apr-06 25-apr-06

575200 02000 575200 06000 575200 07000 575400 00000 575500 00000 711101 20000 711102 20000 711103 20000 711104 20000 717100 20000 717100 70000 720000 20000 720000 20200 720000 20300 720000 20400 720011 01200 720021 00200 722000 21000 722100 20000 722100 22000 722304 20000 722304 21000 723000 31000 725000 20000 726000 20000 731102 00000 732100 74000 742101 20000 742102 20000 781100 21000 783100 70000 783100 71000

25-apr-06 03-jun-04 03-jun-04 25-apr-06 25-apr-06 03-jun-04 23-jul-08 02-aug-99 03-jun-04 23-jul-08 25-apr-06 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 03-jun-04 25-apr-06 23-jul-08 23-jul-08 18-mar-05 23-jul-08 30-nov-05 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 Page 6 of 8


HHI 783100 73000 783106 20000 783107 90000 783112 20000 783112 21000 783114 20000 783123 20000 790000 20000 790000 20500 790000 80000 792103 00000 792106 00000 801101 20000 CM2132 00000 CM2324 00000 CM2371 00010 CM2430 00010 CM2560 00020 CM2560 00021 CM2560 00030 CM2560 00031 CM2564 00020 CM2564 00090 CM2566 00010 CM2566 00020 CM2566 00030 CM2566 00040 CM2600 00010 CM2621 00010 CM2621 00020 CM2622 00010 CM2622 00020 Date: 23-jul-08

737-6

MAINTENANCE SCHEDULE 18-mar-05 23-jul-08 23-jul-08 23-jul-08 23-jul-08 18-mar-05 23-jul-08 23-jul-08 23-jul-08 18-mar-05 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 03-jun-04 23-jul-08 23-jul-08 23-jul-08 23-jul-08 18-mar-05 25-apr-06 23-jul-08 03-jun-04 22-mar-07 26-jun-02 22-mar-07 30-nov-05 03-jun-04 30-nov-05 03-jun-04

CM2623 00010 CM2626 00010 CM2626 00020 CM2721 00010 CM2740 00020 CM2822 00010 CM2900 00010 CM2900 00020 CM2900 00030 CM2911 00010 CM2921 00010 CM2921 00020 CM2999 00010 CM2999 00020 CM2999 00030 CM3131 00010 CM3211 00010 CM3211 00020 CM3211 00030 CM3211 00040 CM3211 00050 CM3211 00060 CM3211 00070 CM3211 00080 CM3211 00090 CM3211 00100 CM3211 02000 CM3211 03000 CM3211 04000 CM3211 05000 CM3211 06000 CM3211 07000

03-jun-04 30-nov-05 30-nov-05 30-nov-05 23-jul-08 03-jun-04 03-jun-04 23-jul-08 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 23-jul-08 03-jun-04 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02

CM3211 08000 CM3211 09000 CM3211 10000 CM3211 11000 CM3211 12000 CM3211 13000 CM3211 14000 CM3211 15000 CM3211 16000 CM3211 17000 CM3211 18000 CM3211 19000 CM3211 20000 CM3211 21000 CM3211 22000 CM3211 23000 CM3211 24000 CM3211 25000 CM3211 26000 CM3211 27000 CM3211 28000 CM3211 29000 CM3211 30000 CM3211 31000 CM3211 32000 CM3211 33000 CM3211 34000 CM3211 35000 CM3211 36000 CM3211 37000 CM3211 38000 CM3211 39000

LIST OF EFFECTIVE ITEMS

17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02

CM3211 40000 CM3221 00010 CM3221 00020 CM3221 00030 CM3221 01040 CM3221 02000 CM3221 03000 CM3221 04000 CM3221 05000 CM3221 06000 CM3221 07000 CM3221 08000 CM3221 09000 CM3221 10000 CM3221 11000 CM3221 12000 CM3221 13000 CM3221 14000 CM3221 15000 CM3221 16000 CM3221 17000 CM3221 18000 CM3221 19000 CM3221 20000 CM3221 21000 CM3232 00010 CM3241 00020 CM3241 00030 CM3351 00010 CM3410 00010 CM3453 00010 CM3510 00010

17-oct-02 03-jun-04 03-jun-04 03-jun-04 12-jun-01 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 03-jun-04 17-oct-02 17-oct-02 17-oct-02 17-oct-02 22-mar-07 03-jun-04 03-jun-04 23-jul-08 29-apr-03 23-jul-08 03-jun-04 Page 7 of 8


HHI CM3512 00010 CM3512 01010 CM3522 00110 CM3531 00010 CM3610 00010 CM3610 00020 CM4900 01010 CM4900 01020 CM4900 01030 CM4900 01040 CM7200 20010 CM7200 20020 CM7200 20030 CM7200 20040 CM7200 20050 CM7200 20051 CM7200 20060 CM7200 20070 CM7200 20080 CM7200 20090 CM7200 20100 CM7200 20110 CM7200 20120 CM7200 20130 CM7200 20140 CM7200 20150 CM7200 20160 CM7200 20170 CM7200 20180 CM7200 20200 CM7200 20210 CM7200 20230 Date: 23-jul-08

MAINTENANCE SCHEDULE 30-nov-05 03-jun-04 03-jun-04 23-jul-08 18-mar-05 03-jun-04 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 22-mar-07 22-mar-07 18-mar-05 22-mar-07 22-mar-07 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 18-mar-05 18-mar-05 18-mar-05 18-mar-05 22-mar-07 18-mar-05 11-jan-01 23-jul-08 23-jul-08

CM7200 20240

737-6

23-jul-08

LIST OF EFFECTIVE ITEMS

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1

737-6

GENERAL

This Maintenance Schedule constitutes the maintenance program for the systems, power plant and structure of the B737-700 aircraft as defined/required by Regulation (EC) 2042/2003 Part M. It includes scheduled maintenance tasks and frequencies required by the B737-6/-7/-8 MAINTENANCE REVIEW BOARD REPORT (MRB Document) and other mandatory requirements, complemented by additional maintenance tasks considered for their economical effectiveness, reliability improvement as well as for passenger comfort and appearance reasons. The Maintenance Schedule is part of the approved maintenance system. Other part of the maintenance system is the Component Maintenance Section.

1.1

Validity

This Maintenance Schedule is valid for all Boeing B737-700 aircraft equipped with CFM56-7B22 / -7B24 Engine and GTCP131-9B APU operated by: Hamburg International Luftverkehrsgesellschaft mbH Hindenburgstr. 171 D-22297 Hamburg Germany For aircraft basic data information, see chapter 5.

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1.2

737-6

Responsibilities

This Maintenance Schedule is prepared under the responsibility of Hamburg International by: Lufthansa Technik Aktiengesellschaft Department FRA WE Rhein-Main Airport 60546 Frankfurt/Main Germany This Maintenance Schedule is owned and released by : Hamburg International Luftverkehrsgesellschaft mbH Hindenburgstr. 171 D-22297 Hamburg Germany

1.3

Average Utilization

The application of this maintenance program assumes an average utilization of 3000 + 10% FH per year. Some items are sensitive to flight length and require both flight hours and flight cycles to determine the implementation threshold. For those items the threshold is determined by the Flight Length Sensitive (FLS) Threshold Curve (MPD Section 9 Figure 1 and 2). In addition, for supplemental structural inspection items the Damage Tolerance Rating (DTR) system is used to determine the inspections and repeat intervals necessary to provide adequate fatigue damage detection . All Items depending on Flight Length Sensitive (FLS) Threshold Curve and DTR Check Forms are determined based on an average FC to FH ratio of 0.46. The thresholds/intervals will be recalculated if a major change to the HHI flight profile occurs. Items depending on FLS/DTR are identified in the Interval Note NOTE(I), e.g. MS57.14.00.05500

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1.4

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Operator’s Statement

With reference to Appendix 1 to AMC M.A.302 Para. 1.1.4, Hamburg International confirms, that aircraft mentioned under section 1.1 will be maintained to this program, which will be reviewed and updated as required by AMC M.A.302 and as outlined in MM & OE Part 3, Chapter 3.2.

With reference to Appendix 1 to AMC M.A.302, Para. 1.1.18, Hamburg International confirms, that the practices and procedures to satisfy this program are to the standards specified in the Type Certificate Holder’s Maintenance Instructions.

-------------------------------------------------------------------Hamburg International Luftverkehrsgesellschaft mbH the Operator

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1.5

737-6

Authority Approval

According to M.A.302 (a) & (b), this document and any subsequent amendment must be approved by the German Airworthiness Authority „Luftfahrt Bundesamt (LBA)“. Details about approval requirement are described in para. 2.14.1. For signature, see Document Approval Sheet.

1.6 A.

B. C.

D.

Explanation of Regulation Due to practical considerations, splitting of maintenance checks or packages and performance together with lower maintenance events may be possible as long as it is assured that each check item mentioned in the interval column of the Maintenance Schedule will be repeated at the required maintenance interval. Flight hour and cycle limited items can also be treated in accordance with this paragraph. If necessary, a check to be performed on parts/components located in several positions at the aircraft (e.g. at engine 1 and 2) may be performed together with other, lower maintenance events as long as the time between the check does not exceed the inspection interval. The maintenance intervals specified in the Maintenance Schedule must not exceed the end of a scheduled flight program (see Flight Program). If a flight program should exceed the normal standard flight time (see Normal Standard Flight Time) respectively the scheduled layover time due to events that are beyond the control of the Aircraft Routing Department. (e.g. alternate landings, strong headwinds, holding, delays, cancellations) the maintenance interval (flight hours or calendar time) may be exceeded as far as it is necessary for the aircraft to complete its flight program until reaching the maintenance station (see Maintenance Station) determined for this particular flight program. Continuing Airworthiness and other Service Information must be continuously evaluated by the operator and, where necessary, appropriate action must be taken to amend the Maintenance Schedule.

1.6.1 Flight Program Is a flight of a certain aircraft from a certain predetermined maintenance station, via several line stations, back to that maintenance station or to another predetermined maintenance station.

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1.6.2 Normal Standard Flight Time Is the time, which has been pre calculated and will serve as a basis for aircraft routing and operational control.

1.6.3 Maintenance Station In this context is a station, where Daily-Checks and higher checks are performed

1.7

Revision Procedure

Revisions of this Maintenance Schedule will be prepared under the responsibility of Hamburg International by Lufthansa Technik AG, Engineering Dept. FRA WE and released by Hamburg International Luftverkehrsgesellschaft mbH and approved by the German Airworthiness Authority „Luftfahrt Bundesamt (LBA). MS pages amendments will be issued with a new effectivity date. Every amendments issue will include a list of highlights indicating significant changes. Each revision should be signed off in the Record Sheet of Revision. Following chapters of the MS are reissued completely with every MS revision : • • • • • •

Table of Contents Highlights ATA Break Down List of Effective Items Introduction Aircraft Zones

Only those pages with issue date of the latest revision (according to Record of Revision page) shall be used.

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Temporary Revisions Changes to the Maintenance Schedule with high importance and/or high urgency may be incorporated between the regular revision periods by issue of a Temporary Revision (TR). The TR is edited including the following parts: • List of Effective Pages (LEP) • Approval Sheet • Record of Eff. Temporary Revisions • Introduction Page(s) (if necessary) and /or MS Page(s), where tasks have been changed/added/deleted. The TR must be filed into the Maintenance Schedule document, which should be confirmed in the “Record of Revision“ Sheet 2 (“Page 2 of 2”). If a subsequent regular MS Revision includes or supersedes a TR, this will be stated in the Highlights of that respective Revision. The “Record of Eff. Temporary Revisions“ Sheet lists only those TRs which are still effective.

1.8

Reliability Monitoring Program

A Reliability Monitoring Program acc. to M.A.301 (4) is necessary to ensure the effectiveness of the maintenance program. Review of the reliability data will be used to adjust the maintenance program as required. Accordance. to Appendix 1 to AMC M.A.302 Item 5.2.the Operator will review the detailed requirements for the Maintenance Program annually for continued validity in the light of operating experience. See also CAMOE Part 3 Chapter 3.10.

1.8.1 Aircraft Reliability Monitoring Aircraft and engine reliability data can be retrieved from the HHI Reliability Report, issued on a monthly basis. The report contains data regarding operational parameters such as aircraft in service, total flight hours, total take off, daily utilization, etc... including data regarding incidents, maintenance- and pilot-reports and delays/cancellations.

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1.8.2 Engine Condition Monitoring Engine parameters like EGT, Fuel Flow, N2 and N1 will be recorded on the Engine and Cruise Report and sent to Engineering. The parameters are continuously analyzed by engineering and, if necessary, will result in a corrective maintenance action.

1.8.3 Component Reliability Monitoring Component reliability data such as MTBR, MTBUR and MTBF will be retrieved from Lufthansa Technik EDP system with „CORIS“.

1.9

Reference Documents

This Maintenance Schedule is developed from the following documents : - B737-6/-7/-8 Maintenance Review Board Report, issued by the FAA // Revision March 2007 // incl. TR 02-003 and TR02-004 - B737-6/-7/-8 Maintenance Planning Document (Boeing-Document No.: D626A001), issued by Boeing // Revision June 2008 // - B737 Airworthiness Limitation (AWLs) and Certification Maintenance Requirements CMR (Boeing-Doc No. D626A001-CMR) dated // March 2008 // - CFM56-7B Engine Manual Revision 37 issued by SNECMA, dated 15 May 2008. - APU Manual 49-00-00, Revision 4, dated 05. Oct. 2007.

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2

MAINTENANCE PROGRAM

2.1

Line Maintenance

737-6

The responsibility for accomplishing the task may be indicated in the "Performed-by"-column (FC = Flight Crew incl. Cabin Crew / SM = Station Mechanic). If this column is blank, the task is the duty of the maintenance personal. T = Trip Check Tasks to be performed by flight crew are to be accomplished prior to each flight. Tasks may also be performed by station mechanics. Trip Check has to be performed at ramp position not earlier than two hours before take-off. The Trip Check covers the requirements from Appendix 1 to AMC M.A.302, Item 1.1.9 Pre-Flight-Inspection Note: Before training - and test-flights - before the first takeoff of a training period and after each flight training period a walk around check has to be performed. The trip check has to be repeated if the training /test flight is interrupted for more than 2 hours. Z = Daily Check Tasks to be accomplished every 48 hours elapsed time. All other items in this Maintenance Schedule issue are listed in usage parameters (days, month, flight hours, cycles), as given in the manufacturer documentation. Where intervals are given in two dimensions (e.g. 75 days / 400 cycles), the rule "Which ever comes first" applies. HHI together with LHT production planning may find it useful to group the items from this Maintenance Schedule to packages which will be performed together. Eventually, these groups may be given check abbreviations as monthly, annual or letter checks. However, the maximum interval given in this Maintenance Schedule must not be exceeded. These groups may be handled independent from this Maintenance Schedule, or if deemed useful, be introduced in this Maintenance Schedule.

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2.2

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Base Maintenance

All tasks included within the Annual Visit inspections and higher are considered to be Base Maintenance.

2.3

Time Controlled Maintenance

In addition to the intervals expressed in letter-codes, usage parameters such as • flight hours: FLH • flight cycles: CYC • calendar time • days: DAY • months: MTH • years: YRS • Engine/APU change : EC/AC • S. N (see Note): Indicated that check-interval is described in an interval (I) note. are called for where appropriate.

2.4

Zonal Inspection Program

The Zonal Inspection Program is contained in the ATA Chapter 05. It requires a General Visual Inspection (i.e. task code E1 or E2) of the specified aircraft zone in order to check system and power plant installation and structure for security and general condition. The extent of the inspection is defined by the access (identification of access doors, positioning of surfaces, removal of linings) and the whole of the zone is to be inspected as visible with the relevant access open. No inspection aid is required for accomplishment of inspections, however an additional lighting source may be used as deemed necessary. According AOM, VOL II, chapter 6.10, the flight crew shall perform an airplane's inspection of general condition which must include a check for obvious wear and damage of engines in/outlets, nose/main gear wheels, tires and brakes. This inspection is required due to the flight crew's obligation to assess the airworthiness of the airplane before each flight. As a result general visual inspection of airplane's condition and for obvious wear and damage of engines in/outlets, nose/main gear wheels, tires and brakes before each flight may be considered as crew tasks and therefore be excluded from the scheduled maintenance program. Date: 23-Jul-2008

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2.4.1 Enhanced Zonal Analysis Procedure (EZAP) An enhanced zonal analysis was performed for the interior of fuel tanks which contain electrical wiring and have a potential for combustible materials being present. This enhanced zonal analysis provided a means to identify applicable and effective tasks to minimize wiring contamination and to detect significant wiring installation discrepancies that may not be reliably detected through a standard zonal inspection. These dedicated tasks, containing (EZAP) in parenthesis as an identifier, are included in this MS under ATA 20. They are not system specific and do not have a failure effect category. Unless otherwise specified in the task, the disassembly of the bundle, connections, or clamps is not required. Wiring that is undisturbed will have less degradation than wiring that is disturbed during maintenance. The enhanced zonal analysis uses the existing Zonal requirements for a basis. All Zonal inspection requirements constitute Electrical Wiring Interconnection System (EWIS) Instructions for Continued Airworthiness (ICA). Electrical Wiring Interconnection System (EWIS) is used to describe inspection criteria. The term EWIS means any wire, wiring device, or combination of these, including termination devices, installed in the airplane for transmitting electrical energy between two of more termination points.

2.5

Structure Program

The Structure Program provides tasks and frequencies applicable to the aircraft structure with respect to fatigue damage, environment deterioration (corrosion) and accidental damage. For fatigue, flight cycles are used as the parameter for inspection thresholds and repeat intervals. (Threshold figures are identified by the abbreviation "T" in the intervals column). For environmental deterioration, as corrosion is mainly age dependent, inspection thresholds and repeat intervals are expressed in letter codes IL or D, which is a calendar time limit. For accidental damage, the repeat intervals are expressed in letter codes or flight cycles according to the damage consequence considered. Due to the random characteristics of accidental damage an inspection threshold is not introduced.

2.6

(Not used)

2.7

Corrosion Prevention and Control Program (CPCP)

The B737-600/-700/-800 Corrosion Prevention and Control Program (CPCP) is an integral part of the Structural Maintenance Program.

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2.8

737-6

Identification of Type Certification and MRB Requirements

2.8.1 MSI, SSI, AWL and CMR Maintenance Significant Items (MSI) and Structural Significant Items (SSI) arise from the B737-6/-7/-8 MRB-Document. Airworthiness Limitation Items (AWLs) arise from the B737-6/-7/-8/-9 AWL and CMR-Document D626A001-CMR. One section of the Airworthiness Limitations contains an FAA approved program of scheduled inspections for operators to incorporate into their maintenance program for this type design to meet the new standards and assumptions introduced by FAA AC 25.981 and Special Federal Aviation Regulation SFAR No. 88. An AWL may be: an Airworthiness Limitation Instruction (ALI) or a Critical Design Configuration Control Limitation (CDCCL). ALIs identify inspection tasks related to fuel tank ignition source prevention which must be done to maintain the design level of safety for the operational life of the airplane. These ALIs are mandatory and cannot be changed or deleted without the approval of the FAA office that is responsible for the airplane model Type Certificate, or applicable regulatory agency. Strict adherence to methods, techniques and practices as prescribed is required to ensure the ALI is complied with. Any use of methods, techniques or practices not contained in these ALIs must be approved by the FAA office that is responsible for the airplane model Type Certificate, or applicable regulatory agency. Certification Maintenance Requirements (CMR) for system tasks arise from systems safety assessment. They are described in Section 9 of the B737-6/-7/-8 Maintenance Planning Document. These requirements are allocated to two categories (identified as "one star" and "two star") according to the failure condition consequence and the sensitivity of the safety objective to an interval increase. The identification of these items in the Maintenance Schedule is provided as follows: • MSIs are identified by quoting the MSI-number from the MRB-Document together with the MSG 3-Route (named MSG-Cat in the Maintenance Schedule) selected for this MSI. - Route 5 = Evident Safety Effects - Route 6 = Evident Economic (Operational) Effects - Route 7 = Evident Economic (Non-Operational) Effects - Route 8 = Hidden Function Safety Effects - Route 9 = Hidden Function Non-Safety Effects - Route 0 = Task Generated by MRB Determination Example: MRB 25-020-00 RTE:8 Date: 23-Jul-2008

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SSIs All SSI’s identified by the Manufacturer have been subjected to the MSG-3 analysis. This process has resulted in the identification of maintenance inspection tasks which are contained in the MRBR. SSIs are identified by quoting “MRB XX-3XX”. • AWLs are identified by quoting “AAR XX-AWL-XX“. The first and the second digits are the ATA Chapter Number. Example: AAR 28-AWL-01 • CMRs are identified by quoting “AAR CMR“. Example: CMR (525199 00002) All these references are located in the References column of the Maintenance Schedule.

2.9

Component Maintenance Program

The Component Maintenance Section ( Chapter CMS) reflects specific component maintenance tasks mandated by Airworthiness Authority Requirements. The storage requirements and limitations of Components are processed and controlled by Lufthansa Technik Component Tracking department.

2.10 Inspection Techniques Whenever the term "inspect" or "check" for satisfactory conditions is specified in this schedule, the term is defined as follows: • That the Zone / System / Item inspection is sufficient to establish at the time of inspection it is free of any defects likely to affect airworthiness and is expected to remain airworthy until the next scheduled inspection is due. • The inspection must comply with the minimum standards set out hereunder having regard to the environment and to the materials of construction of the Zone / System / Item. • Unless otherwise stated in the schedule, all the inspection requirements are to be applied without removing an item from the aircraft or dismantling the item in-situ unless this is considered essential, in which case this is specified. This, however, does not preclude removal or dismantling, or such other inspection activity as is considered essential. • Where a particular area or item is highlighted in the item it is considered as significant and should be given special attention during inspection.

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Metal Parts All structural members, honeycomb bonded structure, bodies or casings of units in systems and in instrument, electrical and radio installations, metal pipes ducting, tubes, rods, levers, etc., inspect for: • Cleanliness, evidence of external damage, leaks, overheating or discharge, bulging, obstructions of drainage or vent holes, security of attachments, fasteners and visible connections, locking and bonding. • Freedom of cracks (visual) distortion, dents, bolts, screws. • Separation of bond, failure of welds and spot welds. Deterioration of protective treatment and corrosion. Correct sealing of fairings, fluid ingress. Rubber, Fabric, Fiber Glass and Plastic Parts Honeycomb bonded structure, ducting, flexible pipes, flexible mountings, seals, insulation of electrical cables, windows etc. Inspect for: • Separation of bond, cleanliness, cracks, cuts, chafing, kinking, twisting, crushing, sufficient free length for movement, deterioration, crazing, loss of flexibility, overheating, fluid spillage. • Security of attachment (supports, packings and electrical bonding correctly positioned, serviceable). Fuel Airworthiness Limitations CDCCLs • The purpose of the CDCCL is to provide instructions to retain critical ignition source prevention feature during configuration change that may be caused by alterations, repairs, or maintenance actions. For details refer to Boeing CMR (Boeing-Doc No. D626A001-CMR), latest revision (see chapter 1.9). All applicable manufacturer documents have been revised accordingly. (e.g. AMM,CMM,…) Control System Components Inspect for: • Correct alignment, no fouling. Free movement, distortion, evidence of bowing, scores, chafing, fraying, kinking, evidence of wear, fretting, cracks, loose rivets, deterioration of protective treatment, corrosion. Electrical bonding correctly positioned, undamaged and secure. Attachments, connections and locking secure. Electrical Motors, Alternators, Generators and Actuators Inspect for: • Cleanliness, obvious damage, corrosion, evidence of overheating, security of attachments and connections. • If protective covers are required to be removed: check for cleanliness, scoring, pitting, brushes free in holders, not excessively worn and correct bedding. Adequate spring tension, overheating and fluid ingress. Date: 23-Jul-2008

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Relays, Solenoids and Contactors Inspect for: • Cleanliness, obvious damage, corrosion, evidence of overheating, security of attachments and connections. • If protective covers are required to be removed: check for cleanliness, pitting or burning of contactors, evidence of overheating and security of contacts exposed. Electrical looms For the purpose of electrical inspections, it is understood that the stripping of looms is not normally contemplated, though in particular instances it may be required and will be called for at the discretion of the supervisor. Check for: • The condition of external cables within a loom or duct will be taken to indicate the condition of inner cables. • The condition of cables entering and leaving a conduit will be taken to indicate the condition of the cables within the conduit, unless otherwise suspect. Special precautionary checks All flight, engine, fuel and landing gear control systems: • Whenever inspections are made or work is undertaken on any part of above systems, detailed investigation must be made after completion to verify that distortion, tools, rags or any other loose articles or foreign objects cannot impede free movement and safe operation of the system(s). • Fuel systems: If, as a result of the application of this Maintenance Schedule, any part of the fuel system is dismantled, adjusted, repaired or renewed, affected parts of the system shall be checked for free movement and correct operation after completion of the work. Panel opening charts • Panel opening charts provide panel identification. • For the purpose of physical inspection, panel removal requirements shall not limit the degree of inspection required. Removal of other panels shall be at the discretion of inspection personnel.

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2.11 Task Codes E1 EXAMINATION 1 GENERAL VISUAL examination of the exposed structure or systems accomplished from the ground or from inside the control cabin, passenger cabin or cargo compartments. This examination does not require any access means or manual action to be performed except landing gear door opening and flap deflection, if required. E2 EXAMINATION 2 VISUAL examination using access means: it may require, for example, the use of stands, docks, "snorkel" crane, and if necessary, opening of specific panels. A mirror and/or suitable light may be necessary to ensure visual access to all surfaces. For cables, check for broken wire and corrosion. E3 EXAMINATION 3 THOROUGH/DETAILED VISUAL examination which may necessitate the use of access means, access door opening, and removal of fairings, linings, etc. and any other action to be performed in order to clear the inspection area. Visual thorough/detailed examination is including all usual normal work as required to check for proper attachment, play, loosening, interference, etc. Inspection aids such as mirrors, magnifying lenses, etc. may be necessary. E4 EXAMINATION 4 SPECIAL DETAILED examination using the following techniques: • Ultrasonic • Radiographic • Low Frequency Eddy Current • High Frequency Eddy Current • Dye penetrant • Resonance (by tapping). This method, used for detecting any panel bond separation, consists in slightly tapping the surface of bonded sheet metal and honeycomb panels, at spots approximately 10 cm apart. • Magnifying glass These various inspection methods are defined in specific documents. The use of any of these methods has to be clearly stated. S SERVICING This task can involve one of the following actions: a) Regular lubricant using grease, gun-squirt-can, brush or spray Date: 23-Jul-2008

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b) Fluid level check with refilling to proper level as required c) Cleaning d) Periodical software update (e.g. FMS data-base). F1 OPERATIONAL CHECK (OP/C) A qualitative check to determine that a system or component is operating in a normal or intended manner. Does not require quantitative tolerances. F2 FUNCTIONAL CHECK (F/C) A quantitative check to determine if one or more functions of a system or component perform within specified limits. M1 MEASUREMENT WITHOUT RECORDING Is a measurement of play, travel, torque, pressure level, cable tension, etc... to ensure that an item is within tolerance. M2 MEASUREMENT WITH RECORDING As above but actual figures shall be noted and entered into the record book or cards. W1 EXAMINATION OF WIRING AND COAXIAL-CABLES Check external condition or wire bundles, coaxial cables and attachments for physical condition, cleanliness, proper appearance (aging, weathering, overheating, chafing, distortion possible detrimental to characteristics), without systemically opening out harness or bundles. W2 THOROUGH EXAMINATION OF WIRING AND COAXIAL CABLES In addition to the above outlined inspection open all access doors and remove all readily detachable panels, shields or system units concealing wire bundles and coaxial cables. Check identification sleeves or tags, coatings, padding and protective devices. Wire bundles and coaxial cables concealed by floor or lining panels, unit of structural members which cannot be removed without extensive work, are checked by sampling inspections, whose extent and intervals are specified in each case. I1 EXAMINATION OF INTERCONNECTIONS (connectors, splices, pressurized bulkhead connectors terminal strips, clamps) Externally check that connectors are clean, corrosion free, and properly tightened, safetied and locked. Checking the connection tightness does not necessarily imply the use of a tool. The check may be visual - when, for instance, index mark dots where painted on the screw head and the component body or on the bolt head and its mating nut - or manual by pressing with the finger so as to detect any looseness of terminal lugs. I2 THOROUGH EXAMINATION OF CONNECTORS Date: 23-Jul-2008

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In addition to the above outlined inspection disconnect connectors and pressurized bulkhead connectors and check physical and electrical condition, inspect for oxidation traces: replace seals, gaskets, grommets, ferrules or other parts if necessary. Check tightness of connections on all electrical system accessories, bonding and grounding jumpers, bus bars, terminal strips, check all connectors not provided with safety wires. R1 EXAMINATION OF RACKS, SUPPORTING FRAMES AND SHELVES Without removing any system units, externally check that wire bundles, connectors, extractors, ducts, attachments, shock mounts, bonding jumpers are in proper physical condition, properly tightened, safetied and locked and their aspect is satisfactory. Externally check condition of all parts exposed when- ever system units are removed for testing or replacement. R2 THOROUGH EXAMINATION OF RACKS; SUPPORTING FRAMES AND SHELVES In addition to the above outlined inspection remove all system units. Clean and blow out dust from panels, shelves, slide channels, air valve ports, seals and ventilation ducts. Safety as applicable system unit attachment upon reinstallation. Check placards and nameplates. P1 EXAMINATION OF PANELS, JUNCTION BOXES, ACCESSORIES Without removal, externally check that panels, junction boxes, accessories and system units are in physical condition, clean, properly attached and locked and their aspect is satisfactory. P2 THOROUGH EXAMINATION OF PANELS, JUNCTION BOXES AND ACCESSORIES Open panels and protective boxes and externally check physical condition cleanliness, appearance, tightness, locking and safetying of the above components. Blow out dust and clean if necessary. Check placards and nameplates. Check physical condition of fuse-holders and inspect for evidence of overheating. Check that fuses (installed and spares) are in proper condition and conformance with nominal value.

2.12 (Not used) 2.13 Parking, Storage and Return to Service 2.13.1 Parking For normal parking procedures: see AMM 10-11-01.

2.13.2 Storage For prolonged parking (storage) procedures: see AMM 10-12-02.

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737-6

2.13.3 Return to Service For the return to service procedure: see AMM 10-12-02.

2.13.4 Special Regulations for Parked or Stored Aircraft An aircraft which has been taken out of operation and is parked or stored for more than 24 hours has to be maintained according the following rules: • All maintenance requirements and checks defined in this Maintenance Schedule, which become due during the parking/storage period, may be postponed until the end of the parking period (unless required by AMM 10-00). • All deferred complaints and open items, which are scheduled for rectification during the parking period, may be postponed until the end of the parking period (unless required by AMM 10-00). • All changes of components, which become due during the parking period according the CMS, may be postponed until the end of the parking period (unless required by AMM 10-00). • ALL EO´s, SB´s, SL´s, SIL´s, AD´s, CDN´s and national Airworthiness Requirements, which become due during the parking period, may be postponed until the end of the parking period, provided there is no specific requirement for the parking/storage period. • Provisioning related component, APU or engine removals during the parking/storage period are possible in general. The reinstallation of a component, APU or engine can be postponed until the end of the parking/storage period, but has to be performed in accordance with all relevant procedures. All outstanding work and component replacements must be completed before return of the aircraft back into service. For appropriate handling of a removed component, APU or engine before installation in another aircraft, refer to the relevant procedures. • For maintenance requirements and maintenance checks which are limited in Maintenance Schedule or in the CMS with calendar time, an interval credit may be used in principle. The amount of the interval credit depends on the duration and the condition of the parking/storage and is subject to LBA-approval. • Before the aircraft is returned to service, all open defects need to be rectified, and all relevant maintenance program tasks required to return the aircraft to airworthiness standards need to be complied with.

2.14 Authority Requirements 2.14.1 Approval of Maintenance Schedule by Authority All changes to the Maintenance Schedule revising the task interval and/or the task code of an item require authority approval. Tasks from the MRB Report can be developed or escalated in compliance with para. 2.14.2 and require authority approval. The responsible national authority for approvals is the Luftfahrt Bundesamt (LBA). Date: 23-Jul-2008

INTRODUCTION

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MAINTENANCE SCHEDULE

737-6

2.14.2 Interval Escalation Procedure Generally, intervals defined in this Maintenance Schedule may be increased based on engineering judgment under consideration of operational, service or industry experience/standards. A minimum of 90% usage of the valid interval is required for escalation. MPD or MRB originated task intervals shall not be escalated more than 25% of the valid, presently applied interval. The following procedures for task escalation have to be followed : • For Line Maintenance tasks : - Qualitative assessment of findings from the existing interval. The number of tasks accomplished which will be investigated is the percentage of the intended escalation step applied to the number of aircraft in the fleet. The resulting figure is used for each task. - Request for approval by the responsible authority for use of the new interval on a trial basis. - Detailed assessment of findings from tasks accomplished under the new interval. The number of tasks which will be investigated is the percentage of the intended escalation step applied to the number of aircraft in the fleet. The resulting figure is used for each task. - Presentation of the assessment results to the responsible authority and request for final approval of the new interval. • For Base Maintenance tasks : - Detailed assessment of findings from the existing interval. - The number of tasks that will be investigated depends on fleet size and is subject to approval by the responsible authority. - Request for approval by the responsible authority for use of the new interval on a "trial" base. - Detailed assessment of findings from tasks accomplished under the new interval. - The number of tasks under trial that will be investigated depends on fleet size and is subject to approval by the responsible authority. - Presentation of the assessment results to the responsible authority and request for final approval of the new interval.

2.14.3 Permitted Variations to Task Frequencies Corrosion Prevention and Control Program ( CPCP): To accommodate unanticipated scheduling requirements, Repeat Intervals of CPCP Items may, occasionally, be increased by up to ten percent (10%), with a maximum of 6 months ( requires regulatory notification and regulatory approval in writing ).

Date: 23-Jul-2008

INTRODUCTION

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MAINTENANCE SCHEDULE

737-6

2.15 (Not used) 2.16 (Not used) 2.17 (Not used) 2.18 Maintenance Requirements for Specific Aircraft Operations 2.18.1 MNPS Maintenance Procedures In accordance with EU OPS 1.870, no scheduled maintenance tasks nor specific recommendations on MNPS involved systems/tasks are needed on B737 aircraft to hold their MNPS capability.

2.18.2 RVSM (Reduced Vertical Separation Minimum) Capability The goal of RVSM is to reduce the vertical separation above flight level 290 from the current 2000- ft minimum to 1000-ft minimum. This will allow the aircraft to safely fly more optimum profiles, gain fuel savings and increase airspace capacity. This requires that the mean altimetry system error does not exceed specified values. In accordance with Boeing Service Letter 737-SL-02-017-G all required scheduled maintenance tasks are defined in the Boeing B737-6/7/8/9 MPD.

2.18.3 CAT II / CAT III Operation Specific Maintenance Tasks for Automatic Approach and Landing CAT II / CAT III Operation should be reflected in the Maintenance Schedule if applicable. On all Boeing B737-700 aircraft CAT II / CAT III are inherent functions of the basic aircraft design standard. Therefore related tasks are covered by the respective Maintenance Program without special recommendation for scheduled Maintenance Tasks. Consequently all Boeing B737-700 do not require scheduled periodic tests / functional checks / calibrations to assure CAT II / CAT III certification. However, HHI will comply with supplemental national requirements if applicable.

Date: 23-Jul-2008

INTRODUCTION

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3

FORMAT LAYOUT DESCRIPTION AND DEFINITION OF TERMS

3.1

Revision Column

737-6

A letter code gives the status of the item at the date of publication shown in the page header: "N" : New "R" : Revised "D" : Deleted Blank : No change

3.2

ITEM Column

It lists in numerical sequence for each separate ATA 100 chapter and subchapter, all the items leading to a periodic maintenance or overhaul task. The item number is split into three figures groups: • group 1 : 6 digits giving the ATA Spec. 100 reference, • group 2 : 3 digits giving a sequence number (all sequence numbers from 001 to 999 can be used) • group 3 : 2 digits giving a "sub-sequence" number allowing grouping of items of same nature, but applying with different parameters. If only one item is used, this sequence number is "00". In principle each item corresponds to one task (which may cover several "tasks codes") and one interval (and possibly one threshold). If several intervals do appear, they are always in different units (FLH, CYC,...) and in that case the meaning of such a situation is: to apply the interval "what ever comes first".

Date: 23-Jul-2008

INTRODUCTION

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3.3

737-6

DESCRIPTION Column

It gives a brief but accurate description of the task to be accomplished. In addition in that column may appear some notes when necessary. These notes are of 3 categories: Note: General notes affecting some of the parameters produced in the layout (INTERVAL, TASK CODE, etc.). In any case a highlight "NOTE" appear, with, in front of it, a note mark identifying the affected parameters. These possible note marks are: • Z : zone • E : effectivity • T : threshold • I : interval • J : task code • R : reference • M : miscellaneous Access Note: Specific note when special access (other than those mentioned in ACCESS column) has to be made to perform the task (i.e.: landing gear doors closed, flaps extended ...). In that case a highlight "ACCESS" appears. Condition Note: Specific note when the task to be performed depends on the embodiment of such modifications which are then indicated in that note. In that case a highlight "CONDITION" appears.

Date: 23-Jul-2008

INTRODUCTION

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3.4

737-6

ZONE Column

Shows the zones concerned with the task, using the Boeing zone system for the B737-700 aircraft.

3.5

ACCESS Column

It lists all the access panels, corresponding to each zone of the ZONE column, to be opened to perform the task.

3.6

STRUCTURE Column

If applicable, shows the sampling fraction corresponding to that portion of the operators fleet which must be inspected (see Sampling Inspections for details).

Date: 23-Jul-2008

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3.7

737-6

REFERENCES Column

It shows each document or manual necessary to be consulted to produce a clear understanding of the requested task, as well as references covering the origin of the item. For items which are affected by Directive from Airworthiness Authorities, the letter's reference will be mentioned in this column, and the maximum allowable limit shown in a NOTE preceded by the note mark "I" (for interval). Such references are indicated by means of their alphabetical code and their number. Examples of references types: Indicates an Airworthiness Requirement • AAR (FAA) Airworthiness Directive • AD Aircraft Maintenance Manual • AMM Aircraft Maintenance Task Oriented Support System • AMTOSS Corrosion Prevention and Control Program • CPCP Maintenance Planning Document • MPD Task of the Maintenance Review Board Report • MRB MS item number related to this task • MS Non-Destructive Testing Manual • NTM Service Bulletin • SB Structural Significant Item of the MRB • SSI Service Information. Indicates if source of task is experience of Lufthansa Technik (LHT) or a customer request. • SI Standard Practices Manual • SPM

Date: 23-Jul-2008

INTRODUCTION

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3.8

737-6

THRESHOLD/INTERVAL Column

It shows the maximum allowed interval for each task to be performed. This interval is preceded by the letter "I:". Should the task become effective only after expiration of a certain limit, this limit appears (as a THRESHOLD) preceded by the letter "T:". The units in which intervals/ thresholds are expressed are as follows: • • • • • •

FLH CYC MTH YRS T Z

3.9

flight hours flight cycles months years trip check (preflight) daily additional items

TASK Column

The task code indicated in this column gives a more extensive definition of the task than that described in the column "DESCRIPTION". In the coding layout it has been considered that: − the access and degree of disassembly (if required) should be stated in the columns "ACCESS" and "DESCRIPTION", the object to be examined must be cleaned if the normal degree of operation contamination is exceeded and a perfect check of performance is not ensured.

3.10 EFFECTIVITY Column It describes the Aircraft model, or Engine type, or specific individual a/c to which the concerned task applies. "ALL" appears when the task applies to all aircraft

3.11 BY Column The indication FC (flight crew) or SM (station mechanic) appears each time the specific task is of "line maintenance" nature, neither "T" or "Z" checks.

Date: 23-Jul-2008

INTRODUCTION

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737-6

3.12 REP Column Information for Lufthansa Technik internal purposes only.

3.13 LEV Column It shows, for each time, the revision level of this item (00 for the first issue, 01 to 99 for revisions).

3.14 ITEM REVISION DATE Column Shows, for each item, the latest revision date. This date is always lower or equal to the date of revision of the whole Maintenance

Date: 23-Jul-2008

INTRODUCTION

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4

WEIGHING

4.1

Weighing Periods

737-6

A. Each aircraft will be weighed and the C of G location established prior to being placed into service. New production aircraft delivered to operators and weighed by the manufacturer are eligible to be placed into operations without re weighing if only minor change and equipment installation are accomplished by the operator. B. Each aircraft will be weighed at overhaul. C. Each aircraft will be weighed after major repair or after major alteration unless reliable data allowing analytical calculation of weight and balance change are available. D. Every 4 years each aircraft within a fleet have to be weighed to allow correct assessment of the weight and C.G. position variation. E. The aircraft weighing schedule is published in Chapter 5.

4.2

Weighing Procedure

The weighing procedure will be carried out according to AMM 08-12-00.

4.3

Weighing Results

Before each weighing, the responsible weight and balance engineer or a qualified delegate, who must be familiar with the equipment of the aircraft will check the condition of the aircraft at the time of weighing against a standard equipment list. This standard equipment list must represent the actual condition of the aircraft in service. The responsible weight and balance engineer or qualified delegate carries out the weighing and reports the weighing results by documents as follows : One weighing record and a completed standard equipment list acc. to the actual configuration of the aircraft at time of weighing.

Date: 23-Jul-2008

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5

737-6

AIRCRAFT

Aircraft Basic Data Table REGIST NEW D-AHIA

CUST ID HHI

D-AHIB D-AHIC

SERIES B737-73S

CON FIG PAX

ENGINE TYPE CFM56-7B22

APU TYPE 131-9(B)

HHI

B737-73S

PAX

CFM56-7B22

HHI

B737-7BK

PAX

CFM56-7B22

D-AHID

HHI

B737-73S

PAX

D-AHIE

HHI

B737-73S

D-AHIF

HHI

B737-73S

IPC EFF

LINE NO 229

PROD. NO YA 577

SERIAL NO 29082

131-9(B)

392

YA 578

131-9(B)

812

YB 276

CFM56-7B22

131-9(B)

211

PAX

CFM56-7B24

131-9(B)

PAX

CFM56-7B24

131-9(B)

AIR FRAME

DATE OF FIRST FLIGHT 05-mar-1999

REGIST OLD D-ASKH

REMARKS

29083

01-oct-1999

D-AWOH

30617

23-mar-2001

N/A

YA575

29080

04-feb-1999

EI-CRQ

Phased out

215

YA576

29081

01-mar-1999

TC-SUF

Phased out

194

YA574

29079

17-jan-1999

TC-SUE

Phased out

Phased out

Aircraft Additional Data Table

REGIST NEW D-AHIA

NEXT WEIGHING 16-Feb-2011

SAMPLING A/C NO

ETOPS A/C NO

REMARKS Last weighing date 16-Feb-2007

D-AHIB

07-mar-2011

NO

NO

Last weighing date 07-Mar-2007

D-AHIC

22-feb-2009

NO

NO

Last weighing date 22-feb-2005

D-AHID

10-Mar-2011

NO

NO

Last weighing date 10-Mar-2007

D-AHIE

23-Dec-2010

NO

NO

Last weighing date 23-Dec -2006

D-AHIF

26-Mar-2011

NO

NO

Last weighing date 26-Mar-2007

Date: 23-Jul-2008

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PARA

NATIONAL SPECIAL REQUIREMENTS

Comment

EASA PART M.A.710 EASA PART M.A.901 NfL II-23/03

CONTINUING AIRWORTHINESS REVIEW

CAMOE 6.2 – 6.7

LEAK TEST OF STBY ALTITUDE AND STBY AIRSPEED SYSTEM

acc. MS- and CMS -Items ATA 34

SEAT BELTS

see MS-Item 250000 01000

737-6

NfL II-56/01 NfL II-83/99 NfL II-96/79 NfL II-92/99 NfL II-56/01 NfL II-56/01 EASA-OPS 1.700-1.725

PORTABLE FIRE EXTINGUISHER

see MS-Item 260000 01000 and 262500 01000

FLEXIBLE HOSES 2.3.7 FLIGHT DATA RECORDER AND COCKPIT VOICE RECORDER

NfL II-56/01

2.3.6

EASA-OPS 1.870

2.3.9 MNPS (Minimum Navigation Performance Specification Airspace) Maintenance Procedures 2.3.10 CAT II/III Maintenance Procedure

Vendor Rec. see MS 237100 73000 see MS 313100 97000 Functional Check of “FLIGHT DATA RECORDER” and VOICE RECORDER SYSTEM” must be performed according to NfL II-56/01 every 12 MTH (with exception of 24 MTHS for SSFDR) STANDBY COMPASS COMPENSATION must be performed according to NfL II-56/01every 12 MTH. see MS-Item 342400 02000 N/A

EASA-OPS 1.460 OR 3.460 EASA-OPS 1.872

Date: 23-Jul-2008

COMPENSATION OF MAGNETIC STBY COMPASS

2.3.11 RVSM Maintenance Procedure

CAMOE 2.26 See MS Items 05230 00000, 341102 20000 and 530900 12000

NATIONAL AND INTERNATIONAL SPECIAL REQUIREMENTS

Page: 1 of 1


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MAINTENANCE SCHEDULE

737-700 Major Zones

Description / Boundaries

100

LOWER HALF OF FUSELAGE

200

UPPER HALF OF FUSELAGE

300

EMPENNAGE AND BODY SECTION 48

400

POWER PLANTS AND NACELLE STRUTS

500

LEFT WING

600

RIGHT WING

700

LANDING GEAR AND LANDING GEAR DOORS

800

PASSENGER AND CARGO DOORS

800*

ONLY ON 737-800/900

800**

737-700 ONLY

MAJOR AIRCRAFT ZONES

Date: 23-jul-08

AIRCRAFT ZONES

Page: 1 Z


HHI

MAINTENANCE SCHEDULE

737-700

MAJOR ZONE 100 - LOWER HALF OF FUSELAGE

Date: 23-jul-08

AIRCRAFT ZONES

Page: 2 Z


MAINTENANCE SCHEDULE

HHI Major Zones

Description / Boundaries

Major Zones

110

STA 130 TO STA 360

111

RADOM

141/142

AFT CARGO COMPARTMENT

112

AREA FWD OF NOSE WHEEL WELL

143/144

AREA BELOW AFT CARGO COMPARTMENT

113/114

AREA ABOVE NOSE WHEEL WELL AREA OUTBD OF NOSE WHEEL WELL

145/146

AFT CARGO COMPARTMENT EQUIPMENT BAY

115/116

NOSE WHEEL WELL

117/118

ELECTRICAL AND ELECTRONICS COMPARTMENT

120

140

Description / Boundaries

Description / Boundaries

Major Zones

Description / Boundaries

BODY STA 727 TO STA 1016

149

KEEL BEAM (PART) STA 727 TO STA 743.95

190

FAIRING BODY STA 500B+15 TO STA 727D+8

191

LOWER WING, WING TO BODY FAIRING FWD OF WING BOX

BODY STA 360 TO STA 540

121/122

FWD CARGO COMPARTMENT

123/124

AREA BELOW FWD CARGO COMPARTMENT

192

LOWER WING, WING TO BODY FAIRING UNDER WING BOX

125/126

AIR CONDITIONING DISTRIBUTION BAY

193

LOWER WING, WING TO BODY FAIRING WHEEL WELL

129

KEEL BEAM (PART) STA 501.70 TO STA 540

194

LOWER WING, WING TO BODY FAIRING AFT OF WHEEL WELL

195 130

BODY STA 540 TO STA 727

ABOVE RIGHT WING, WING TO BODY FAIRING

196

ABOVE LEFT WING, WING TO BODY FAIRING

131/132

CENTER SECTION WING BOX (STA540 TO STA 663.75)

133/134

MAIN LANDING GEAR WELL (STA 633.75 TO STA 727)

135/136

AREA ABOVE WING CENTER SECTION (STA 540 TO STA 663.75)

137/138

AREA ABOVE MAIN LANDING GEAR WELL (STA 633.75 TO STA 727)

139

Major Zones

737-700

KEEL BEAM (PART) STA 540 TO STA 727

Date: 23-jul-08

AIRCRAFT ZONES

Page: 3 Z


HHI

MAINTENANCE SCHEDULE

737-700 Major Zones 210 211/212 220 221/222

230 231/232 240 241/242

Description / Boundaries FLIGHT COMPARTMENT BODY STA 178 TO STA 259.2 FLIGHT COMPARTMENT PASSENGER COMPARTMENT BODY STA 259.5 TO STA 360 PASSENGER COMPARTMENT - AFT OF CONTROL COMPARTMENT TO FWD ENTRY DOOR PASSENGER COMPARTMENT BODY STA 360 TO STA 663.75 FWD PASSENGER COMPARTMENT FWD ENTRY DOOR TO STA 663.75 PASSENGER COMPARTMENT AFT PASSENGER COMPARTMENT STA 633.75 TO AFT PRESSURE BULKHEAD

MAJOR ZONE 200 - UPPER HALF OF FUSELAGE

Date: 23-jul-08

AIRCRAFT ZONES

Page: 4 Z


HHI

MAINTENANCE SCHEDULE

737-700 Major Zones 310

Description / Boundaries FUSELAGE STA 1016 TO STA 1217

311/312

AREA AFT OF PRESSURE BULKHEAD

313/314

STABILIZER TORSION BOX COMPARTMENT

315/316

APU COMPARTMENT

317/318

TAIL CONE

320

FIN AND RUDDER

321

DORSAL FIN

322

FIN REMOVABLE LEADING EDGE

323

FIN FRONT SPAR TO REAR SPAR

324

FIN REAR SPAR TO TRAILING EDGE

325

RUDDER

326

FIN TIP

MAJOR ZONE 300 - FUSELAGE 310 - FIN AND RUDDER 320

Date: 23-jul-08

AIRCRAFT ZONES

Page: 5 Z


HHI

MAINTENANCE SCHEDULE

737-700 Major Zones

Description / Boundaries

330

HORIZONTAL STABILIZER AND ELEVATOR LEFT

331

REMOVABLE LEADING EDGE

332

FRONT SPAR TO REAR SPAR, STAB. STA 57.93 TO STAB. BL 249.81

333

REAR SPAR TO TRAILING EDGE

334

ELEVATOR

335

TIP

340

HORIZONTAL STABILIZER AND ELEVATOR RIGHT

341

REMOVABLE LEADING EDGE

342

FRONT SPAR TO REAR SPAR, STAB. STA 57.93 TO STAB. BL 249.81

343

REAR SPAR TO TRAILING EDGE

344

ELEVATOR

345

TIP

MAJOR ZONE 300 - HORIZONTAL STABILIZER

Date: 23-jul-08

AIRCRAFT ZONES

Page: 6 Z


HHI

MAINTENANCE SCHEDULE

737-700 Major Zones

Description / Boundaries

410

NO.1 POWER PLANT

411

ENGINE

412

NOSE INLET COWL

413

FAN COWL - LEFT

414

FAN COWL - RIGHT

415

THRUST REVERSER - LEFT

416

THRUST REVERSER - RIGHT

417

PRIMARY EXHAUST NOZZLE AND PLUG

420

NO.2 POWER PLANT

421

ENGINE

422

NOSE INLET COWL

423

FAN COWL - LEFT

424

FAN COWL - RIGHT

425

THRUST REVERSER - LEFT

426

THRUST REVERSER - RIGHT

427

PRIMARY EXHAUST NOZZLE AND PLUG

430/440

LEFT/RIGHT NACELLE STRUT

431/441

FORWDRD STRUT FAIRING

432/442

FAN COWL SUPPORT BEAM

433/443

STRUT TORQUE BOX

434/444

AFT STRUT FAIRING

MAJOR ZONE 400 - CFM56-7 POWERPLANT AND NACELLE

Date: 23-jul-08

AIRCRAFT ZONES

Page: 7 Z


HHI

MAINTENANCE SCHEDULE

737-700

MAJOR ZONE 500 - LEFT WING (SHOWN), MAJOR ZONE 600 - RIGHT WING (OPPOSITE)

Date: 23-jul-08

AIRCRAFT ZONES

Page: 8 Z


MAINTENANCE SCHEDULE

HHI Major Zones 510/610

Description / Boundaries WING LEADING EDGE - FORWARD OF FRONT SPAR, INBOARD OF NACELLE STRUT, INCLUDING NACELLE GAB COVER AREA

511/611

LEADING EDGE TO FRONT SPAR

512/612

KRUEGER FLAP NO. 2 AND NO. 3

513/613 520/620

Major Zones

Description / Boundaries

Major Zones

Description / Boundaries

540/640

WING TRAILING EDGE FLAP TRACK FAIRINGS

570/670

WING TRAILING EDGE - OUTBOARD OF OUTBOARD FLAP, INBOARD OF WING TIP, WING BL 658. 17

541/641

FAIRING FLAP SUPPORT NO. 4 AND NO. 5

571/671

FIXED TRAILING EDGE

572/672

AILERON

542/642

FAIRING FLAP SUPPORT NO. 3 AND NO. 6

KRUEGER FLAP NO. 1 AND NO. 4

543/643

FAIRING FLAP SUPPORT NO. 2 AND NO. 7

WING LEADING EDGE - FORWARD OF FRONT SPAR, OUTBOARD OF NACELLE STRUT

544/644

FAIRING FLAP SUPPORT NO. 1 AND NO. 8

521/621

LEADING EDGE TO FRONT SPAR

550/560

522/622

SLATS NO. 4 AND NO. 5

WING TRAILING EDGE - AFT OF REAR SPAR, INBOARD OF OUTBOARD TRAILING EDGE FLAP

523/623

SLATS NO. 3 AND NO. 6

551/651

REAR SPAR TO LANDING GEAR SUPPORT BEAM

524/624

SLATS NO. 2 AND NO. 7

552/652

SPOILER NO. 6 AND NO. 7

525/625

SLATS NO. 1 AND NO. 8

553/653

INBOARD FLAP

526/626

WING TIP

560/660

530/630

WING INSPAR AREA (FUEL TANKS) INBOARD OF WING RIB 22, WING STA 643.50

WING TRAILING EDGE - AFT OF REAR SPAR, OUTBOARD OF INBOARD FLAP, INBOARD OF FIXED TRAILING EDGE

531/631

CENTER FUEL TANK RIB 1 TO RIB 5

561/661

532/632

MAIN TANK, RIB 5 TO RIB 25, WING STA 204.25 TO WING STA 643.50

REAR SPAR TO TRAILING EDGE, OUTBOARD OF INBOARD FLAP, INBOARD OF FIXED TRAILING EDGE

562/662

SPOILER NO. 5 AND NO. 8

533/633

SURGE TANK, RIB 22 TO RIB 25, WING STA 616.75 TO WING BL 643. 50

563/663

SPOILER NO. 4 AND NO. 9

564/664

SPOILER NO. 3 AND NO. 10

534/634

DRY BAY

565/665

SPOILER NO. 2 AND NO. 11

566/666

SPOILER NO. 1 AND NO. 12

567/667

OUTBOARD FLAP

Date: 23-jul-08

AIRCRAFT ZONES

737-700 Major Zones

Description / Boundaries

Page: 9 Z


HHI

MAINTENANCE SCHEDULE

737-700 Major Zones

Description / Boundaries

710

NOSE LANDING GEAR AND L. G. DOORS

711

NOSE LANDING GEAR DOOR, LEFT

712

NOSE LANDING GEAR DOOR, RIGHT

713

NOSE LANDING GEAR

730

LEFT MAIN LANDING GEAR AND L. G. DOORS

731

OUTBOARD DOOR, LEFT

732

CENTER DOOR, LEFT

733

INBOARD DOOR, LEFT

734

LEFT MAIN LANDING GEAR

740

RIGHT MAIN LANDING GEAR AND L. G. DOORS

741

OUTBOARD DOOR, RIGHT

742

CENTER DOOR, RIGHT

743

INBOARD DOOR, RIGHT

744

RIGHT MAIN LANDING GEAR

MAJOR ZONE 700 - LANDING GEAR AND LANDING GEAR DOORS

Date: 23-jul-08

AIRCRAFT ZONES

Page: 10 Z


HHI

MAINTENANCE SCHEDULE

737-700 Major Zones

Description / Boundaries

820

LOWER HALF OF FUSELAGE RIGHT SIDE

821

FORWARD CARGO DOOR

822

AFT CARGO DOOR

830

UPPER HALF OF FUSELAGE LEFT SIDE

831

FORWARD ENTRY DOOR

832

AUTOMATIC OVERWING EXIT (-800/900)

833

AUTOMATIC OVERWING EXIT

834

AFT ENTRY DOOR

835

MAIN DECK CARGO DOOR (-700C ONLY)

840

UPPER HALF OF FUSELAGE RIGHT SIDE

841

FORWARD ENTRY DOOR

842

AUTOMATIC OVERWING EXIT (-800/900)

843

AUTOMATIC OVERWING EXIT

844

AFT ENTRY DOOR

MAJOR ZONE 800 - PASSENGER AND CARGO DOORS

Date: 23-jul-08

AIRCRAFT ZONES

Page: 11 Y


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 05 05 - 10

05100- 00000

05100- 01000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

ZONAL ZONE 100 FUSELAGE -LOWER HALFVISUALLY INSPECT LOWER HALF OF FUSELAGE E X T E R N A L

100

GENERAL VISUAL INSPECTION OF THE LOWER FUSELAGE. THE NLG WHEEL WELL AND MLG WHEEL WELL ARE ALSO INCLUDED. E X T E R N A L NOTE( J ) INSPECTION FROM GROUND WITHOUT THE USE OF STANDS OR LADDERS

110 120 130 140

emp

empty

SERVICE EXPERIENCE emp emp emp emp

ITEMS

MPD MRB

I: 1 T

E1 HHI 737-700

I: 560 CYC I: 90 DAY

E2 HHI 737-700

FC SM

1 03-jun-04

53-800-00 MSI 53-800-00

ATA: 05 - 10

5 22-mar-07

Page 1 of 1


HHI R E V

ITEM 05 - 11 05110- 00000

05110- 01000

05110- 02000

R

737-6

MAINTENANCE SCHEDULE

05111- 00000

R

05112- 00000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

BODY STA 130 TO STA 360 GENERAL VISUAL INSPECTION OF THE AREA ABOVE AND OUTBOARD OF 113 THE NOSE WHEEL WELL. emp I N T E R N A L emp 114 emp emp

113AC 113AW 113BW 114AC 114AW 114BW

MPD MRB

GENERAL VISUAL INSPECTION OF THE ELECTRICAL AND ELECTRONICS 117 COMPARTMENT. emp I N T E R N A L 118 ACCESS FORWARD AIRSTAIR DRIP PAN ACCESS PANEL MUST BE REMOVED IF AIRSTAIR INSTALLED. ACCESS PANEL 117BL ONLY AT A/C WITH AIRSTAIR INSTALLED OR PROVISIONS.

117A 117BL emp

MPD MRB

GENERAL VISUAL INSPECTION OF THE ELECTRICAL AND ELECTRONICS 117 COMPARTMENT ACCESS DOOR. 118 I N T E R N A L

117AW emp

MPD MRB

GENERAL VISUAL INSPECTION OF THE RADOME I N T E R N A L NOTE( Z ) ZONE 111 INTERNAL INSPECTION INCLUDES THE BS 178 STRUCTURE AND INSTALLATIONS AND THE INTERNAL SIDE OF THE RADOME.

111

111

GENERAL VISUAL INSPECTION OF THE AREA FORWARD OF THE NOSE 112 WHEEL WELL - SECTION 41, STA 178 TO 224.8. I N T E R N A L

112A

ITEMS

MPD MRB

MPD MRB

53-806-00 MSI 53-806-00 I: 24 MTH I: 5500 CYC

E2 HHI 737-700

2 03-jun-04

I: 5500 CYC I: 24 MTH

E2 HHI 737-700

3 03-jun-04

I: 5500 CYC I: 24 MTH

E2 HHI 737-700

2 03-jun-04

I: 24 MTH I: 5500 CYC

E2 HHI 737-700

3 23-jul-08

I: 5500 CYC I: 24 MTH

E2 HHI 737-700

2 03-jun-04

53-808-00 MSI 53-808-00

53-810-00 MSI 53-810-00

53-802-00 MSI 53-802-00

53-804-00 MSI 53-804-00

ATA: 05 - 11

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 05 - 12

05120- 00000

05120- 01000

05120- 02000

05120- 03000

05120- 04000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

BODY STA 360 TO STA 540 GENERAL VISUAL INSPECTION OF THE FORWARD CARGO COMPARTMENT 121 - SECTION 43, STA 396 TO FWD CARGO COMPARTMENT AFT BULKHEAD. 122 I N T E R N A L ACCESS NO CARGO LINERS REMOVED.

821 emp

GENERAL VISUAL INSPECTION OF THE AIR CONDITIONING DISTRIBUTION 125 BAY - SECTION 43, FWD CARGO COMPARTMENT BULKHEAD TO STA 540. 126 I N T E R N A L ACCESS FORWARD CARGO COMPARTMENT AFT BULKHEAD CENTER PANEL REMOVAL REQUIRED.

821 emp

GENERAL VISUAL INSPECTION OF THE AREA ABOVE THE FORWARD CARGO COMPARTMENT - SECTION 43, STA 396 TO FWD CARGO COMPARTMENT AFT BULKHEAD I N T E R N A L ACCESS CEILING PANELS REMOVAL REQUIRED

821 emp

121 122

GENERAL VISUAL INSPECTION OF THE AREA BELOW THE FORWARD 123 CARGO COMPARTMENT - SECTION 43, STA 396 TO FWD CARGO 124 COMPARTMENT BULKHEAD I N T E R N A L ACCESS CENTER FLOOR PANELS REMOVAL REQUIRED. INSULATION BLANKETS REMOVED OR DISPLACED.

821 emp

GENERAL VISUAL INSPECTION OF THE FORWARD CARGO COMPARTMENT 121 - SECTION 43, STA 396 TO FWD CARGO COMPARTMENT AFT BULKHEAD 122 I N T E R N A L ACCESS SIDEWALL PANELS REMOVAL REQUIRED. INSULATION BLANKETS REMOVED OR DISPLACED.

821 emp

ITEMS

MPD MRB

MPD MRB

MPD MRB

MPD MRB

MPD MRB

53-812-00 MSI 53-812-00 I: 560 CYC I: 90 DAY

E2 HHI 737-700

6 22-mar-07

I: 5500 CYC I: 24 MTH

E2 HHI 737-700

5 18-mar-05

I: 13000 CYC I: 60 MTH

E2 HHI 737-700

3 18-mar-05

I: 13000 CYC I: 60 MTH

E2 HHI 737-700

3 18-mar-05

I: 36000 CYC I: 12 YRS

E2 HHI 737-700

2 03-jun-04

53-822-00 MSI 53-822-00

53-814-00 MSI 53-814-00

53-820-00 MSI 53-820-00

53-816-00 MSI 53-816-00

ATA: 05 - 12

Page 1 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

05122- 00000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

GENERAL VISUAL INSPECTION OF THE FORWARD CARGO DOOR 122 SURROUND STRUCTURE FITTINGS AND STOPS - SECTION 43, STA 460. E X T E R N A L

STRUCTURE

821

REFERENCES MPD MRB

THRESHOLD INTERVAL

EFF

R L ITEM BY E E REVISION P V DATE

53-818-00 MSI 53-818-00 I: 1500 CYC I: 180 DAY

ITEMS

TSK

ATA: 05 - 12

E2 HHI 737-700

5 22-mar-07

Page 2 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 05 - 13

05130- 00000

05130- 01000

05130- 02000

05139- 00000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

BODY STA 540 TO STA 727 GENERAL VISUAL INSPECTION OF THE PRESSURE DECK ABOVE THE 137 MAIN LANDING GEAR WHEEL WELL - SECTION 44, STA 663.75 TO STA 727. 138 I N T E R N A L ACCESS FLOOR PANELS REMOVAL REQUIRED. INSULATION AS REQUIRED.

emp emp

GENERAL VISUAL INSPECTION OF THE CENTER SECTION WING BOX SECTION 44, STA 540 TO STA 663.75. I N T E R N A L

131 132

131AB 192CL

GENERAL VISUAL INSPECTION OF THE AREA ABOVE THE CENTER SECTION WING BOX - SECTION 44, STA 540 TO 663.75. I N T E R N A L ACCESS FLOOR PANELS REMOVAL REQUIRED. INSULATION AS REQUIRED.

135 136

GENERAL VISUAL INSPECTION OF THE KEEL BEAM (PART) - SECTION 44, 139 STA 540 TO 727. emp I N T E R N A L

emp emp

192CL 192CR

ITEMS

MPD MRB

MPD MRB

MPD MRB

MPD MRB

53-826-00 MSI 53-826-00 I: 13000 CYC I: 60 MTH

E2 HHI 737-700

2 18-mar-05

I: 36000 CYC I: 10 YRS

E2 HHI 737-700

2 18-mar-05

I: 36000 CYC I: 12 YRS

E2 HHI 737-700

2 03-jun-04

I: 4800 CYC I: 24 MTH

E2 HHI 737-700

2 22-mar-07

57-800-00 MSI 57-800-00

53-824-01 MSI 53-824-01

53-828-00 MSI 53-828-00

ATA: 05 - 13

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 05 - 14

05141- 00000

05141- 01000

05141- 02000

05141- 03000

05142- 00000

05143- 00000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

BODY STA 727 TO 1016 GENERAL VISUAL INSPECTION OF THE AFT CARGO COMPARTMENT SECTION 46 AND 47 (PART), STA 727 TO STA 947.5. ACCESS NO CARGO LINERS REMOVED.

141 142

GENERAL VISUAL INSPECTION OF THE AFT CARGO COMPARTMENT VACUUM WASTE COMPARTMENT I N T E R N A L ACCESS VACUUM WASTE COMPARTMENT PANELS REMOVAL REQUIRED

141

822 emp

822

GENERAL VISUAL INSPECTION OF THE AFT CARGO COMPARTMENT - 141 SECTION 46 AND 47 (PART), STA 727 TO STA 947.5 142 I N T E R N A L ACCESS UPPER ANGLED SIDEWALL AND CEILING PANELS REMOVAL REQUIRED

822 emp

GENERAL VISUAL INSPECTION OF THE AFT CARGO COMPARTMENT SECTION 46 AND 47 (PART), STA 727 TO STA 947.5 I N T E R N A L ACCESS SIDEWALL PANELS REMOVAL REQUIRED. INSULATION BLANKETS REMOVED OR DISPLACED.

822 emp

141 142

GENERAL VISUAL INSPECTION OF THE AFT CARGO DOOR SURROUND 142 STRUCTURE FITTINGS AND STOPS -SECTION 46, STA 827. E X T E R N A L

822

GENERAL VISUAL INSPECTION OF THE AREA BELOW THE AFT CARGO 143 COMPARTMENT - SECTION 46 AND 47 (PART), STA 727 TO STA 947.5. 144 I N T E R N A L ACCESS CENTER FLOOR PANELS REMOVAL REQUIRED. INSULATION BLANKETS REMOVED OR DISPLACED.

emp 822

ITEMS

MPD MRB

MPD MRB

MPD MRB

MPD MRB

MPD MRB

MPD MRB

53-830-00 MSI 53-830-00 I: 560 CYC I: 90 DAY

E2 HHI 737-700

6 22-mar-07

I: 24 MTH I: 5500 CYC

E2 HHI 737-700

2 03-jun-04

I: 13000 CYC I: 60 MTH

E2 HHI 737-700

2 18-mar-05

I: 36000 CYC I: 12 YRS

E2 HHI 737-700

2 18-mar-05

I: 1500 CYC I: 180 DAY

E2 HHI 737-700

6 22-mar-07

I: 13000 CYC I: 60 MTH

E2 HHI 737-700

2 18-mar-05

53-838-00 MSI 53-838-00

53-832-00 MSI 53-832-00

53-834-00 MSI 53-834-00

53-836-00 MSI 53-836-00

53-840-00 MSI 53-840-00

ATA: 05 - 14

Page 1 of 2


HHI

737-6

MAINTENANCE SCHEDULE

R E V

ITEM

R

05145- 00000

R

Date: 23-jul-08

DESCRIPTION GENERAL VISUAL INSPECTION OF THE AFT CARGO COMPARTMENT EQUIPMENT BAY - SECTION 47, STA 947.5 TO STA 1016. I N T E R N A L ACCESS AFT CARGO PANELS AT 947 BULKHEAD REMOVAL REQUIRED

ZONE ACCESS 145 146

STRUCTURE

822 emp

ITEMS

REFERENCES MPD MRB MPD MRB

53-842-00 MSI 53-842-00 53-842-00 MSI 53-842-00

AMM

05-41-01-210

THRESHOLD INTERVAL

I: 5500 CYC I: 24 MTH

ATA: 05 - 14

TSK

EFF

E2 HHI 737-700

R L ITEM BY E E REVISION P V DATE

4 23-jul-08

Page 2 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 05 - 19

05190- 00000

05191- 00000

05192- 00000

05194- 00000

05194- 01000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

WING TO BODY FAIRINGS GENERAL VISUAL INSPECTION OF THE WING TO BODY FAIRING. 190 E X T E R N A L NOTE( J ) INSPECTION FROM GROUND WITHOUT THE USE OF STANDS OR LADDERS

emp

GENERAL VISUAL INSPECTION OF THE LOWER WING TO BODY FAIRING - FORWARD OF WING BOX. I N T E R N A L ACCESS THROUGH ACCESS PROVIDED

191 emp emp emp

191GL 191GR 192CL 192CR

MPD MRB

GENERAL VISUAL INSPECTION OF THE LOWER WING TO BODY FAIRING - UNDER THE WING BOX. I N T E R N A L ACCESS THROUGH ACCESS PROVIDED

192 emp emp emp emp

192BL 192BR 192CL 192CR 192DR

MPD MRB

GENERAL VISUAL INSPECTION OF THE LOWER WING TO BODY FAIRING 194 - AFT OF WHEEL WELL. I N T E R N A L ACCESS THROUGH ACCESS PROVIDED

194DR

MPD MRB

GENERAL VISUAL INSPECTION OF THE LOWER WING TO BODY FAIRING 194 - AFT OF WHEEL WELL. emp I N T E R N A L emp emp emp emp emp emp emp emp emp emp emp emp emp

194AL 194AR 194BL 194BR 194CL 194CR 194DL 194DR 194E 194FL 194FR 194GL 194GR 194HL 194HR

ITEMS

MPD MRB

MPD MRB

53-844-00 MSI 53-844-00 I: 560 CYC I: 90 DAY

E2 HHI 737-700

5 22-mar-07

I: 5500 CYC I: 24 MTH

E2 HHI 737-700

2 03-jun-04

I: 5500 CYC I: 24 MTH

E2 HHI 737-700

2 03-jun-04

I: 24 MTH I: 5500 CYC

E2 HHI 737-700

2 03-jun-04

I: 24000 CYC I: 8 YRS

E2 HHI 737-700

1 03-jun-04

53-846-00 MSI 53-846-00

53-848-00 MSI 53-848-00

53-852-00 MSI 53-852-00

53-850-00 MSI 53-850-00

ATA: 05 - 19

Page 1 of 2


HHI

737-6

MAINTENANCE SCHEDULE

R E V

ITEM

R

05195- 00000

R

Date: 23-jul-08

DESCRIPTION GENERAL VISUAL INSPECTION OF THE ABOVE WING, WING TO BODY FAIRING - RIGHT AND LEFT SIDE. I N T E R N A L

ZONE ACCESS 195 emp emp emp emp emp 196 emp emp emp emp emp

STRUCTURE

195AL 195AR 195BL 195BR 195CL 195CR 196AL 196AR 196BL 196BR 196CL 196CR

ITEMS

REFERENCES MPD MPD MRB MRB MPD MPD MRB MRB

53-854-02 53-856-01 MSI 53-854-02 MSI 53-856-01 53-854-02 53-856-01 MSI 53-854-01 MSI 53-856-02

AMM

05-41-01-210

THRESHOLD INTERVAL

I: 24000 CYC I: 8 YRS

ATA: 05 - 19

TSK

EFF

E2 HHI 737-700

R L ITEM BY E E REVISION P V DATE

2 23-jul-08

Page 2 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 05 - 20

05200- 00000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

FUSELAGE - UPPER HALF VISUALLY INSPECT THE UPPER HALF OF FUSELAGE AS FAR AS VISIBLE 200 FROM GROUND E X T E R N A L

emp

empty

SERVICE EXPERIENCE

ITEMS

I: 1 T

ATA: 05 - 20

E1 HHI 737-700

FC SM

1 03-jun-04

Page 1 of 1


HHI R E V

ITEM 05 - 21 05210- 00000

R

737-6

MAINTENANCE SCHEDULE

05210- 01000

R

05210- 02000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

FLIGHT COMPARTMENT BODY STA 178 TO STA 259.5 GENERAL VISUAL INSPECTION OF THE FLIGHT CONTROL COMPARTMENT 211 - SECTION 41, STA 178 TO STA 259.5. 212 E X T E R N A L

emp emp

GENERAL VISUAL INSPECTION OF THE FLIGHT CONTROL COMPARTMENT 211 - SECTION 41, STA 178 TO STA 259.5. 212 I N T E R N A L ACCESS CONTROL STAND ACCESS PANELS 211A AND 212A REMOVAL REQUIRED

211A 212A

GENERAL VISUAL INSPECTION OF THE FLIGHT CONTROL COMPARTMENT 211 - SECTION 41, STA 178 TO STA 259.5. 212 I N T E R N A L ACCESS WITH ACCESS PROVIDED. SEATS REMOVED. CONTROL STAND ACCESS PANELS, OVERHEAD AND SIDEWALL PANELS AND FLOOR PANEL REMOVAL REQUIRED

emp emp

ITEMS

MPD MRB

53-858-00 MSI 53-858-00

MPD MRB

53-860-00 MSI 53-860-00

AMM

05-41-02-210

MPD MRB

53-862-00 MSI 53-862-00

I: 5500 CYC I: 24 MTH

E2 HHI 737-700

3 03-jun-04

I: 5500 CYC I: 24 MTH

E2 HHI 737-700

4 23-jul-08

I: 36000 CYC I: 10 YRS

E2 HHI 737-700

2 03-jun-04

ATA: 05 - 21

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 05 - 22

05220- 00000

05220- 01000

05220- 02000

05221- 00000

05222- 00000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

PASSENGER COMPARTMENT BODY STA 259.5 TO STA 360 GENERAL VISUAL INSPECTION OF THE PASSENGER COMPARTMENT AFT OF THE CONTROL COMPARTMENT TO FORWARD ENTRY DOOR LEFT AND RIGHT - SECTION 41, STA 259.5 TO STA 360. E X T E R N A L

221 222

GENERAL VISUAL INSPECTION OF THE PASSENGER COMPARTMENT LEFT AND RIGHT - SECTION 41, STA 259.5 TO STA 360. I N T E R N A L

221 222

emp emp

emp emp

GENERAL VISUAL INSPECTION OF THE PASSENGER COMPARTMENT - 221 AFT OF THE CONTROL COMPARTMENT TO FORWARD ENTRY DOOR - 222 LEFT AND RIGHT - SECTION 41, STA 259.5 TO STA 360. I N T E R N A L ACCESS WITH ACCESS PROVIDED. GALLEYS AND LAVS REMOVED. FLOOR PANELS, SIDEWALL PANELS AND CEILING PANELS REMOVAL REQUIRED

emp emp

GENERAL VISUAL INSPECTION OF THE FORWARD PASSENGER ENTRY 221 DOOR STOPS, LATCHES AND HINGES -SECTION 41, STA 345. E X T E R N A L

831

GENERAL VISUAL INSPECTION OF THE FORWARD GALLEY SERVICE DOOR STOPS, LATCHES AND HINGES - SECTION 41, STA 340. E X T E R N A L

841

222

ITEMS

MPD MRB

MPD MRB

MPD MRB

MPD MRB

MPD MRB

53-864-00 MSI 53-864-00 I: 5500 CYC I: 24 MTH

E2 HHI 737-700

2 03-jun-04

I: 4800 CYC I: 24 MTH

E2 HHI 737-700

3 22-mar-07

I: 8 YRS I: 36000 CYC

E2 HHI 737-700

1 03-jun-04

I: 1500 CYC I: 180 DAY

E2 HHI 737-700

5 22-mar-07

I: 1500 CYC I: 180 DAY

E2 HHI 737-700

5 22-mar-07

53-866-00 MSI 53-866-00

53-868-00 MSI 53-868-00

53-870-00 MSI 53-870-00

53-872-00 MSI 53-872-00

ATA: 05 - 22

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 05 - 23

05230- 00000

05230- 01000

05230- 02000

05230- 03000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

PASSENGER COMPARTMENT BODY STA 360 TO STA 663.75 GENERAL VISUAL INSPECTION OF THE FORWARD PASSENGER 231 COMPARTMENT - LEFT AND RIGHT - SECTION 43 AND 44 (PART), STA 360 232 TO STA 663.75. ATTENTION TO SKIN DAMAGE AROUND CRITICAL AREODYNAMIC AREAS OF THE FUSELAGE AT A/C OPERATING WITH RVSM (PITOT AND FLUSH STATIC PROBES AREA). E X T E R N A L

emp emp

GENERAL VISUAL INSPECTION OF THE FORWARD PASSENGER 231 COMPARTMENT - LEFT AND RIGHT - SECTION 43 AND 44 (PART), STA 360 232 TO STA 663.75. I N T E R N A L

emp emp

GENERAL VISUAL INSPECTION OF THE FORWARD PASSENGER 231 COMPARTMENT - LEFT AND RIGHT - SECTION 43 AND 44 (PART), STA 360 232 TO STA 663.75 WET AREAS (WITHIN APPROXIMATELY 20 INCHES FROM GALLEY OR LAV). I N T E R N A L ACCESS GALLEYS AND LAVS REMOVED. FLOOR PANELS, SIDEWALL PANELS AND CEILING PANELS REMOVAL REQUIRED IN WET AREAS

emp emp

GENERAL VISUAL INSPECTION OF THE FORWARD PASSENGER 231 COMPARTMENT - LEFT AND RIGHT - SECTION 43 AND 44 (PART), STA 360 232 TO STA 663.75 DRY AREA (AWAY FROM DOORS, GALLEYS AND LAVS). I N T E R N A L ACCESS FLOOR PANELS, SIDEWALL PANELS AND CEILING PANELS REMOVAL REQUIRED

emp emp

ITEMS

MPD MRB

53-874-00 MSI 53-874-00

SIL

737-SL-02-017-B

MPD MRB

53-876-00 MSI 53-876-00

MPD MRB

53-878-00 MSI 53-878-00

AMM

05-41-02-210

MPD MRB

53-880-00 MSI 53-880-00

AMM

05-41-02-210

I: 5500 CYC I: 24 MTH

E2 HHI 737-700

3 03-jun-04

I: 4800 CYC I: 24 MTH

E2 HHI 737-700

2 22-mar-07

I: 8 YRS I: 36000 CYC

E2 HHI 737-700

3 05-sep-06

I: 36000 CYC I: 12 YRS

E2 HHI 737-700

3 05-sep-06

ATA: 05 - 23

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 05 - 24

05240- 00000

05240- 01000

05240- 02000

05240- 03000

05241- 00000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

PASSENGER COMPARTMENT BODY STA 663.75 TO STA 1016 GENERAL VISUAL INSPECTION OF THE AFT PASSENGER COMPARTMENT 241 -STA 663.75 TO THE AFT PRESSURE BULKHEAD - LEFT AND RIGHT 242 SECTION 44 (PART), 46 AND 47, STA 663.75 TO THE AFT PRESSURE BULKHEAD. E X T E R N A L

emp emp

GENERAL VISUAL INSPECTION OF THE AFT PASSENGER COMPARTMENT 241 -STA 663.75 TO THE AFT PRESSURE BULKHEAD - LEFT AND RIGHT 242 SECTION 44 (PART), 46 AND 47, STA 663.75 TO THE AFT PRESSURE BULKHEAD. I N T E R N A L

emp emp

GENERAL VISUAL INSPECTION OF THE AFT PASSENGER COMPARTMENT 241 -STA 663.75 TO THE AFT PRESSURE BULKHEAD WET AREA (WITHIN 242 APPROXIMATELY 20 INCHES FROM GALLEY SERVICE DOOR, PASSENGER DOOR, GALLEY OR LAV) - LEFT AND RIGHT - SECTION 44 (PART), 46 AND 47, STA 663.75 TO THE AFT PRESSURE BULKHEAD. I N T E R N A L ACCESS GALLEYS AND LAVS REMOVED. FLOOR PANELS, SIDEWALL PANELS AND CEILING PANELS REMOVAL REQUIRED IN WET AREAS.

emp emp

GENERAL VISUAL INSPECTION OF THE AFT PASSENGER COMPARTMENT 241 -STA 663.75 TO THE AFT PRESSURE BULKHEAD DRY AREA (AWAY FROM 242 DOORS, GALLEYS OR LAVS) - LEFT AND RIGHT - SECTION 44 (PART), 46 AND 47, STA 663.75 TO THE AFT PRESSURE BULKHEAD. I N T E R N A L ACCESS FLOOR PANELS, SIDEWALL PANELS AND CEILING PANELS REMOVAL REQUIRED.

emp emp

GENERAL VISUAL INSPECTION OF THE AFT PASSENGER ENTRY DOOR 241 STOPS, LATCHES AND HINGES - SECTION 47, STA 980. E X T E R N A L

834

ITEMS

MPD MRB

MPD MRB

MPD MRB

MPD MRB

MPD MRB

53-882-00 MSI 53-882-00 I: 5500 CYC I: 24 MTH

E2 HHI 737-700

3 22-mar-07

I: 4800 CYC I: 24 MTH

E2 HHI 737-700

2 22-mar-07

I: 8 YRS I: 36000 CYC

E2 HHI 737-700

2 22-mar-07

I: 36000 CYC I: 12 YRS

E2 HHI 737-700

3 22-mar-07

I: 1500 CYC I: 180 DAY

E2 HHI 737-700

5 22-mar-07

53-884-00 MSI 53-884-00

53-886-00 MSI 53-886-00

53-888-00 MSI 53-888-00

53-890-00 MSI 53-890-00

ATA: 05 - 24

Page 1 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

05242- 00000

Date: 23-jul-08

DESCRIPTION GENERAL VISUAL INSPECTION OF THE AFT GALLEY SERVICE DOOR STOPS, LATCHES AND HINGES- SECTION 47, STA 980. E X T E R N A L

ZONE ACCESS 242

STRUCTURE

844

REFERENCES MPD MRB

THRESHOLD INTERVAL

EFF

R L ITEM BY E E REVISION P V DATE

53-892-00 MSI 53-892-00 I: 1500 CYC I: 180 DAY

ITEMS

TSK

ATA: 05 - 24

E2 HHI 737-700

5 22-mar-07

Page 2 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 05 - 30

05300- 00000

05300- 01000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

ZONE 300-EMPENNAGE AND SECTION 48 GENERAL VISUAL INSPECTION OF THE VERTICAL FIN AND HORIZONTAL 320 STABILIZER. 330 E X T E R N A L 340 NOTE( J ) INSPECTION FROM GROUND WITHOUT THE USE OF STANDS OR LADDERS

emp emp emp

MPD MRB

VISUALLY CHECK VERTICAL FIN AND RUDDER, HORIZONTAL STABILIZERS 300 AND ELEVATORS FOR OBVIOUS DAMAGE, EVIDENCE OF FLUID LEAKAGE 330 AND MISSING OR DAMAGED DISCHARGERS 340 E X T E R N A L

emp emp emp

empty

ITEMS

55-800-00 MSI 55-800-00

SERVICE EXPERIENCE

I: 560 CYC I: 90 DAY

E2 HHI 737-700

I: 1 T

E1 HHI 737-700

ATA: 05 - 30

5 22-mar-07

FC SM

1 13-apr-00

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 05 - 31

05310- 00000

05310- 01000

05310- 02000

05310- 03000

05310- 04000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

FUSELAGE STA 1016 TO 1217 GENERAL VISUAL INSPECTION OF THE AREA AFT OF PRESSURE 310 BULKHEAD - SECTION 48, STA 1016 TO STA 1088. E X T E R N A L NOTE( J ) INSPECTION FROM GROUND WITHOUT THE USE OF STANDS OR LADDERS.

emp

GENERAL VISUAL INSPECTION OF THE AREA AFT OF PRESSURE BULKHEAD - SECTION 48, AFT OF PRESSURE BULKHEAD TO STA 1088. I N T E R N A L

311BL emp

311 312

GENERAL VISUAL INSPECTION OF THE STABILIZER TORSION BOX 313 COMPARTMENT - SECTION 48, STA 1088 TO STA 1156. 314 I N T E R N A L ACCESS TORSION BOX COMPARTMENT VISIBLE THROUGH BS 1088 PENETRATION FOR THE HORIZONTAL STABILIZER CENTER SECTION HINGE FITTING.

311BL emp

GENERAL VISUAL INSPECTION OF THE APU COMPARTMENT - SECTION 315 48, STA 1088 TO STA 1156. 316 I N T E R N A L

315A emp

GENERAL VISUAL INSPECTION OF THE TAIL CONE - SECTION 48, STA 1156 TO STA 1217. I N T E R N A L

emp 318BR

317 318

ITEMS

MPD MRB

MPD MRB

MPD MRB

MPD MRB

MPD MRB

53-894-00 MSI 53-894-00 I: 560 CYC I: 90 DAY

E2 HHI 737-700

5 22-mar-07

I: 5500 CYC I: 24 MTH

E2 HHI 737-700

3 22-mar-07

I: 4800 CYC I: 24 MTH

E2 HHI 737-700

2 22-mar-07

I: 5500 CYC I: 24 MTH

E2 HHI 737-700

2 03-jun-04

I: 24 MTH I: 5500 CYC

E2 HHI 737-700

2 03-jun-04

53-896-00 MSI 53-896-00

53-898-00 MSI 53-898-00

53-900-00 MSI 53-900-00

53-902-00 MSI 53-902-00

ATA: 05 - 31

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 05 - 32

05321- 00000

05322- 00000

05322- 01000

05322- 02000

05323- 00000

05323- 01000

05324- 00000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

FIN AND RUDDER GENERAL VISUAL INSPECTION OF THE VERTICAL FIN DORSAL FIN E X T E R N A L

321

GENERAL VISUAL INSPECTION OF THE VERTICAL FIN - LEADING EDGE 322 I N T E R N A L

GENERAL VISUAL INSPECTION OF THE VERTICAL FIN - LEADING EDGE 322 E X T E R N A L

GENERAL VISUAL INSPECTION OF THE VERTICAL FIN - LEADING EDGE 322 I N T E R N A L

emp

322AL

emp

322B

MPD MRB

MPD MRB

MPD MRB

MPD MRB

GENERAL VISUAL INSPECTION OF THE VERTICAL FIN - FRONT SPAR TO 323 REAR SPAR emp I N T E R N A L emp emp emp emp emp

323AL 323BL 323CL 323DL 323EL 323FL 323GL

MPD MRB

GENERAL VISUAL INSPECTION OF THE VERTICAL FIN - FRONT SPAR TO 323 REAR SPAR E X T E R N A L

emp

MPD MRB

GENERAL VISUAL INSPECTION OF THE VERTICAL FIN - REAR SPAR TO TRAILING EDGE I N T E R N A L

324AL 324BL 324DL 324HL

324 emp emp emp

ITEMS

MPD MRB

55-802-00 MSI 55-802-00 I: 5500 CYC I: 24 MTH

E2 HHI 737-700

2 03-jun-04

I: 4800 CYC I: 24 MTH

E2 HHI 737-700

3 22-mar-07

I: 5500 CYC I: 24 MTH

E2 HHI 737-700

2 03-jun-04

I: 36000 CYC I: 12 YRS

E2 HHI 737-700

1 03-jun-04

I: 4800 CYC I: 24 MTH

E2 HHI 737-700

2 22-mar-07

I: 5500 CYC I: 24 MTH

E2 HHI 737-700

2 03-jun-04

I: 4800 CYC I: 24 MTH

E2 HHI 737-700

2 22-mar-07

55-804-00 MSI 55-804-00

55-806-00 MSI 55-806-00

55-808-00 MSI 55-808-00

55-810-00 MSI 55-810-00

55-812-00 MSI 55-812-00

55-814-00 MSI 55-814-00

ATA: 05 - 32

Page 1 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

05324- 01000

GENERAL VISUAL INSPECTION OF THE VERTICAL FIN - REAR SPAR TO TRAILING EDGE E X T E R N A L

324

GENERAL VISUAL INSPECTION OF THE RUDDER E X T E R N A L

325

05325- 00000

05326- 00000

Date: 23-jul-08

GENERAL VISUAL INSPECTION OF THE VERTICAL FIN TIP E X T E R N A L

ZONE ACCESS

326

STRUCTURE

emp

emp

emp

ITEMS

REFERENCES MPD MRB

MPD MRB

MPD MRB

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

55-816-00 MSI 55-816-00 I: 5500 CYC I: 24 MTH

E2 HHI 737-700

2 03-jun-04

I: 5500 CYC I: 24 MTH

E2 HHI 737-700

2 03-jun-04

I: 5500 CYC I: 24 MTH

E2 HHI 737-700

2 03-jun-04

55-818-00 MSI 55-818-00

55-820-00 MSI 55-820-00

ATA: 05 - 32

Page 2 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 05 - 33

05331- 00000

05332- 00000

05332- 01000

05333- 00000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

HORIZONTAL STABILIZER & ELEVATOR LEFT GENERAL VISUAL INSPECTION OF THE HORIZONTAL STABILIZER LEADING EDGE - LEFT AND RIGHT E X T E R N A L

331 341

GENERAL VISUAL INSPECTION OF THE HORIZONTAL STABILIZER - FRONT 332 SPAR TO REAR SPAR - LEFT AND RIGHT 342 E X T E R N A L

emp emp

emp emp

GENERAL VISUAL INSPECTION OF THE HORIZONTAL STABILIZER - FRONT 332 SPAR TO REAR SPAR - LEFT AND RIGHT 342 I N T E R N A L ACCESS WITH ACCESS PROVIDED. AS AN ALTERNATE ACCESS PANEL 332AB AND 342AB CAN BE REMOVED FOR INSPECTION FROM LOWER SIDE OF STABILIZER.

332AT 342AT

GENERAL VISUAL INSPECTION OF THE HORIZONTAL STABILIZER - REAR 333 SPAR TO TRAILING EDGE - LEFT AND RIGHT emp I N T E R N A L emp emp emp emp emp 343 emp emp emp emp emp emp emp

333AB 333AT 333AZ 333BB 333CB 333DB 333EB 343AB 343AT 343AZ 343BB 343CB 343DB 343EB 343FB

ITEMS

MPD MPD MRB MRB

MPD MPD MRB MRB

MPD MPD MRB MRB

MPD MPD MRB MRB

55-822-01 55-836-02 MSI 55-822-01 MSI 55-836-02 I: 5500 CYC I: 24 MTH

E2 HHI 737-700

2 03-jun-04

I: 4000 CYC I: 18 MTH

E2 HHI 737-700

1 03-jun-04

I: 4000 CYC I: 18 MTH

E2 HHI 737-700

2 18-mar-05

I: 4800 CYC I: 24 MTH

E2 HHI 737-700

2 22-mar-07

55-824-01 55-838-02 MSI 55-824-01 MSI 55-838-02

55-826-01 55-840-02 MSI 55-826-01 MSI 55-840-02

55-828-01 55-842-02 MSI 55-828-01 MSI 55-842-02

ATA: 05 - 33

Page 1 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

05333- 01000

05334- 00000

05335- 00000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

GENERAL VISUAL INSPECTION OF THE HORIZONTAL STABILIZER - REAR 333 SPAR TO TRAILING EDGE - LEFT AND RIGHT 343 E X T E R N A L

GENERAL VISUAL INSPECTION OF THE HORIZONTAL STABILIZER ELEVATOR - LEFT AND RIGHT E X T E R N A L

GENERAL VISUAL INSPECTION OF THE HORIZONTAL STABILIZER STABILIZER TIP - LEFT AND RIGHT E X T E R N A L

334 344

335 345

STRUCTURE

emp emp

emp emp

emp emp

ITEMS

REFERENCES MPD MPD MRB MRB

MPD MPD MRB MRB

MPD MPD MRB MRB

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

55-830-01 55-844-02 MSI 55-830-01 MSI 55-844-02 I: 4800 CYC I: 24 MTH

E2 HHI 737-700

2 22-mar-07

I: 4800 CYC I: 24 MTH

E2 HHI 737-700

2 22-mar-07

I: 5500 CYC I: 24 MTH

E2 HHI 737-700

2 03-jun-04

55-832-01 55-846-02 MSI 55-832-01 MSI 55-846-02

55-834-01 55-848-02 MSI 55-834-01 MSI 55-848-02

ATA: 05 - 33

Page 2 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 05 - 40

05400- 00000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

POWER PLANTS & NACELLE STRUTS VISUALLY INSPECT POWERPLANTS, NACELLES AND PYLONS E X T E R N A L

400

emp

empty

SERVICE EXPERIENCE

ITEMS

I: 1 T

ATA: 05 - 40

E1 HHI 737-700

FC SM

1 03-jun-04

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 05 - 41

05410- 00000

05410- 01000

05410- 02000

05410- 03000

05411- 00000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

NO. 1 POWERPLANT+ L/H NACELLE STRUT GENERAL VISUAL INSPECTION OF THE ENGINE NO.1 AND NO.2, AND ENGINE NO.1 AND NO.2 STRUT FAIRINGS. E X T E R N A L

410 420 430 440

GENERAL VISUAL INSPECTION OF THE THRUST REVERSER - ENGINE NO.1 AND NO.2 E X T E R N A L ACCESS THRUST REVERSER IN STOWED AND DEPLOYED POSITION

415 416 425 426

GENERAL VISUAL INSPECTION OF THE THRUST REVERSER - ENGINE NO.1 AND NO.2 E X T E R N A L ACCESS INNER AND OUTER EXTERIOR SURFACES

415 416 425 426

GENERAL VISUAL INSPECTION OF THE FAN COWL - ENGINE NO.1 AND NO.2 E X T E R N A L ACCESS INNER AND OUTER EXTERIOR SURFACE

413 414 423 424

GENERAL VISUAL INSPECTION OF THE ENGINE NO.1 AND NO.2 E X T E R N A L

411 emp emp emp 421 emp emp emp

emp emp emp emp

emp emp emp emp

415 416 425 426

413 414 423 424

413 414 415 416 423 424 425 426

ITEMS

MPD MPD MRB MRB

MPD MPD MRB MRB

MPD MPD MRB MRB

MPD MPD MRB MRB

MPD MPD MRB MRB

70-800-01 70-810-02 MSI 70-800-01 MSI 70-810-02 I: 560 CYC I: 90 DAY

E2 HHI 737-700

5 22-mar-07

I: 2000 CYC

E2 HHI 737-700

1 03-jun-04

I: 2000 CYC

E2 HHI 737-700

1 03-jun-04

I: 4000 CYC

E2 HHI 737-700

1 03-jun-04

I: 2000 CYC

E2 HHI 737-700

1 03-jun-04

70-806-01 70-816-02 MSI 70-806-01 MSI 70-816-02

70-808-01 70-818-02 MSI 70-808-01 MSI 70-818-02

70-804-01 70-814-02 MSI 70-804-01 MSI 70-814-02

70-802-01 70-812-02 MSI 70-802-01 MSI 70-812-02

ATA: 05 - 41

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 05 - 43

05431- 00000

05432- 00000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

LEFT NACELLE STRUT GENERAL VISUAL INSPECTION OF THE FORWARD STRUT FAIRING ENGINE NO.1 AND ENGINE NO.2 I N T E R N A L

GENERAL VISUAL INSPECTION OF THE FAN COWL SUPPORT BEAM ENGINE NO.1 AND ENGINE NO.2 I N T E R N A L

431 emp emp emp emp emp emp emp emp emp emp 441 emp emp emp emp emp emp emp emp emp emp

431AL 431AR 431AT 431BL 431BR 431CL 431CR 431DL 431DR 431EL 431ER 441AL 441AR 441AT 441BL 441BR 441CL 441CR 441DL 441DR 441EL 441ER

MPD MPD MRB MRB

432 442

431AT 441AT

MPD MPD MRB MRB

ITEMS

54-800-01 54-808-02 MSI 54-800-01 MSI 54-808-02 I: 9000 CYC I: 30 MTH

E2 HHI 737-700

1 03-jun-04

I: 5500 CYC I: 24 MTH

E2 HHI 737-700

3 05-sep-06

54-802-01 54-810-02 MSI 54-802-01 MSI 54-810-02

ATA: 05 - 43

Page 1 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

05433- 00000

05434- 00000

Date: 23-jul-08

DESCRIPTION GENERAL VISUAL INSPECTION OF THE STRUT TORQUE BOX - ENGINE NO.1 AND ENGINE NO.2 I N T E R N A L

GENERAL VISUAL INSPECTION OF THE AFT STRUT FAIRING - ENGINE NO.1 AND ENGINE NO.2 I N T E R N A L

ZONE ACCESS

STRUCTURE

REFERENCES

433 emp emp emp emp emp 443 emp emp emp emp emp

433AL 433AR 433AT 433BT 433CT 433DT 443AL 443AR 443AT 443BT 443CT 443DT

MPD MPD MRB MRB

434 emp emp emp 444 emp emp emp

434AL 434AR 434BL 434CL 444AL 444AR 444BR 444CR

MPD MPD MRB MRB

ITEMS

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

54-804-01 54-812-02 MSI 54-804-01 MSI 54-812-02 I: 9000 CYC I: 30 MTH

E2 HHI 737-700

1 03-jun-04

I: 9000 CYC I: 30 MTH

E2 HHI 737-700

1 03-jun-04

54-806-01 54-814-02 MSI 54-806-01 MSI 54-814-02

ATA: 05 - 43

Page 2 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 05 - 50

05500- 00000

05500- 01000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

LEFT WING / RIGHT WING GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT WING E X T E R N A L NOTE( J ) INSPECTION FROM GROUND WITHOUT THE USE OF STANDS OR LADDERS. ACCESS EXTEND CONTROL SURFACES

510 520 530 540 550 560 570 610 620 630 640 650 660 670

emp emp emp emp emp emp emp emp emp emp emp emp emp emp

MPD MPD MRB MRB

VISUALLY CHECK LOWER WING SURFACE AND WING TIP OR WINGLETS 500 (IF INSTALLED) FOR OBVIOUS DAMAGE AND FUEL LEAKAGE 600 E X T E R N A L

emp emp

empty

ITEMS

57-802-01 57-872-02 MSI 57-802-01 MSI 57-872-02

SERVICE EXPERIENCE

I: 560 CYC I: 90 DAY

E2 HHI 737-700

I: 1 T

E1 HHI 737-700

ATA: 05 - 50

5 22-mar-07

FC SM

3 03-jun-04

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 05 - 51

05511- 00000

05511- 01000

05512- 00000

05512- 01000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

WING LEADING EDGE - FORWARD OF FRONT SPAR - INBOARD OF NACELLE STRUT - INCLUDING NACELLE GAP COVER AREA GENERAL VISUAL INSPECTION OF THE LEADING EDGE TO FRONT SPAR 511 - INBOARD OF NACELLE STRUT - LEFT AND RIGHT WING. 611 E X T E R N A L ACCESS EXCLUDING SURFACE UNDER WING TO BODY FAIRING

emp emp

GENERAL VISUAL INSPECTION OF THE LEADING EDGE TO FRONT SPAR - INBOARD OF NACELLE STRUT - LEFT AND RIGHT WING. I N T E R N A L ACCESS FLAPS DEPLOYED

511AB 511AT 511BT 611AB 611AT 611BT

MPD MPD MRB MRB

emp emp emp emp

MPD MPD MRB MRB

511 emp emp 611 emp emp

GENERAL VISUAL INSPECTION OF THE KRUEGER FLAPS NO.1 AND NO.2 512 - LEFT WING, AND NO.3 AND NO.4 - RIGHT WING. 513 E X T E R N A L 612 613

GENERAL VISUAL INSPECTION OF THE KRUEGER FLAPS NO.1 AND NO.2 - LEFT WING, AND NO.3 AND NO.4 - RIGHT WING. I N T E R N A L ACCESS FLAPS DEPLOYED

512 513 612 613

emp emp emp emp

ITEMS

MPD MPD MRB MRB

MPD MPD MRB MRB

57-804-01 57-874-02 MSI 57-804-01 MSI 57-874-02 I: 5500 CYC I: 24 MTH

E2 HHI 737-700

2 03-jun-04

I: 5500 CYC I: 24 MTH

E2 HHI 737-700

2 03-jun-04

I: 5500 CYC I: 24 MTH

E2 HHI 737-700

2 03-jun-04

I: 5500 CYC I: 24 MTH

E2 HHI 737-700

2 03-jun-04

57-806-01 57-876-02 MSI 57-806-01 MSI 57-876-02

57-808-01 57-878-02 MSI 57-808-01 MSI 57-878-02

57-810-01 57-880-02 MSI 57-810-01 MSI 57-880-02

ATA: 05 - 51

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 05 - 52

05520- 00000

05521- 00000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

WING LEADING EDGE - FORWARD OF FRONT SPAR - OUTBOARD OF NACELLE STRUT GENERAL VISUAL INSPECTION OF THE SLATS NO. 1, NO.2, NO.3 AND NO.4 - LEFT WING AND, SLATS NO.5, NO.6, NO.7 AND NO.8 - RIGHT WING. E X T E R N A L ACCESS SLATS IN FULL EXTEND POSITION

522 523 524 525 622 623 624 625

emp emp emp emp emp emp emp emp

MPD MPD MRB MRB

GENERAL VISUAL INSPECTION OF THE LEADING EDGE TO FRONT SPAR 521 - OUTBOARD OF THE NACELLE STRUT - LEFT AND RIGHT WING. 621 E X T E R N A L ACCESS SLATS DEPLOYED

emp emp

MPD MPD MRB MRB

ITEMS

57-816-01 57-886-02 MSI 57-816-01 MSI 57-886-02 I: 5500 CYC I: 24 MTH

E2 HHI 737-700

2 03-jun-04

I: 5500 CYC I: 24 MTH

E2 HHI 737-700

2 03-jun-04

57-812-01 57-882-02 MSI 57-812-01 MSI 57-882-02

ATA: 05 - 52

Page 1 of 3


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

05521- 01000

GENERAL VISUAL INSPECTION OF THE LEADING EDGE TO FRONT SPAR - OUTBOARD OF THE NACELLE STRUT - LEFT AND RIGHT WING. I N T E R N A L ACCESS SLATS DEPLOYED 521AAB, 521ABB, 621AAB

Date: 23-jul-08

ZONE ACCESS 521 emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp 621 emp emp emp emp emp emp emp emp emp emp emp emp emp emp

STRUCTURE

521AB 521BB 521CB 521DB 521EB 521FB 521GB 521HB 521JB 521KB 521LB 521MB 521NB 521PB 521QB 521RB 521SB 521TB 521UB 521VB 521WB 521XB 521YB 521ZB 621AB 621BB 621CB 621DB 621EB 621FB 621GB 621HB 621JB 621KB 621LB 621MB 621NB 621PB 621QB

ITEMS

REFERENCES MPD MPD MRB MRB

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

57-814-01 57-884-02 MSI 57-814-01 MSI 57-884-02 I: 5500 CYC I: 24 MTH

ATA: 05 - 52

E2 HHI 737-700

3 03-jun-04

Page 2 of 3


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

ZONE ACCESS emp emp emp emp emp emp emp emp emp

05526- 00000

05526- 01000

Date: 23-jul-08

GENERAL VISUAL INSPECTION OF THE WING TIP - LEFT AND RIGHT WING 526 E X T E R N A L 626

GENERAL VISUAL INSPECTION OF THE WING TIP - LEFT AND RIGHT WING 526 I N T E R N A L emp emp 626 emp emp

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

621RB 621SB 621TB 621UB 621VB 621WB 621XB 621YB 621ZB emp emp

526AB 526BB 526CB 626AB 626BB 626CB

ITEMS

MPD MPD MRB MRB

MPD MPD MRB MRB

57-818-01 57-888-02 MSI 57-818-01 MSI 57-888-02 I: 5500 CYC I: 24 MTH

E2 HHI 737-700

2 03-jun-04

I: 21600 CYC I: 6 YRS

E2 HHI 737-700

2 25-apr-06

57-820-01 57-890-02 MSI 57-820-01 MSI 57-890-02

ATA: 05 - 52

Page 3 of 3


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

05 - 53

WING INSPAR AREA (FUEL TANKS) - INBOARD OF WING RIB 22 - WS 643.50

05531- 00000

05531- 01000

05532- 00000

Date: 23-jul-08

ZONE ACCESS

GENERAL VISUAL INSPECTION OF THE CENTER FUEL TANK - LEFT AND 531 RIGHT WING 631 E X T E R N A L ACCESS EXCLUDING SURFACE UNDER WING TO BODY FAIRING

emp emp

GENERAL VISUAL INSPECTION OF THE CENTER FUEL TANK - LEFT AND 531 RIGHT WING emp I N T E R N A L 631 emp

531AB 531BB 631AB 631BB

GENERAL VISUAL INSPECTION OF THE MAIN FUEL TANK - LEFT AND RIGHT WING E X T E R N A L

532 632

STRUCTURE

emp emp

ITEMS

REFERENCES

MPD MPD MRB MRB

MPD MPD MRB MRB

MPD MPD MRB MRB

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

57-824-01 57-894-02 MSI 57-824-01 MSI 57-894-02 I: 5500 CYC I: 24 MTH

E2 HHI 737-700

2 03-jun-04

I: 36000 CYC I: 10 YRS

E2 HHI 737-700

1 03-jun-04

I: 5500 CYC I: 24 MTH

E2 HHI 737-700

2 03-jun-04

57-822-01 57-892-02 MSI 57-822-01 MSI 57-892-02

57-828-01 57-898-02 MSI 57-828-01 MSI 57-898-02

ATA: 05 - 53

Page 1 of 3


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

05532- 01000

Date: 23-jul-08

DESCRIPTION GENERAL VISUAL INSPECTION OF THE MAIN FUEL TANK - LEFT AND RIGHT WING I N T E R N A L ACCESS ZONE 532: DO NOT REMOVE 532AZ AND 532BZ AT THE SAME TIME ZONE 632: DO NOT REMOVE 632AZ AND 632BZ AT THE SAME TIME

ZONE ACCESS 532 emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp 632 emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp

STRUCTURE

532AB 532AZ 532BB 532BZ 532CB 532DB 532EB 532FB 532GB 532HB 532JB 532KB 532LB 532MB 532NB 532PB 532QB 532RB 632AB 632AZ 632BB 632BZ 632CB 632DB 632EB 632FB 632GB 632HB 632JB 632KB 632LB 632MB 632NB 632PB 632QB 632RB

ITEMS

REFERENCES MPD MPD MRB MRB

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

57-826-01 57-896-02 MSI 57-826-01 MSI 57-896-02 I: 36000 CYC I: 10 YRS

ATA: 05 - 53

E2 HHI 737-700

1 03-jun-04

Page 2 of 3


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

05533- 00000

05533- 01000

05534- 00000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

GENERAL VISUAL INSPECTION OF THE SURGE TANK - LEFT AND RIGHT 533 WING 633 E X T E R N A L

STRUCTURE

emp emp

REFERENCES MPD MPD MRB MRB

GENERAL VISUAL INSPECTION OF THE SURGE TANK - LEFT AND RIGHT 533 WING emp I N T E R N A L emp 633 emp emp

533AB 533BB 533CB 633AB 633BB 633CB

MPD MPD MRB MRB

GENERAL VISUAL INSPECTION OF THE DRY BAY - LEFT AND RIGHT WING 534 E X T E R N A L 634

emp emp

MPD MPD MRB MRB

ITEMS

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

57-832-01 57-902-02 MSI 57-832-01 MSI 57-902-02 I: 5500 CYC I: 24 MTH

E2 HHI 737-700

2 03-jun-04

I: 36000 CYC I: 10 YRS

E2 HHI 737-700

1 03-jun-04

I: 5500 CYC I: 24 MTH

E2 HHI 737-700

2 03-jun-04

57-830-01 57-900-02 MSI 57-830-01 MSI 57-900-02

57-834-01 57-904-02 MSI 57-834-01 MSI 57-904-02

ATA: 05 - 53

Page 3 of 3


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 05 - 54

05541- 00000

05542- 00000

05542- 01000

05543- 00000

05543- 01000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

WING TRAILING EDGE FLAP TRACK FAIRINGS GENERAL VISUAL INSPECTION OF THE FLAP SUPPORT NO. 4 - LEFT WING , AND FLAP SUPPORT NO.5 - RIGHT WING - SECTION 46, STA 727. I N T E R N A L ACCESS FLAPS EXTENDED

133 134 194 541 641 emp

emp emp emp emp 194BL 194BR

MPD MPD MRB MRB

GENERAL VISUAL INSPECTION OF THE FAIRING FLAP SUPPORT NO.3 - 542 LEFT WING, AND THE FAIRING FLAP SUPPORT NO.6 - RIGHT WING 642 E X T E R N A L ACCESS FLAPS EXTENDED

emp emp

MPD MPD MRB MRB

GENERAL VISUAL INSPECTION OF THE FAIRING FLAP SUPPORT NO.3 - 542 LEFT WING, AND THE FAIRING FLAP SUPPORT NO.6 - RIGHT WING 642 I N T E R N A L ACCESS FLAPS EXTENDED, INSIDE OF FAIRING

emp emp

GENERAL VISUAL INSPECTION OF THE FAIRING FLAP SUPPORT NO.2 - 543 LEFT WING, AND THE FAIRING FLAP SUPPORT NO.7 - RIGHT WING 643 E X T E R N A L ACCESS FLAPS EXTENDED

emp emp

GENERAL VISUAL INSPECTION OF THE FAIRING FLAP SUPPORT NO.2 - 543 LEFT WING, AND THE FAIRING FLAP SUPPORT NO.7 - RIGHT WING 643 I N T E R N A L ACCESS FLAPS EXTENDED, INSIDE OF FAIRING

emp emp

ITEMS

MPD MPD MRB MRB

MPD MPD MRB MRB

MPD MPD MRB MRB

53-904-01 53-906-02 MSI 53-904-01 MSI 53-906-02 I: 5500 CYC I: 24 MTH

E2 HHI 737-700

5 18-mar-05

I: 5500 CYC I: 24 MTH

E2 HHI 737-700

2 03-jun-04

I: 5500 CYC I: 24 MTH

E2 HHI 737-700

3 18-mar-05

I: 5500 CYC I: 24 MTH

E2 HHI 737-700

2 03-jun-04

I: 5500 CYC I: 24 MTH

E2 HHI 737-700

3 18-mar-05

57-836-01 57-906-02 MSI 57-836-01 MSI 57-906-02

57-838-01 57-908-02 MSI 57-838-01 MSI 57-908-02

57-840-01 57-910-02 MSI 57-840-01 MSI 57-910-02

57-842-01 57-912-02 MSI 57-842-01 MSI 57-912-02

ATA: 05 - 54

Page 1 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

05544- 00000

05544- 01000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

GENERAL VISUAL INSPECTION OF THE FAIRING FLAP SUPPORT NO.1 - 544 LEFT WING, AND THE FAIRING FLAP SUPPORT NO.8 - RIGHT WING 644 E X T E R N A L ACCESS FLAPS EXTENDED

emp emp

GENERAL VISUAL INSPECTION OF THE FAIRING FLAP SUPPORT NO.1 - 544 LEFT WING, AND THE FAIRING FLAP SUPPORT NO.8 - RIGHT WING 644 I N T E R N A L ACCESS FLAPS EXTENDED, INSIDE OF FAIRING

emp emp

STRUCTURE

ITEMS

REFERENCES MPD MPD MRB MRB

MPD MPD MRB MRB

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

57-844-01 57-914-02 MSI 57-844-01 MSI 57-914-02 I: 5500 CYC I: 24 MTH

E2 HHI 737-700

2 03-jun-04

I: 5500 CYC I: 24 MTH

E2 HHI 737-700

3 18-mar-05

57-846-01 57-916-02 MSI 57-846-01 MSI 57-916-02

ATA: 05 - 54

Page 2 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

05 - 55

WING TRAILING EDGE - AFT OF REAR SPAR - INBOARD OF OUTBOARD TRAILING EDGE FLAP

05551- 00000

05551- 01000

05552- 00000

Date: 23-jul-08

ZONE ACCESS

STRUCTURE

REFERENCES

GENERAL VISUAL INSPECTION OF THE REAR SPAR TO LANDING GEAR 551 SUPPORT BEAM - LEFT AND RIGHT WING 651 E X T E R N A L ACCESS EXCLUDING SURFACE UNDER WING TO BODY FAIRING

emp emp

GENERAL VISUAL INSPECTION OF THE REAR SPAR TO LANDING GEAR 551 SUPPORT BEAM - LEFT AND RIGHT WING emp I N T E R N A L emp emp emp emp emp emp emp emp emp 651 emp emp emp emp emp emp emp emp emp emp

551AB 551AT 551BB 551BT 551CB 551CT 551DB 551DT 551EB 551ET 551FB 651AB 651AT 651BB 651BT 651CB 651CT 651DB 651DT 651EB 651ET 651FB

MPD MPD MRB MRB

GENERAL VISUAL INSPECTION OF THE INBOARD SPOILER NO.6 - LEFT WING, AND THE INBOARD SPOILER NO.7 - RIGHT WING. E X T E R N A L ACCESS SPOILER RAISED

emp emp

MPD MPD MRB MRB

552 652

ITEMS

MPD MPD MRB MRB

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

57-848-01 57-918-02 MSI 57-848-01 MSI 57-918-02 I: 5500 CYC I: 24 MTH

E2 HHI 737-700

2 03-jun-04

I: 21600 CYC I: 6 YRS

E2 HHI 737-700

2 25-apr-06

I: 5500 CYC I: 24 MTH

E2 HHI 737-700

2 03-jun-04

57-850-01 57-920-02 MSI 57-850-01 MSI 57-920-02

57-852-01 57-922-02 MSI 57-852-01 MSI 57-922-02

ATA: 05 - 55

Page 1 of 2


HHI R E V

ITEM 05553- 00000

R

737-6

MAINTENANCE SCHEDULE

05553- 01000

DESCRIPTION

ZONE ACCESS

GENERAL VISUAL INSPECTION OF THE INBOARD FLAPS - LEFT AND RIGHT 553 WING 653 E X T E R N A L ACCESS FLAPS EXTENDED

emp emp

GENERAL VISUAL INSPECTION OF THE INBOARD MAIN FLAPS - LEFT AND 553 RIGHT WING 653 I N T E R N A L ACCESS FLAPS EXTENDED

553BB 653BB

STRUCTURE

R

Date: 23-jul-08

ITEMS

REFERENCES MPD MPD MRB MRB

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

57-854-01 57-924-02 MSI 57-854-01 MSI 57-924-02

MPD MPD MRB MRB MPD MPD MRB MRB

57-926-02 57-856-01 MSI 57-856-01 MSI 57-926-02 57-856-01 57-926-02 MSI 57-856-01 MSI 57-926-02

AMM AMM

05-41-05-210 05-41-06-210

I: 5500 CYC I: 24 MTH

E2 HHI 737-700

2 03-jun-04

I: 21600 CYC I: 6 YRS

E2 HHI 737-700

3 23-jul-08

ATA: 05 - 55

Page 2 of 2


HHI R E V

R

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

05 - 56

WING TRAILING EDGE - AFT OF REAR SPAR - OUTBOARD OF INBOARD TRAILING EDGE FLAP - INBOARD OF FIXED TRAILING EDGE

05560- 00000

GENERAL VISUAL INSPECTION OF THE SPOILERS NO.1, 2, 3, 4, 5 - LEFT WING, AND SPOILERS NO.8, 9, 10, 11, 12 - RIGHT WING E X T E R N A L ACCESS SPOILERS RAISED

05567- 00000

Date: 23-jul-08

STRUCTURE

REFERENCES

562 563 564 565 566 662 663 664 665 666

emp emp emp emp emp emp emp emp emp emp

MPD MPD MRB MRB MPD MPD MRB MRB

57-860-01 57-930-02 MSI 57-860-01 MSI 57-930-02 57-860-01 57-930-02 MSI 57-860-01 MSI 57-930-02

AMM AMM

05-41-05-210 05-41-06-210

GENERAL VISUAL INSPECTION OF THE REAR SPAR TO TRAILING EDGE 561 - OUTBOARD OF INBOARD FLAP - INBOARD OF FIXED TRAILING EDGE - 661 LEFT AND RIGHT WING E X T E R N A L ACCESS FLAPS DOWN, SPOILERS RAISED

emp emp

MPD MPD MRB MRB

57-858-01 57-928-02 MSI 57-858-01 MSI 57-928-02

GENERAL VISUAL INSPECTION OF THE OUTBOARD FLAPS - LEFT AND RIGHT WING E X T E R N A L ACCESS FLAPS EXTENDED

emp emp

R 05561- 00000

ZONE ACCESS

567 667

ITEMS

MPD MPD MRB MRB

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

I: 5500 CYC I: 24 MTH

E2 HHI 737-700

3 23-jul-08

I: 5500 CYC I: 24 MTH

E2 HHI 737-700

2 03-jun-04

I: 5500 CYC I: 24 MTH

E2 HHI 737-700

2 03-jun-04

57-862-01 57-932-02 MSI 57-862-01 MSI 57-932-02

ATA: 05 - 56

Page 1 of 1


HHI R E V

ITEM

DESCRIPTION

05 - 57

FIXED TRAILING EDGE - OUTBOARD OF OUTBOARD FLAP - INBOARD OF WING TIP WBL 658.17

05571- 00000

05571- 01000

R

737-6

MAINTENANCE SCHEDULE

05571- 02000

R

Date: 23-jul-08

ZONE ACCESS

GENERAL VISUAL INSPECTION OF THE FIXED TRAILING EDGE - LEFT AND 571 RIGHT WING 671 E X T E R N A L

GENERAL VISUAL INSPECTION OF THE FIXED TRAILING EDGE - LEFT AND RIGHT WING I N T E R N A L ACCESS AILERON CONTROL AREA ONLY

571 emp 671 emp

GENERAL VISUAL INSPECTION OF THE FIXED TRAILING EDGE - LEFT AND 571 RIGHT WING emp I N T E R N A L emp emp emp emp emp emp 671 emp emp emp emp emp emp emp

STRUCTURE

emp emp

571AB 571BB 671AB 671BB

571AB 571AT 571BB 571BT 571CB 571DB 571EB 571FB 671AB 671AT 671BB 671BT 671CB 671DB 671EB 671FB

ITEMS

REFERENCES

MPD MPD MRB MRB

MPD MPD MRB MRB

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

57-864-01 57-934-02 MSI 57-864-01 MSI 57-934-02 I: 5500 CYC I: 24 MTH

E2 HHI 737-700

2 03-jun-04

I: 5500 CYC I: 24 MTH

E2 HHI 737-700

2 03-jun-04

I: 10 YRS

E2 HHI 737-700

2 23-jul-08

57-868-01 57-938-02 MSI 57-868-01 MSI 57-938-02

MPD MPD MRB MRB MPD MPD MRB MRB

57-866-01 57-936-02 MSI 57-866-01 MSI 57-936-02 57-866-01 57-936-02 MSI 57-866-01 MSI 57-936-02

AMM AMM

05-41-05-210 05-41-06-210

ATA: 05 - 57

Page 1 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

05572- 00000

DESCRIPTION

ZONE ACCESS

GENERAL VISUAL INSPECTION OF THE AILERON - LEFT AND RIGHT WING 572 E X T E R N A L 672

STRUCTURE

emp emp

REFERENCES MPD MPD MRB MRB

THRESHOLD INTERVAL

ITEMS

EFF

R L ITEM BY E E REVISION P V DATE

57-870-01 57-940-02 MSI 57-870-01 MSI 57-940-02 I: 5500 CYC I: 24 MTH

Date: 23-jul-08

TSK

ATA: 05 - 57

E2 HHI 737-700

2 03-jun-04

Page 2 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 05 - 70

05700- 00000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

LANDING GEAR VISUALLY INSPECT LANDING GEARS, LANDING GEAR DOORS INCLUDING 700 WHEEL WELLS E X T E R N A L

emp

empty

SERVICE EXPERIENCE

ITEMS

I: 1 T

ATA: 05 - 70

E1 HHI 737-700

FC SM

1 03-jun-04

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 05 - 71

05710- 00000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

NOSE LANDING GEAR & DOORS GENERAL VISUAL INSPECTION OF THE NOSE LANDING GEAR AND 710 LANDING GEAR DOORS. E X T E R N A L ACCESS INSPECTION FROM GROUND WITHOUT THE USE OF STANDS OR LADDERS.

emp

MPD MRB

32-800-00 MSI 32-800-00 I: 560 CYC I: 90 DAY

ITEMS

ATA: 05 - 71

E2 HHI 737-700

5 22-mar-07

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 05 - 73

05730- 00000

05730- 01000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

LEFT MAIN LANDING GEAR & L.G. DOORS GENERAL VISUAL INSPECTION OF THE MAIN LANDING GEAR AND LANDING 730 GEAR DOORS - LEFT AND RIGHT. 740 E X T E R N A L ACCESS INSPECTION FROM GROUND WITHOUT THE USE OF STANDS OR LADDERS.

emp emp

GENERAL VISUAL INSPECTION OF THE MAIN LANDING GEAR AND LANDING 730 GEAR DOORS - LEFT AND RIGHT. 740 E X T E R N A L

emp emp

ITEMS

MPD MPD MRB MRB

MPD MPD MRB MRB

32-804-01 32-808-02 MSI 32-804-01 MSI 32-808-02 I: 560 CYC I: 90 DAY

E2 HHI 737-700

5 22-mar-07

I: 5500 CYC I: 24 MTH

E2 HHI 737-700

3 18-mar-05

32-806-01 32-810-02 MSI 32-806-01 MSI 32-810-02

ATA: 05 - 73

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 05 - 80

05800- 00000

05800- 01000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

ZONE 800- PASSENGER AND CARGO DOORS GENERAL VISUAL INSPECTION OF THE ENTRY DOORS, SERVICE DOORS, 820 AUTOMATIC OVERWING EXITS, AND CARGO DOORS. 830 E X T E R N A L 840 ACCESS DOORS CLOSED. INSPECTION FROM GROUND WITHOUT THE USE OF STANDS OR LADDERS.

emp emp emp

MPD MRB

VISUALLY INSPECT ENTRY AND SERVICE DOORS, CARGO DOORS AND 800 EMERGENCY EXITS, INCLUDING DOOR SEALS E X T E R N A L ACCESS INSPECTION FROM GROUND WITHOUT THE USE OF STANDS OR LADDERS

emp

empty

52-800-00 MSI 52-800-00

SERVICE EXPERIENCE

ITEMS

I: 560 CYC I: 90 DAY

E2 HHI 737-700

I: 1 T

E1 HHI 737-700

ATA: 05 - 80

5 22-mar-07

FC SM

3 03-jun-04

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 05 - 82

05821- 00000

05821- 01000

05822- 00000

05822- 01000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

DOORS, LOWER HALF FUSELAGE, L/H GENERAL VISUAL INSPECTION OF THE FORWARD CARGO DOOR SECTION 43, STA 460. E X T E R N A L

821

GENERAL VISUAL INSPECTION OF THE FORWARD CARGO DOOR SECTION 43, STA 460. I N T E R N A L

821 emp emp emp

821

MPD MRB

821AR 821AZ 821BR 821BZ

MPD MRB

GENERAL VISUAL INSPECTION OF THE AFT CARGO DOOR - SECTION 46, 822 STA 827. E X T E R N A L

822

MPD MRB

GENERAL VISUAL INSPECTION OF THE AFT CARGO DOOR - SECTION 46, 822 STA 827. emp I N T E R N A L emp emp

822AR 822AZ 822BR 822BZ

ITEMS

MPD MRB

52-802-02 MSI 52-802-02 I: 1500 CYC I: 180 DAY

E2 HHI 737-700

5 22-mar-07

I: 5500 CYC I: 24 MTH

E2 HHI 737-700

2 03-jun-04

I: 1500 CYC I: 180 DAY

E2 HHI 737-700

5 22-mar-07

I: 5500 CYC I: 24 MTH

E2 HHI 737-700

2 03-jun-04

52-804-02 MSI 52-804-02

52-806-02 MSI 52-806-02

52-808-02 MSI 52-808-02

ATA: 05 - 82

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 05 - 83

05831- 00000

05831- 01000

05833- 00000

05833- 01000

05834- 00000

05834- 01000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

DOORS, UPPER HALF FUSELAGE, L/H GENERAL VISUAL INSPECTION OF THE FORWARD PASSENGER DOOR - 831 SECTION 41, STA 345. E X T E R N A L

831

GENERAL VISUAL INSPECTION OF THE FORWARD PASSENGER DOOR - 831 SECTION 41, STA 345. emp I N T E R N A L emp emp emp emp

831AW 831AZ 831BZ 831CZ 831DZ 831EZ

MPD MRB

GENERAL VISUAL INSPECTION OF THE AUTOMATIC OVERWING EXIT SECTION 44, STA 627. E X T E R N A L

833

833

MPD MRB

GENERAL VISUAL INSPECTION OF THE AUTOMATIC OVERWING EXIT SECTION 44, STA 627. I N T E R N A L ACCESS AUTOMATIC OVERWING EXIT DOOR LINER REMOVAL REQUIRED.

833

833AZ

GENERAL VISUAL INSPECTION OF THE AFT PASSENGER DOOR - SECTION 834 47, STA 980. E X T E R N A L

834

GENERAL VISUAL INSPECTION OF THE AFT PASSENGER DOOR - SECTION 834 47, STA 980. emp I N T E R N A L emp emp emp emp

834AW 834AZ 834BZ 834CZ 834DZ 834EZ

ITEMS

MPD MRB

MPD MRB

MPD MRB

MPD MRB

52-810-01 MSI 52-810-01 I: 1500 CYC I: 180 DAY

E2 HHI 737-700

5 22-mar-07

I: 5500 CYC I: 24 MTH

E2 HHI 737-700

2 03-jun-04

I: 5500 CYC I: 24 MTH

E2 HHI 737-700

2 03-jun-04

I: 18000 CYC I: 8 YRS

E2 HHI 737-700

1 03-jun-04

I: 1500 CYC I: 180 DAY

E2 HHI 737-700

6 22-mar-07

I: 5500 CYC I: 24 MTH

E2 HHI 737-700

2 03-jun-04

52-812-01 MSI 52-812-01

52-818-01 MSI 52-818-01

52-820-01 MSI 52-820-01

52-822-01 MSI 52-822-01

52-824-01 MSI 52-824-01

ATA: 05 - 83

Page 1 of 1


HHI R E V

ITEM 05 - 84 05841- 00000

R

737-6

MAINTENANCE SCHEDULE

05841- 01000

R

05843- 00000

05843- 01000

05844- 00000

05844- 01000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

DOORS, UPPER HALF FUSELAGE, R/H GENERAL VISUAL INSPECTION OF THE FORWARD GALLEY SERVICE DOOR - SECTION 41, STA 340. E X T E R N A L

841

841

GENERAL VISUAL INSPECTION OF THE FORWARD GALLEY SERVICE DOOR - SECTION 41, STA 340. I N T E R N A L

841 emp emp emp emp emp

841AW 841AZ 841BZ 841CZ 841DZ 841EZ

MPD MRB

GENERAL VISUAL INSPECTION OF THE AUTOMATIC OVERWING EXIT SECTION 44, STA 627. E X T E R N A L

843

843

MPD MRB

GENERAL VISUAL INSPECTION OF THE AUTOMATIC OVERWING EXIT SECTION 44, STA 627. I N T E R N A L ACCESS AUTOMATIC OVERWING EXIT DOOR LINER REMOVAL REQUIRED

843

GENERAL VISUAL INSPECTION OF THE AFT GALLEY SERVICE DOOR SECTION 47, STA 980. E X T E R N A L

844

GENERAL VISUAL INSPECTION OF THE AFT GALLEY SERVICE DOOR SECTION 47, STA 980. I N T E R N A L

844 emp emp emp emp emp

843AZ

844

844AW 844AZ 844BZ 844CZ 844DZ 844EZ

ITEMS

MPD MRB

MPD MRB

MPD MRB

MPD MRB

52-826-02 MSI 52-826-02 I: 1500 CYC I: 180 DAY

E2 HHI 737-700

5 22-mar-07

I: 4000 CYC I: 18 MTH I: 24 MTH

E2 HHI 737-700

3 23-jul-08

I: 5500 CYC I: 24 MTH

E2 HHI 737-700

2 03-jun-04

I: 18000 CYC I: 8 YRS

E2 HHI 737-700

1 03-jun-04

I: 1500 CYC I: 180 DAY

E2 HHI 737-700

5 22-mar-07

I: 4800 CYC I: 24 MTH

E2 HHI 737-700

2 22-mar-07

52-828-02 MSI 52-828-02

52-834-02 MSI 52-834-02

52-836-02 MSI 52-836-02

52-838-02 MSI 52-838-02

52-840-02 MSI 52-840-02

ATA: 05 - 84

Page 1 of 1


HHI R E V

ITEM 05 - 90

N

737-6

MAINTENANCE SCHEDULE

05900- 20290

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

05900- 20300

N

N

05900- 20310

N

N

05900- 20320

N

N

05900- 20330

N N

05900- 20340

N

Date: 23-jul-08

TSK

EFF

R L ITEM BY E E REVISION P V DATE

EZAP CLEAN AREA FORWARD OF NOSE WHEEL WELL. (EZAP)

112

112A

MPD MRB

20-290-00 MSI 20-290-00

N N

THRESHOLD INTERVAL

CLEAN THE AREA ABOVE AND OUTBOARD OF NOSE WHEEL WELL. (EZAP) LEFT AND RIGHT SIDE. ACCESS REMOVE/DISPLACE INSULATION BLANKETS AS REQUIRED.

113 emp emp 114 emp emp

113AC 113AW 113BW 114AC 114AW 114BW

MPD MRB

CLEAN THE AREA BEHIND THE ELECTRICAL AND ELECTRONICS RACK AND IN THE AIRSTAIR COMPARTMENT (IF INSTALLED). (EZAP) ACCESS ACCESS PANEL 117BL IS ONLY FOR AIRPLANES WITH AIRSTAIRS INSTALLED. ALTERNATE ACCESS BEHIND E2, E3, AND E4 ELECTRONICS RACK IS THROUGH 121JW, 121KW, 121LW AND 122HW PANELS.

117 emp 118 emp emp emp

117A 117BL 121JW 121KW 121LW 122HW

MPD MRB

INSPECT (DETAILED) THE POWER FEEDER AND EXPOSED EWIS BEHIND THE ELECTRICAL AND ELECTRONICS RACK. (EZAP) ACCESS ALTERNATE ACCESS BEHIND E2, E3, AND E4 ELECTRONICS RACK IS THROUGH 121JW, 121KW, 121LW AND 122HW PANELS.

117 118 emp emp emp

117A 121JW 121KW 121LW 122HW

MPD MRB

CLEAN AREAS BEHIND CEILING AND SIDEWALLS. (EZAP) ACCESS CEILING AND SIDEWALL PANELS REMOVAL REQUIRED.

121 122

emp emp

MPD MRB

CLEAN AREAS BELOW FORWARD CARGO COMPARTMENT. (EZAP) 123 124 ACCESS CENTER FLOOR PANELS REMOVAL REQUIRED. CARGO LOADING SYSTEM REMOVED/DISPLACED AS REQUIRED.

emp emp

ITEMS

MPD MRB

I: 36000 CYC I: 12 YRS

S

HHI 737-700

0 23-jul-08

I: 36000 CYC I: 12 YRS

S

HHI 737-700

0 23-jul-08

I: 18000 CYC I: 6 YRS

S

HHI 737-700

0 23-jul-08

I: 18000 CYC I: 6 YRS

E3 HHI 737-700

0 23-jul-08

I: 18000 CYC I: 6 YRS

S

HHI 737-700

0 23-jul-08

I: 18000 CYC I: 6 YRS

S

HHI 737-700

0 23-jul-08

20-300-00 MSI 20-300-00

20-310-00 MSI 20-310-00

20-320-00 MSI 20-320-00

20-330-00 MSI 20-330-00

20-340-00 MSI 20-340-00

ATA: 05 - 90

Page 1 of 8


HHI R E V

ITEM

N

05900- 20350

DESCRIPTION CLEAN AREA AFT OF FORWARD CARGO COMPARTMENT. (EZAP)

05900- 20360

N N

05900- 20370

N

N

05900- 20380

N N

05900- 20390

N N

05900- 20400

N N

05900- 20410

N

Date: 23-jul-08

ZONE ACCESS

STRUCTURE

REFERENCES

125 emp 126

121EW 121HW 122GW

MPD MRB

INSPECT (GENERAL VISUAL) THE EWIS IN THE MAIN LANDING GEAR WHEEL WELL. (EZAP) ACCESS THROUGH MAIN LANDING GEAR OPENING.

133 134

emp emp

MPD MRB

CLEAN AREAS BEHIND THE AFT CARGO COMPARTMENT CEILING AND SIDEWALL PANELS. (EZAP) ACCESS CEILING AND SIDEWALL PANELS REMOVAL REQUIRED.

141 142

N N

737-6

MAINTENANCE SCHEDULE

emp emp

CLEAN AREA BELOW AFT CARGO COMPARTMENT. (EZAP) 143 144 ACCESS CENTER FLOOR PANELS REMOVAL REQUIRED. CARGO LOADING SYSTEM REMOVED/DISPLACED AS REQUIRED.

emp emp

CLEAN AREA IN AFT CARGO COMPARTMENT EQUIPMENT BAY. (EZAP) ACCESS AFT CARGO PANELS AT 947 BULKHEAD REMOVAL REQUIRED.

emp emp

145 146

CLEAN FROM WATERLINE 208 TO 232 AND STA. 186 TO STA 211. (EZAP) 211 212 ACCESS ACCESSIBLE AREAS FORWARD OF AND ABOVE THE RUDDER PEDALS.

emp emp

INSPECT (DETAILED) THE EXPOSED EWIS IN THE FLIGHT COMPARTMENT. 211 (EZAP) 212 ACCESS WITH ACCESS PROVIDED. SEATS REMOVED. CONTROL STAND ACCESS PANELS, OVERHEAD AND SIDEWALL PANELS, GLARESHIELD, INSTRUMENT PANELS, P6, P18 FRONT PANELS, REMOVAL REQUIRED.

emp emp

ITEMS

MPD MRB

MPD MRB

MPD MRB

MPD MRB

MPD MRB

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

20-350-00 MSI 20-350-00 I: 36000 CYC I: 12 YRS

S

HHI 737-700

0 23-jul-08

I: 5500 CYC I: 30 MTH

E2 HHI 737-700

0 23-jul-08

I: 18000 CYC I: 6 YRS I: 1 s.N

S

HHI 737-700

0 23-jul-08

I: 18000 CYC I: 6 YRS

S

HHI 737-700

0 23-jul-08

I: 18000 CYC I: 6 YRS

S

HHI 737-700

0 23-jul-08

I: 18000 CYC I: 6 YRS

S

HHI 737-700

0 23-jul-08

I: 36000 CYC I: 12 YRS

E3 HHI 737-700

0 23-jul-08

20-360-00 MSI 20-360-00

20-370-00 MSI 20-370-00

20-380-00 MSI 20-380-00

20-390-00 MSI 20-390-00

20-400-00 MSI 20-400-00

20-410-00 MSI 20-410-00

ATA: 05 - 90

Page 2 of 8


HHI R E V

ITEM

N

05900- 20420

N

N

05900- 20430

N

N

05900- 20440

N

N

737-6

MAINTENANCE SCHEDULE

05900- 20450

DESCRIPTION

ZONE ACCESS

CLEAN AREAS ABOVE CEILING, SIDEWALLS AND UNDER THE RACEWAY 221 COVER PLATES ON BOTH SIDES OF THE PASSENGER COMPARTMENT. 222 (EZAP) ACCESS WITH ACCESS PROVIDED. GALLEYS AND LAVS REMOVED. CEILING AND SIDEWALL PANELS REMOVAL REQUIRED.

emp emp

CLEAN AREAS ABOVE CEILING, SIDEWALLS AND RETURN AIR GRILLES 231 IN FORWARD PASSENGER COMPARTMENT. (EZAP) 232 ACCESS GALLEYS AND LAVS REMOVED. SIDEWALL PANELS, CEILING PANELS AND AIR RETURN GRILLES REMOVAL REQUIRED.

emp emp

CLEAN AREAS ABOVE CEILING, SIDEWALLS AND RETURN AIR GRILLES 241 IN AFT PASSENGER COMPARTMENT. (EZAP) 242 ACCESS GALLEYS AND LAVS REMOVED. SIDEWALL PANELS, CEILING PANELS AND AIR RETURN GRILLES REMOVAL REQUIRED.

emp emp

INSPECT (DETAILED) THE POWER FEEDERS AND EXPOSED EWIS IN THE 311 AREA AFT OF PRESSURE BULKHEAD. (EZAP) 312

311BL emp

STRUCTURE

REFERENCES MPD MRB

MPD MRB

MPD MRB

MPD MRB

05900- 20460

INSPECT (DETAILED) THE GENERATOR POWER FEEDERS, IGNITION LEADS AND ELECTRIC STARTER IN THE APU COMPARTMENT. (EZAP)

315 316

315A emp

MPD MRB

05900- 20470

INSPECT (DETAILED) THE GENERATOR POWER FEEDERS ON ENGINE NO. 1. (EZAP)

N N

05900- 20480

N

Date: 23-jul-08

INSPECT (DETAILED) THE GENERATOR POWER FEEDERS ON ENGINE NO. 2. (EZAP)

411 emp emp emp

413 414 415 416

MPD MRB

421 emp emp emp

423 424 425 426

MPD MRB

ITEMS

EFF

R L ITEM BY E E REVISION P V DATE

I: 36000 CYC I: 12 YRS

S

HHI 737-700

0 23-jul-08

I: 36000 CYC I: 12 YRS

S

HHI 737-700

0 23-jul-08

I: 36000 CYC I: 12 YRS

S

HHI 737-700

0 23-jul-08

I: 36000 CYC I: 12 YRS

S

HHI 737-700

0 23-jul-08

I: 5500 CYC I: 30 MTH

E3 HHI 737-700

0 23-jul-08

I: 5500 CYC I: 30 MTH

E3 HHI 737-700

0 23-jul-08

I: 5500 CYC I: 30 MTH

E3 HHI 737-700

0 23-jul-08

20-430-00 MSI 20-430-00

20-440-00 MSI 20-440-00

20-450-00 MSI 20-450-00

20-460-00 MSI 20-460-00

N N

TSK

20-420-00 MSI 20-420-00

N N

THRESHOLD INTERVAL

20-470-00 MSI 20-470-00

20-480-00 MSI 20-480-00

ATA: 05 - 90

Page 3 of 8


HHI R E V

ITEM

DESCRIPTION

N

05900- 20490

INSPECT (DETAILED) THE POWER FEEDERS AND EXPOSED EWIS IN FWD STRUT FAIRING. (EZAP) NOTE( E ) ENGINE NO. 1

N

N

737-6

MAINTENANCE SCHEDULE

05900- 20500

ZONE ACCESS

STRUCTURE

REFERENCES

431 emp emp emp emp emp emp emp emp emp emp

431AL 431AR 431AT 431BL 431BR 431CL 431CR 431DL 431DR 431EL 431ER

MPD MRB

INSPECT (DETAILED) THE POWER FEEDERS AND EXPOSED EWIS IN FAN 432 COWL SUPPORT BEAM. (EZAP)

431AT

MPD MRB

05900- 20510

N

N

05900- 20520

N

Date: 23-jul-08

INSPECT (DETAILED) THE POWER FEEDERS AND EXPOSED EWIS IN STRUT TORQUE BOX. (EZAP)

433 emp emp emp emp emp

433AL 433AR 433AT 433BT 433CT 433DT

MPD MRB

INSPECT (DETAILED) THE POWER FEEDERS AND EXPOSED EWIS IN FWD 441 STRUT FAIRING. (EZAP) emp emp emp emp emp emp emp emp emp emp

441AL 441AR 441AT 441BL 441BR 441CL 441CR 441DL 441DR 441EL 441ER

MPD MRB

ITEMS

TSK

EFF

R L ITEM BY E E REVISION P V DATE

20-490-00 MSI 20-490-00 I: 18000 CYC I: 6 YRS I: 1 s.N

E3 HHI 737-700

0 23-jul-08

I: 18000 CYC I: 6 YRS

E3 HHI 737-700

0 23-jul-08

I: 18000 CYC I: 6 YRS

E3 HHI 737-700

0 23-jul-08

I: 18000 CYC I: 6 YRS

E3 HHI 737-700

0 23-jul-08

20-500-00 MSI 20-500-00

N N

THRESHOLD INTERVAL

20-510-00 MSI 20-510-00

20-520-00 MSI 20-520-00

ATA: 05 - 90

Page 4 of 8


HHI

737-6

MAINTENANCE SCHEDULE

R E V

ITEM

N

05900- 20530

DESCRIPTION

ZONE ACCESS

INSPECT (DETAILED) THE POWER FEEDERS AND EXPOSED EWIS IN FAN 442 COWL SUPPORT BEAM. (EZAP)

STRUCTURE

441AT

REFERENCES MPD MRB

05900- 20540

INSPECT (DETAILED) THE POWER FEEDERS AND EXPOSED EWIS IN STRUT TORQUE BOX. (EZAP)

N

N

05900- 20550

N

Date: 23-jul-08

INSPECT (DETAILED) THE EXPOSED EWIS IN THE LEADING EDGE TO FRONT SPAR. (EZAP) ACCESS FLAPS DEPLOYED.

443 emp emp emp emp emp

443AL 443AR 443AT 443BT 443CT 443DT

MPD MRB

511 emp emp

511AB 511AT 511BT

MPD MRB

ITEMS

TSK

EFF

R L ITEM BY E E REVISION P V DATE

20-530-00 MSI 20-530-00

N N

THRESHOLD INTERVAL

I: 18000 CYC I: 6 YRS

E3 HHI 737-700

0 23-jul-08

I: 18000 CYC I: 6 YRS

E3 HHI 737-700

0 23-jul-08

I: 18000 CYC I: 6 YRS

E3 HHI 737-700

0 23-jul-08

20-540-00 MSI 20-540-00

20-550-00 MSI 20-550-00

ATA: 05 - 90

Page 5 of 8


HHI R E V

ITEM

N

05900- 20560

N

N

737-6

MAINTENANCE SCHEDULE

05900- 20570

DESCRIPTION INSPECT (DETAILED) THE EXPOSED EWIS IN THE LEADING EDGE TO FRONT SPAR. (EZAP) ACCESS SLATS DEPLOYED.

ZONE ACCESS 521 emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp

INSPECT (DETAILED) THE EXPOSED EWIS FROM THE REAR SPAR TO L.G. 551 SUPPORT BEAM. (EZAP)

STRUCTURE

REFERENCES

521AAB 521AB 521ABB 521AT 521BB 521CB 521DB 521EB 521FB 521GB 521HB 521JB 521KB 521LB 521MB 521NB 521PB 521QB 521RB 521SB 521TB 521UB 521VB 521WB 521XB 521YB 521ZB

MPD MRB

551DB

MPD MRB

05900- 20580

N

Date: 23-jul-08

INSPECT (DETAILED) THE EXPOSED EWIS FROM THE REAR SPAR TO TRAILING EDGE. (EZAP) ACCESS FLAPS DOWN, SPOILERS RAISED.

561

emp

ITEMS

MPD MRB

TSK

EFF

R L ITEM BY E E REVISION P V DATE

20-560-00 MSI 20-560-00 I: 36000 CYC I: 12 YRS

E3 HHI 737-700

0 23-jul-08

I: 18000 CYC I: 6 YRS

E3 HHI 737-700

0 23-jul-08

I: 36000 CYC I: 12 YRS

E3 HHI 737-700

0 23-jul-08

20-570-00 MSI 20-570-00

N N

THRESHOLD INTERVAL

20-580-00 MSI 20-580-00

ATA: 05 - 90

Page 6 of 8


HHI R E V

ITEM

N

05900- 20590

N N

05900- 20600

N

N

737-6

MAINTENANCE SCHEDULE

05900- 20610

DESCRIPTION

ZONE ACCESS

STRUCTURE

INSPECT (DETAILED) THE EXPOSED EWIS IN THE LEADING EDGE TO FRONT SPAR. (EZAP) ACCESS FLAPS DEPLOYED.

611 emp emp

611AB 611AT 611BT

MPD MRB

INSPECT (DETAILED) THE EXPOSED EWIS IN THE LEADING EDGE TO FRONT SPAR. (EZAP) ACCESS SLATS DEPLOYED.

621 emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp

621AAB 621AB 621ABB 621AT 621BB 621CB 621DB 621EB 621FB 621GB 621HB 621JB 621KB 621LB 621MB 621NB 621PB 621QB 621RB 621SB 621TB 621UB 621VB 621WB 621XB 621YB 621ZB

MPD MRB

651DB

MPD MRB

INSPECT (DETAILED) THE EXPOSED EWIS FROM THE REAR SPAR TO L.G. 651 SUPPORT BEAM. (EZAP)

N

Date: 23-jul-08

REFERENCES

ITEMS

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

20-590-00 MSI 20-590-00 I: 36000 CYC I: 12 YRS

E3 HHI 737-700

0 23-jul-08

I: 36000 CYC I: 12 YRS

E3 HHI 737-700

0 23-jul-08

I: 18000 CYC I: 6 YRS

E3 HHI 737-700

0 23-jul-08

20-600-00 MSI 20-600-00

20-610-00 MSI 20-610-00

ATA: 05 - 90

Page 7 of 8


HHI

737-6

MAINTENANCE SCHEDULE

R E V

ITEM

N

05900- 20620

N

Date: 23-jul-08

DESCRIPTION INSPECT (DETAILED) THE EXPOSED EWIS FROM THE REAR SPAR TO TRAILING EDGE. (EZAP) ACCESS FLAPS DOWN, SPOILERS RAISED.

ZONE ACCESS 661

STRUCTURE

emp

REFERENCES MPD MRB

THRESHOLD INTERVAL

EFF

R L ITEM BY E E REVISION P V DATE

20-620-00 MSI 20-620-00 I: 36000 CYC I: 12 YRS

ITEMS

TSK

ATA: 05 - 90

E3 HHI 737-700

0 23-jul-08

Page 8 of 8


HHI R E V

ITEM 08 08 - 10

R

737-6

MAINTENANCE SCHEDULE

081000 01000

R

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

LEVELING AND WEIGHING WEIGHING PERFORM AIRCRAFT WEIGHING. REFER TO WEIGHING PROCEDURE IN MS INTRODUCTION. NOTE( I ) FOR WEIGHING DATES REFER TO MS INTRODUCTION CHAPTER 5.

000

emp

empty

AMM AAR

ITEMS

08-11-00-580-801 EU-OPS 1.605 B

I: 1 s.N

ATA: 08 - 10

M2 HHI 737-700

3 23-jul-08

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 21 21 - 25

212502 40000

212503 00000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

AIR CONDITIONING RECIRCULATION SYSTEM REPLACE THE RECIRCULATION FAN HEPA FILTER (S).

121

PERFORM A DETAILED INSPECTION OF THE RECIRCULATION FAN CHECK 121 VALVE(S) FOR CONDITION, SECURITY AND PROPER OPERATION. emp

emp

1201S 821

ITEMS

MPD MRB

21-010-00 MSI 21-010-00 RTE:7

AMTOSS AMTOSS

21-25-02-40 21-25-02-00

MPD MRB

21-015-00 MSI 21-015-00 RTE:8

AMTOSS

21-25-03-200

I: 6000 FLH

S

HHI 737-700

2 18-mar-05

I: 6000 FLH

E3 HHI 737-700

0 30-nov-05

ATA: 21 - 25

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 21 - 27

212700 70000

212700 71000

212700 89000

212701 00000

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

EQUIPMENT COOLING SYSTEM OPERATIONALLY CHECK THE ALTERNATE E/E COOLING EXHAUST FAN. 211 212 NOTE( J ) THIS TASK ALSO CHECKS THE NORMAL E/E COOLING EXHAUST FAN CHECK VALVE.

emp emp

OPERATIONALLY CHECK THE OVERBOARD EXHAUST VALVE IN SMOKE 211 CLEARANCE MODE. 212

emp emp

OPERATIONALLY CHECK THE ALTERNATE E/E COOLING SUPPLY FAN. 211 212 NOTE( J ) THIS TASK ALSO CHECKS THE NORMAL E/E COOLING SUPPLY FAN CHECK VALVE.

emp emp

REPLACE THE E/E COOLING SUPPLY FAN FILTER

emp

118

MPD MRB

21-030-00 MSI 21-030-00 RTE:9

AMTOSS

21-27-00-70

MPD MRB

21-050-00 MSI 21-050-00 RTE:9

AMTOSS

21-27-00-70

MPD MRB

21-020-00 MSI 21-020-00 RTE:9

AMTOSS

21-27-00-89

MPD MRB

21-040-00 MSI 21-040-00 RTE:6 MSI 21-040-00 RTE:9

MRB AMTOSS AMTOSS

Date: 23-jul-08

THRESHOLD INTERVAL

ITEMS

21-27-01-40 21-27-01-00

I: 4000 FLH

F1 HHI 737-700

1 03-jun-04

I: 6000 FLH

F1 HHI 737-700

2 18-mar-05

I: 4000 FLH

F1 HHI 737-700

1 03-jun-04

I: 6000 FLH

S

2 18-mar-05

ATA: 21 - 27

HHI 737-700

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 21 - 31

213100 71000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

CABIN PRESSURE CONTROL SYSTEM OPERATIONALLY CHECK THE OUTFLOW VALVE MANUAL MODE (MOTOR), 211 SELECTOR PANEL, INDICATOR, INDICATOR FEEDBACK MODULE. 212

emp emp

ITEMS

MPD MRB

21-060-00 MSI 21-060-00 RTE:9

AMTOSS

21-31-00-71

I: 6000 FLH

ATA: 21 - 31

F1 HHI 737-700

2 18-mar-05

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 21 - 32

213203 70000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

CABIN PRESSURE RELIEF FUNCTIONALLY CHECK THE NEGATIVE PRESSURE RELIEF DOOR.

146

emp

ITEMS

MPD MRB

21-090-00 MSI 21-090-00 RTE:9

AMTOSS

21-32-03-700-801

I: 10 YRS

ATA: 21 - 32

F2 HHI 737-700

2 03-jun-04

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 21 - 33

213300 00000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

CABIN PRESSURE INDICATION AND WARNING SYSTEM FUNCTIONAL CHECK OF THE CABIN PRESSURE SWITCH.

112

112A

ITEMS

MPD MRB

31-020-00 MSI 31-020-00 RTE:8

AMTOSS

21-33-00-00

I: 6000 FLH

ATA: 21 - 33

F2 HHI 737-700

3 18-mar-05

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 21 - 51

215103 00000

215105 40000

DESCRIPTION

ZONE ACCESS

STRUCTURE

TSK

EFF

R L ITEM BY E E REVISION P V DATE

AIR COOLING SYSTEM CLEAN THE PRIMARY AND SECONDARY HEAT EXCHANGERS.

CHECK THE LEFT AND RIGHT WATER SEPARATOR INDICATION DISK (WITH THE AIRCONDITIONING SYSTEM OPERATING).

131 132 emp emp emp emp

emp 192BL 192BR 192CL 192CR 192DR

MPD MRB

21-100-00 MSI 21-100-00 RTE:6

AMTOSS

21-51-03-000-801

123 124 emp

192CL 192CR 192DR

MPD MPD MRB

21-140-01 21-140-02 MSI 21-140-01 RTE:9 MSI 21-140-02 RTE:9

MRB AMTOSS

Date: 23-jul-08

THRESHOLD INTERVAL

REFERENCES

ITEMS

21-51-05-40

I: 2000 CYC

S

I: 600 FLH

E2 HHI 737-700

ATA: 21 - 51

HHI 737-700

2 03-jun-04

2 18-mar-05

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 21 - 61

216106 10000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

ZONE TEMPERATURE CONTROL AND INDICATION CLEAN OR REPLACE THE CABIN TEMPERATURE SENSOR FILTERS (737-700 211 HAS ONE EACH IN THE CONTROL AND PASSENGER CABINS) 222

emp emp

ITEMS

MPD MRB

21-150-00 MSI 21-150-00 RTE:6

AMTOSS AMTOSS AMTOSS

21-61-06-10 21-61-06-40 21-61-06-00

I: 1200 FLH

ATA: 21 - 61

S

HHI 737-700

3 25-apr-06

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 23 23 - 24

232400 00000

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

COMMUNICATION EMERGENCY LOCATOR TRANSMITTER OPERATIONALLY CHECK THE EMERGENCY LOCATOR TRANSMITTER (AUTOMATIC/FIXED TYPE). NOTE( I ) AT VENDOR'S RECOMMENDATION

242

emp

MPD MRB

AMM

Date: 23-jul-08

THRESHOLD INTERVAL

ITEMS

23-100-00 MSI 23-100-00 RTE:8 ARTEX I: 18 MTH INSTALLATION AND OPS. MANUAL DOC. NO.570-5004, CHAPTER 4 23-24-00

ATA: 23 - 24

F1 HHI 737-700 only: D-AHIC

0 18-mar-05

Page 1 of 1


HHI R E V

ITEM 23 - 30

R

737-6

MAINTENANCE SCHEDULE

233011 00000

DESCRIPTION

ZONE ACCESS

STRUCTURE

TSK

EFF

R L ITEM BY E E REVISION P V DATE

PASSENGER ADDRESS (PA) AND ENTERTAINMENT SYSTEM OPERATIONAL CHECK OF THE PASSENGER ADDRESS SPEAKERS, ATTENDANT AND LAVATORY SPEAKERS

200

emp

R

Date: 23-jul-08

THRESHOLD INTERVAL

REFERENCES

ITEMS

MPD MRB

23-090-00 MSI 23-090-00 RTE:9

AMTOSS AMM

23-31-00-74 23-31-00-740-801

I: 15000 FLH

ATA: 23 - 30

F1 HHI 737-700

6 23-jul-08

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 23 - 60

236000 76000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

STATIC DISCHARGER CHECK OF RESISTANCE OF STATIC DISCHARGERS.

325 326 330 340 526 570 572 626 670 672

emp emp emp emp emp emp emp emp emp emp

ITEMS

MPD MRB

23-030-00 MSI 23-030-00 RTE:9

AMTOSS

23-61-00-760-801

I: 4 YRS

ATA: 23 - 60

S HHI M1 737-700

2 03-jun-04

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 23 - 71

237100 71000

237100 73000

237121 00000

DESCRIPTION

ZONE ACCESS

STRUCTURE

TSK

EFF

R L ITEM BY E E REVISION P V DATE

VOICE RECORDING SYSTEM OPERATIONAL CHECK OF THE VOICE RECORDER.

FUNCTIONAL CHECK OF THE VOICE RECORDER FOR AUDIO FIDELITY. NOTE( I ) MRB INTERVAL IS 2 YRS

OPERATIONAL CHECK OF THE ULB AT BATTERY REPLACEMENT. NOTE( I ) AT BATTERY REPLACEMENT

211

210

142

emp

emp

822

MPD MRB

23-040-00 MSI 23-040-00 RTE:9

AMTOSS

23-71-00-71

MPD MRB

23-050-00 MSI 23-050-00 RTE:9

AAR AMTOSS

NFL II-56/01 2.3.7 23-71-00-73

MPD MPD MRB

23-060-00 23-070-00 MSI 23-060-00 RTE:9 MSI 23-070-00 RTE:9

MRB AMTOSS AMTOSS AMTOSS AMTOSS

Date: 23-jul-08

THRESHOLD INTERVAL

REFERENCES

ITEMS

23-71-21-70 23-71-21-96 23-71-21-40 23-71-21-00

I: 300 FLH I: 40 DAY

F1 HHI 737-700

2 18-mar-05

I: 12 MTH I: 1 s.N

F2 HHI 737-700

1 03-jun-04

I: 1 s.N

F1 HHI 737-700

2 03-jun-04

ATA: 23 - 71

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 24 24 - 00

240000 01000

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

CHANGE LEFT AND RIGHT IDG OIL.

411 421

413 423

MPD MPD MRB

R L ITEM BY E E REVISION P V DATE

DETAILED INSPECTION OF LEFT AND RIGHT IDG DELTA P INDICATOR

411 421

413AL 423AL

DETAILED INSPECTION OF LEFT AND RIGHT IDG OIL LEVEL. SERVICE IF 411 NECESSARY. 421

413AL 423AL

12-13-21-60

MPD MPD MRB

24-020-01 24-020-02 MSI 24-020-01 RTE:6 MSI 24-020-02 RTE:6

AMTOSS

12-13-21-20

MPD MPD MRB

24-030-01 24-030-02 MSI 24-030-01 RTE:6 MSI 24-030-02 RTE:6

AMTOSS

ITEMS

24-010-01 24-010-02 MSI 24-010-01 RTE:6 MSI 24-010-02 RTE:6

AMTOSS

MRB

Date: 23-jul-08

EFF

GENERAL

MRB

240000 03000

TSK

ELECTRICAL POWER

MRB

240000 02000

THRESHOLD INTERVAL

12-13-21-20

I: 1800 FLH

S

HHI 737-700

2 25-apr-06

I: 400 FLH

E3 HHI 737-700

2 18-mar-05

I: 400 FLH

S HHI E3 737-700

2 18-mar-05

ATA: 24 - 00

Page 1 of 8


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

240000 04000

GENERAL VISUAL INSPECTION OF HIRF/L SENSITIVE WIRE RUNS OUTSIDE THE PRESSURE VESSEL ON LEFT AND RIGHT SIDE OF THE AIRPLANE. LOOK FOR OBVIOUS SIGNS OF DAMAGE AND LACK OF SECURITY OF WIRE RUNS.

240000 05000

Date: 23-jul-08

GENERAL VISUAL INSPECTION OF HIRF/L SENSITIVE WIRE RUNS INSIDE THE PRESSURE VESSEL. LOOK FOR OBVIOUS SIGNS OF DAMAGE AND LACK OF SECURITY OF WIRE RUNS.

ZONE ACCESS

STRUCTURE

REFERENCES

131 133 191 emp 415 416 425 426 441 emp emp emp emp emp emp emp 510 520 550 560 610 620 650 660 730 740

emp emp 191FL 191FR emp emp emp emp 431AL 431AR 431AT 431CR 441AL 441AR 441AT 441CL 511AB emp emp emp 611AB 621GB emp emp emp emp

MPD MPD MRB

AMTOSS AMTOSS

05-55-26-20 05-55-25-20

117 emp emp 118 emp emp emp emp

112A 113BW 117A 121EW 121JW 121KW 122GW 122HW

MPD MRB

20-020-00 MSI 20-020-00 RTE:8

AMTOSS

05-55-15-20

ITEMS

MRB

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

20-010-01 20-010-02 MSI 20-010-01 RTE:8 MSI 20-010-02 RTE:8 I: 15000 FLH

E2 HHI 737-700

3 05-sep-06

I: 30000 FLH

E2 HHI 737-700

2 05-sep-06

ATA: 24 - 00

Page 2 of 8


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

240000 06000

PERFORM A DETAILED VISUAL INSPECTION OF HIRF/L SENSITIVE CONNECTORS OUTSIDE THE PRESSURE VESSEL ON LEFT AND RIGHT SIDE OF THE AIRPLANE.

Date: 23-jul-08

ZONE ACCESS 133 134 191 emp 440 emp emp emp emp emp emp emp emp emp emp emp emp emp 510 520 550 560 610 620 640 730 740

STRUCTURE

emp emp 191FL 191FR 416AR 431AL 431AR 431AT 431BL 431BR 431CL 431CR 441AL 441AR 441AT 441BL 441BR 441CL 511AB emp emp emp 611AB 621GB emp emp emp

ITEMS

REFERENCES MPD MPD MRB MRB AMTOSS AMTOSS

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

20-030-01 20-030-02 MSI 20-030-01 RTE:8 MSI 20-030-02 RTE:8 05-55-24-20 05-55-23-20

I: 12000 FLH

ATA: 24 - 00

E3 HHI 737-700

3 22-mar-07

Page 3 of 8


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

240000 07000

PERFORM A FUNCTIONAL CHECK OF THE HIRF/L SENSITIVE CONNECTORS OUTSIDE THE PRESSURE VESSEL ON THE LEFT AND RIGHT SIDE OF THE AIRPLANE. CHECK DC RESISTANCE FROM THE BACKSHELL TO GROUND.

240000 08000

Date: 23-jul-08

PERFORM A DETAILED VISUAL INSPECTION OF THE HIRF/L SENSITIVE CONNECTORS INSIDE THE PRESSURE VESSEL. DURING THE INSPECTION DO NOT DISCONNECT CONNECTORS. LOOK FOR CONDITION, SECURITY AND SIGNS OF CORROSION.

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

133 134 191 emp 431 emp emp emp 441 emp emp emp 510 520 550 560 610 emp 650 660 730 740

emp emp 191FL 191FR 431AL 431AR 431AT 431CR 441AL 441AR 441AT 441CL 511AB emp emp emp 611AB 621GB emp emp emp emp

MPD MPD MRB

AMM AMM AMTOSS AMTOSS

05-55-44-200 05-55-45-200 05-55-41-20 05-55-40-20

117 emp emp 118 emp emp emp emp 211 212

112A 113BW 117A 121EW 121JW 121KW 122GW 122HW emp emp

MPD MRB

20-050-00 MSI 20-050-00 RTE:8

AMTOSS AMTOSS

20-10-37-12 05-55-15-200-801

ITEMS

MRB

TSK

EFF

R L ITEM BY E E REVISION P V DATE

20-040-01 20-040-02 MSI 20-040-01 RTE:8 MSI 20-040-02 RTE:8 I: 15000 FLH

F2 HHI 737-700

3 22-mar-07

I: 20000 FLH

E3 HHI 737-700

3 05-sep-06

ATA: 24 - 00

Page 4 of 8


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

240000 09000

240000 09100

240000 10000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

FUNCTIONAL CHECK OF HIRF/L SENSITIVE CONNECTORS INSIDE THE 112 PRESSURE VESSEL BY DC RESISTANCE CHECK FROM BACKSHELL TO 113 GROUND. 117 118 emp emp emp emp 121 122 211 212 230

112A 113BW 117A 121EW 121JW 121KW 122GW 122HW emp emp emp emp emp

MPD MRB

20-060-00 MSI 20-060-00 RTE:8

AMTOSS

20-40-11-760-802

PERFORM A FUNCTIONAL CHECK OF THE HIRF/L SENSITIVE CONNECTORS 310 INSIDE THE EMPENNAGE.

311BL

MPD MRB

20-140-00 MSI 20-140-00 RTE:8

AMM AMM

05-55-42-200 05-55-46-200

MPD MRB

20-070-00 MSI 20-070-00 RTE:8

AMTOSS

05-55-15-200-803

PERFORM A DETAILED VISUAL INSPECTION OF THE HIRF/L SENSITIVE PIG TAILS INSIDE THE PRESSURE VESSEL. LOOK FOR CONDITION OF SECURITY AND SIGNS OF CORROSION.

117 emp emp 118 emp emp emp emp 211 212

112A 113BW 117A 121EW 121JW 121KW 122GW 122HW emp emp

ITEMS

TSK

EFF

R L ITEM BY E E REVISION P V DATE

I: 30000 FLH

F2 HHI 737-700

3 05-sep-06

I: 15000 FLH

F2 HHI 737-700

0 22-mar-07

I: 30000 FLH

E3 HHI 737-700

3 05-sep-06

ATA: 24 - 00

Page 5 of 8


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

240000 11000

PERFORM A DETAILED VISUAL INSPECTION OF THE HIRF/L SENSITIVE PIG TAILS OUTSIDE THE PRESSURE VESSEL ON THE LEFT AND RIGHT SIDE OF THE AIRPLANE. INSPECT FOR CONDITION OF SECURITY AND SIGNS OF CORROSION.

Date: 23-jul-08

ZONE ACCESS 133 134 191 emp 415 416 431 emp emp emp emp emp emp emp 510 520 550 560 610 620 650 660 730 740

STRUCTURE

emp emp 191FL 191FR emp emp 431AL 431AR 431AT 431CR 441AL 441AR 441AT 441CL 511AB emp emp emp 611AB 621GB emp emp emp emp

ITEMS

REFERENCES MPD MPD MRB MRB AMTOSS AMTOSS

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

20-080-01 20-080-02 MSI 20-080-01 RTE:8 MSI 20-080-02 RTE:8 05-55-23-20 05-55-24-20

I: 15000 FLH

ATA: 24 - 00

E3 HHI 737-700

5 05-sep-06

Page 6 of 8


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

240000 13000

PERFORM A GENERAL VISUAL INSPECTION OF THE BONDING STRAPS AT THE FOLLOWING LOCATIONS: - 1 STRAP EACH ON THE RUDDER - 2 STRAPS PER AILERON, LEADING EDGE FLAP, SPOILER AND EACH ELEVATOR SURFACE. - STRUT TO WING BONDING USES 1 STRAP PER WING. - EACH AIR CONDITIONING PACK COMPARTMENT DOOR, MAIN LANDING GEAR DOOR, EACH ENGINE COWLING AND EACH STRUT TO ENGINE INSTALLATION USES 2 BONDING STRAPS.

Date: 23-jul-08

ZONE ACCESS 192 emp 325 334 emp 344 emp 431 441 emp 512 513 562 563 564 565 571 emp emp 612 613 662 663 664 665 671 emp emp 731 732 733 741 742 743

STRUCTURE

192CL 192CR 324ABL 334GB 334NB 344GB 344NB emp 431CL 441CR emp emp emp emp emp emp 571BB 571CB 571DB emp emp emp emp emp emp 671BB 671CB 671DB emp emp emp emp emp emp

ITEMS

REFERENCES MPD MRB

20-100-00 MSI 20-100-00 RTE:8

AMTOSS

05-55-08-20

THRESHOLD INTERVAL

I: 15000 FLH

ATA: 24 - 00

TSK

EFF

E2 HHI 737-700

R L ITEM BY E E REVISION P V DATE

4 05-sep-06

Page 7 of 8


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

240000 14000

240000 15000

240000 16000

DESCRIPTION

ZONE ACCESS

STRUCTURE

GENERAL VISUAL INSPECTION OF EXTERNAL (COWL OPEN) HARNESS 411 CONDITION AND SECURITY OF LEFT AND RIGHT ENGINE emp emp emp 421 emp emp emp

413 414 415 416 423 424 425 426

MPD MPD MRB

AMTOSS

05-55-10-20

DETAILED INSPECTION OF THE LEFT AND RIGHT ENGINE CONNECTORS 411 FOR TIGHTNESS (ALL CONNECTORS ON HARNESS J5, J6, J7, J8, J9, J10, emp CJ9, CJ10, MW0301, MW0302, MW0303, MW0304). emp emp 421 emp emp emp

413 414 415 416 423 424 425 426

MPD MPD MRB

20-120-01 20-120-02 MSI 20-120-01 RTE:8 MSI 20-120-02 RTE:8

AMTOSS

05-55-10-22

GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT ENGINE BONDING 415 STRAPS RELATED TO HIRF / LIGHTNING FOR CONDITION AND SECURITY. 416 425 426 433 443

415AL 416AR 425AL 426AR emp emp

MPD MPD MRB

20-130-01 20-130-02 MSI 20-130-01 RTE:8 MSI 20-130-02 RTE:8

MRB

MRB

MRB AMTOSS

240000 18000

Date: 23-jul-08

MEASURE THE AIRPLANE EXTERNAL POWER RECEPTACLE NEUTRAL PIN CONTINUITY TO AIRFRAME GROUND. MEASURE THE AIRPLANE ELECTRICAL RESISTANCE TO GROUND.

118 734 744

emp emp emp

ITEMS

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

20-110-01 20-110-02 MSI 20-110-01 RTE:8 MSI 20-110-02 RTE:8 I: 6000 FLH

E1 HHI 737-700

2 18-mar-05

I: 15000 FLH

E3 HHI 737-700

3 03-jun-04

05-55-11-200-801

I: 6000 FLH

E1 HHI 737-700

5 05-sep-06

737-SL-20-029-B

I: 4000 FLH

M2 HHI 737-700

2 03-jun-04

empty

SIL

ATA: 24 - 00

Page 8 of 8


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 24 - 11

241141 00000

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

REPLACE LEFT AND RIGHT IDG CHARGE AND SCAVENGE FILTERS.

411 421

413 423

MPD MPD MRB

EFF

R L ITEM BY E E REVISION P V DATE

TORQUE CHECK LEFT AND RIGHT ENGINE IDG QUICK ATTACH/DETACH 411 (QAD) COUPLING. 421

413 423

24-11-41-00

MPD MPD MRB

24-050-01 24-050-02 MSI 24-050-01 RTE:6 MSI 24-050-02 RTE:6

AMTOSS

ITEMS

24-040-01 24-040-02 MSI 24-040-01 RTE:6 MSI 24-040-02 RTE:6

AMTOSS

MRB

Date: 23-jul-08

TSK

AC GENERATOR DRIVE SYSTEM

MRB

241161 20000

THRESHOLD INTERVAL

24-11-61-20

I: 1800 FLH

S

HHI 737-700

2 25-apr-06

I: 1800 FLH

M1 HHI 737-700

2 25-apr-06

ATA: 24 - 11

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 24 - 31

243141 72000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

DC GENERATION SYSTEM CHECK REMOTE CONTROL CIRCUIT BREAKER NOTE( E ) FOR DUAL BATTERY INSTALLATION ONLY!

117 118

emp emp

ITEMS

MPD MRB

24-110-00 MSI 24-110-00 RTE:8

AMTOSS

24-31-41-71

I: 10000 CYC

ATA: 24 - 31

F1 HHI 737-700

2 03-jun-04

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 24 - 34

243400 71200

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

STANDBY POWER SYSTEM OPERATIONAL TEST STANDBY POWER CONTROL UNIT NOTE( E ) FOR DUAL BATTERY INSTALLATION ONLY!

210

emp

ITEMS

MPD MRB

24-100-00 MSI 24-100-00 RTE:8

AMTOSS

24-34-00-710-802

I: 15 DAY

ATA: 24 - 34

F1 HHI 737-700

2 03-jun-04

Page 1 of 1


HHI R E V

ITEM

DESCRIPTION

25

EQUIPMENT & FURNISHINGS

25 - 00

EQUIPMENT / FURNISHINGS

250000 01000

250000 04001

250000 05001

250000 06001

250000 08001

D

737-6

MAINTENANCE SCHEDULE

250000 09001

ZONE ACCESS

STRUCTURE

emp

REFERENCES

CHECK THE EXPIRATION DATE OF THE FLIGHT CREW SEAT BELTS, PASSENGER SEAT BELTS, CREW REST BUNKS/SEAT BELTS, SPECIAL EQUIPMENT USING SEAT BELT WEBBING. IF THE EXPIRATION DATE IS LESS THAN 12 MONTH INFORM HHI-ENGINEERING FOR REPLACEMENT DISPOSITION. NOTE( I ) EXPIRATION DATE IS MANUFACTURING DATE PLUS 12 YEARS

200

AAR

INTERIOR CLEANING DURING NIGHT STOP. NOTE( I ) EXCEPTIONALLY, THE INTERVAL MAY BE EXTENDED TO 7 DAYS MAX.

220 240

emp emp

empty

FLOOR COVERING IN ENTRY AND GALLEY AREAS FOR OBVIOUS DAMAGE 220 AND CONTAMINATION 240 NOTE( I ) EXCEPTIONALLY, THE INTERVAL MAY BE EXTENDED TO 7 DAYS

emp emp

empty

GALLEYS FOR GENERAL CONDITION, OBVIOUS DAMAGE AND CONTAMINATION NOTE( I ) EXCEPTIONALLY, THE INTERVAL MAY BE EXTENDED TO 7 DAYS

222

emp

empty

CARPET IN ENTIRE CABIN AREA FOR OBVIOUS DAMAGE AND CONTAMINATION NOTE( I ) EXCEPTIONALLY, THE INTERVAL MAY BE EXTENDED TO 7 DAYS

220 240

emp emp

empty

emp emp

empty

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

NFL II 83/99 I: 12 MTH

E2 HHI 737-700

1 23-jul-08

SERVICE EXPERIENCE

I: 1 Z

S

HHI 737-700

SM

2 11-dec-01

SERVICE EXPERIENCE

I: 1 Z

E1 HHI 737-700

SM

2 11-dec-01

SERVICE EXPERIENCE

I: 1 Z

E2 HHI 737-700

SM

3 03-jun-04

SERVICE EXPERIENCE

I: 1 Z

E1 HHI 737-700

SM

2 11-dec-01

ITEM DELETED.

D

3 23-jul-08 250000 13001

Date: 23-jul-08

SIDEWALL - AND CEILING PANELS, BINS: PARTITIONS AND CURTAINS FOR OBVIOUS DAMAGE AND CONTAMINATION NOTE( I ) EXCEPTIONALLY, THE INTERVAL MAY BE EXTENDED TO 7 DAYS

220 240

ITEMS

SERVICE EXPERIENCE

I: 1 Z

ATA: 25 - 00

E2 HHI 737-700

SM

2 11-dec-01

Page 1 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

250000 14001

250000 15001

250000 22000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

CEILING PANELS FOR PROPER INSTALLATION NOTE( I ) EXCEPTIONALLY, THE INTERVAL MAY BE EXTENDED TO 7 DAYS

220 240

emp emp

empty

TOILETS FOR OBVIOUS DAMAGES AND CONTAMINATION NOTE( I ) EXCEPTIONALLY, THE INTERVAL MAY BE EXTENDED TO 7 DAYS

220 240

emp emp

empty

DIVIDER NET AND COVER, SEPARATION NET, DOOR PROTECTION NET 120 (NETS INCLUDING TENSION BUCKLE, TIE DOWN FITTINGS, ATTACHMENT 140 POINTS)

emp emp

empty

ITEMS

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

SERVICE EXPERIENCE

I: 1 Z

E1 HHI 737-700

SM

2 11-dec-01

SERVICE EXPERIENCE

I: 1 Z

E2 HHI 737-700

SM

2 11-dec-01

SERVICE EXPERIENCE

I: 7 DAY

E2 HHI 737-700

SM

2 11-dec-01

ATA: 25 - 00

Page 2 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 25 - 11

251100 20000

251100 20100

251111 20000

DESCRIPTION

ZONE ACCESS

STRUCTURE

TSK

EFF

R L ITEM BY E E REVISION P V DATE

FLIGHT COMPARTMENT SEATS INSPECT (DETAILED) THE CAPTAIN, FIRST OFFICER, FIRST OBSERVER, 210 AND SECOND OBSERVER (IF INSTALLED) SEAT HARNESSES, CROTCH STRAPS, AND SHOULDER BELTS (AS APPLICABLE) FOR WEAR, CONDITION, AND SECURITY.

emp

OPERATIONALLY CHECK THE CAPTAIN, FIRST OFFICER, AND THE FIRST 210 OBSERVER SEAT HARNESS INERTIA REELS.

emp

FUNCTIONALLY CHECK THE HORIZONTAL ADJUSTMENT HOLES IN THE 211 CAPTAIN AND FIRST OFFICERS SEAT TRACKS FOR ELONGATION AND 212 VERIFY THE CAPTAIN AND FIRST OFFICER SEAT TRACKS FOR WEAR, CONDITION, AND SECURITY.

emp emp

MPD MRB

25-020-00 MSI 25-020-00 RTE:8

AMTOSS

25-11-00-200-801

MPD MRB

25-030-00 MSI 25-030-00 RTE: 8

AMTOSS

25-11-00-200-801

MPD MPD MRB

25-010-01 25-010-02 MSI 25-010-01 RTE:5 MSI 25-010-02 RTE:5

MRB AMTOSS

Date: 23-jul-08

THRESHOLD INTERVAL

REFERENCES

ITEMS

25-11-11-200-801

I: 600 FLH

E3 HHI 737-700

4 22-mar-07

I: 3500 FLH

F1 HHI 737-700

2 03-jun-04

I: 4000 FLH

F2 HHI 737-700

1 03-jun-04

ATA: 25 - 11

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 25 - 22

252200 20000

252200 71000

252200 71100

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

PASSENGER COMPARTMENT SEATS INSPECT (DETAILED) THE PASSENGER SEAT BELTS W/O REMOVAL FOR WEAR, CONDITION, AND SECURITY.

220 230 240

OPERATIONALLY CHECK THE PASSENGER SEAT BREAK-OVER FEATURE 230 ON ALL SEATS ADJACENT (FORWARD AND AFT) TO ALL OF EMERGENCY 240 EXITS..

INSPECT (DETAILED) THE PASSENGER SEAT BACK RECLINE AND RECLINE 220 RESTRICTION MECHANISMS FOR CONDITION, SECURITY, AND PROPER 230 OPERATION. 240

emp emp emp

emp emp

emp emp emp

MPD MRB

25-040-00 MSI 25-040-00 RTE:8

AMTOSS

25-22-00-20

MPD MRB

25-050-00 MSI 25-050-00 RTE:8

AMTOSS

25-22-00-71

MPD MPD MRB

25-060-00 25-070-00 MSI 25-060-00 RTE:5 MSI 25-070-00 RTE:5

MRB AMTOSS

Date: 23-jul-08

THRESHOLD INTERVAL

ITEMS

25-22-00-71

I: 4000 FLH

E3 HHI 737-700

1 03-jun-04

I: 4000 FLH

F1 HHI 737-700

2 03-jun-04

I: 4000 FLH

E3 HHI 737-700

2 03-jun-04

ATA: 25 - 22

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 25 - 25

252512 20000

252512 71000

252512 71200

DESCRIPTION

ZONE ACCESS

STRUCTURE

TSK

EFF

R L ITEM BY E E REVISION P V DATE

CABIN ATTENDANT SEATS INSPECT (DETAILED) THE ATTENDANT SEAT HARNESS W/O REMOVAL FOR WEAR, CONDITION, AND SECURITY.

INSPECT (DETAILED) THE ATTENDANT SEAT BOTTOMS FOR PROPER RETRACTION, CONDITION, AND SECURITY.

221 241

221 241

OPERATIONALLY CHECK THE ATTENDANT SEAT HARNESS INERTIA REEL 221 LOCK FEATURE AND THE INERTIA REEL. 241

emp emp

emp emp

emp emp

MPD MRB

25-090-00 MSI 25-090-00 RTE:8

AMTOSS

25-25-12-200-801

MPD MRB

25-080-00 MSI 25-080-00 RTE:5

AMTOSS

25-25-12-710-801

MPD MPD MRB

25-100-00 25-110-00 MSI 25-100-00 RTE:8 MSI 25-110-00 RTE:8

MRB AMTOSS

Date: 23-jul-08

THRESHOLD INTERVAL

REFERENCES

ITEMS

25-25-12-710-802

I: 4000 FLH

E3 HHI 737-700

2 03-jun-04

I: 4000 FLH

E3 HHI F1 737-700

1 03-jun-04

I: 4000 FLH

F1 HHI 737-700

3 03-jun-04

ATA: 25 - 25

Page 1 of 1


HHI R E V

ITEM 25 - 40

R

737-6

MAINTENANCE SCHEDULE

254008 00000

DESCRIPTION

ZONE ACCESS

STRUCTURE

TSK

EFF

R L ITEM BY E E REVISION P V DATE

LAVATORIES OPERATIONALLY CHECK THE LAVATORY WASTE COMPARTMENT 221 FLAPPER DOOR SPRING. INSPECT (DETAILED) THE LAVATORY WASTE 241 COMPARTMENT FLAPPER DOOR AND THE LAVATORY WASTE 242 COMPARTMENT ACCESS DOOR LATCHING MECHANISM FOR WEAR, CONDITION AND SECURITY. NOTE( I ) INSPECT THE WASTE RECEPTACLES PER AD 74-08-09 AT AN INTERVAL NOT TO EXCEED 1000 HOURS

emp emp emp

AAR MPD MPD MRB MRB

R

Date: 23-jul-08

THRESHOLD INTERVAL

REFERENCES

AMTOSS

ITEMS

AD 74-08-09 REV. 02 25-120-00 25-130-00 MSI 25-120-00 RTE:8 MSI 25-130-00 RTE:8 25-40-08-20

I: 1000 FLH

ATA: 25 - 40

E3 HHI F1 737-700

4 23-jul-08

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 25 - 52

255200 20000

255200 20100

255200 21000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

CARCO COMPARTMENT LINING INSPECT THE STA 396 BULKHEAD PANELS FOR CONDITION AND SECURITY.

121 122

emp emp

MPD MRB

25-140-00 MSI 25-140-00 RTE:8

AMTOSS

25-52-00-20

INSPECT (GENERAL VISUAL) THE CARGO COMPARTMENT FLOOR, CEILING 121 AND SIDEWALL PANELS / LINERS FOR HOLES / TEARS, CONDITION AND 122 SECURITY. 141 142 822

821 emp emp emp emp

MPD MRB

25-160-00 MSI 25-160-00 RTE:8

AMTOSS

25-52-00-20

INSPECT THE CARGO DOOR RESTRAINT SYSTEM FOR CONDITION AND 121 SECURITY. 122 141 142

emp 821 emp 822

MPD MRB

25-170-00 MSI 25-170-00 RTE:9

AMTOSS

25-52-00-21

ITEMS

I: 450 CYC

E2 HHI 737-700

2 03-jun-04

I: 300 CYC

E2 HHI 737-700

3 18-mar-05

I: 4000 CYC

E1 HHI 737-700

2 22-mar-07

ATA: 25 - 52

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

25 - 61

ESCAPE STRAPS AND LANYARDS AND ESCAPE SLIDES (DOOR MOUNTED)

256110 20000

ZONE ACCESS

OPERATIONALLY CHECK THE LEFT AND RIGHT EMERGENCY EXIT HATCH 231 ESCAPE STRAP. 232 emp

STRUCTURE

emp 833 843

REFERENCES

MPD MPD MRB MRB

256110 71000

INSPECT (DETAILED) THE LEFT AND RIGHT EMERGENCY EXIT HATCH ESCAPE STRAP FOR CONDITION AND SECURITY.

231 232 emp

emp 833 843

256110 71100

Date: 23-jul-08

INSPECT (DETAILED) THE FLIGHT COMPARTMENT ESCAPE LANYARDS 211 (2) FOR CONDITION AND SECURITY. 212

emp emp

ITEMS

TSK

EFF

R L ITEM BY E E REVISION P V DATE

25-180-01 25-180-02 MSI 25-180-01 RTE:8 MSI 25-180-02 RTE:8

AMTOSS AMTOSS

25-61-10-71 25-61-10-20

MPD MPD MRB

25-190-01 25-190-02 MSI 25-190-01 RTE:8 MSI 25-190-02 RTE:8

MRB

THRESHOLD INTERVAL

AMTOSS AMTOSS

25-61-10-20 25-61-10-71

MPD MRB

25-210-00 MSI 25-210-00 RTE:8

AMTOSS AMTOSS

25-61-10-21 25-61-10-20

I: 10 YRS

F1 HHI 737-700

3 05-sep-06

I: 10 YRS

E3 HHI 737-700

3 05-sep-06

I: 10 YRS

E3 HHI 737-700

1 03-jun-04

ATA: 25 - 61

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 25 - 62

256299 00001

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

OVER-WATER SURVIVAL EQUIPMENT (OPTIONAL) CHECK THE EXPIRATION DATE OF THE FLIGHT CREW LIFE VEST (P/N 200 63600-505) AND PASSENGER LIFE VESTS (ADULT: P/N 63600-105, P/N 0723E105P, CHILD: P/N 216200-0, P/N 208511-1). IF THE EXPIRATION DATE IS LESS THAN 12 MONTH INFORM HHI-ENGINEERING FOR REPLACEMENT DISPOSITION. NOTE: EXPIRATION DATE FOR VACUUM SEALED LIFE VESTS IS MANUFACTURING DATE PLUS 120 MTH , EXPIRATION DATE FOR NON-VACUUM SEALED LIFE VESTS IS MANUFACTURING DATE PLUS 60 MONTH.

emp

empty

MS MS

ITEMS

CM2560 00020 CM2560 00030 SERVICE EXPERIENCE

I: 12 MTH

ATA: 25 - 62

S

HHI 737-700

0 23-jul-08

Page 1 of 1


HHI R E V

ITEM 25 - 64 256400 21000

256400 71100

256400 71200

256401 21000

R

737-6

MAINTENANCE SCHEDULE

256401 71000

DESCRIPTION

ZONE ACCESS

STRUCTURE

TSK

EFF

R L ITEM BY E E REVISION P V DATE

DETACHABLE EMERGENCY EQUIPMENT VISUALLY CHECK THE LIFE RAFT PRESSURE BOTTLE FOR PROPER PRESSURE.

OPERATIONALLY CHECK THE POWER MEGAPHONES.

REPLACE THE POWER MEGAPHONE BATTERIES AT THE MANUFACTURER'S RECOMMENDED INTERVAL.

221 241

221 241

221 241

VISUALLY CHECK ALL DETACHABLE EMERGENCY EQUIPMENT (GLOVES, 221 SMOKE GOGGLES, CRASH AXE, FLASH LIGHTS, FIRST AID KITS, AND 241 MEDICAL KITS AS APPLICABLE) FOR CONDITION AND PRESENCE.

OPERATIONALLY CHECK THE EMERGENCY FLASH LIGHTS. NOTE( I ) AT VENDOR RECOMMENDATION

221 241

emp emp

emp emp

emp emp

emp emp

emp emp

R

Date: 23-jul-08

THRESHOLD INTERVAL

REFERENCES

ITEMS

MPD MRB

25-310-00 MSI 25-310-00 RTE:8

AMTOSS

25-64-00-21

MPD MRB

25-330-00 MSI 25-330-00 RTE:9

AMTOSS

25-64-00-71

MPD MRB

25-340-00 MSI 25-340-00 RTE:9

AMTOSS

25-64-00-900

MPD MRB

25-370-00 MSI 25-370-00 RTE:8

AMTOSS

25-64-00-21

MPD MRB

25-380-00 MSI 25-380-00 RTE:9

AMTOSS AMTOSS AMM AMM

25-64-00-20 25-64-00-71 25-64-00-200-802 25-64-00-200-803

I: 15 MTH

E2 HHI 737-700

1 03-jun-04

I: 18 MTH

F1 HHI 737-700

2 30-nov-05

I: 18 MTH

S

HHI 737-700

0 30-nov-05

I: 2 YRS

E2 HHI 737-700

1 03-jun-04

I: 18 MTH

F1 HHI 737-700

2 23-jul-08

ATA: 25 - 64

Page 1 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

256402 90000

256403 20000

256404 90000

256405 90000

Date: 23-jul-08

DESCRIPTION REPLACE THE EMERGENCY FLASH LIGHT BATTERIES. NOTE( I ) VENDOR RECOMMENDATION

ZONE ACCESS 200

STRUCTURE

emp

PROTECTIVE BREATHING EQUIPMENT (SMOKE HOODS) - VENDOR: SCOTT. 221 CHECK FOR CONDITION OF BOX AND ATTACHMENTS. REPLACE IF 241 DAMAGED, CLEAN IF NECESSARY. CHECK FOR EXPIRATION DATE. EXPIRATION DATE IS MANUFACTURE DATE + 10 YEARS. NOTE( M ) IF EXPIRATION DATE IS REACHED DURING NEXT 20 MONTHS, INFORM HHI-ENGINEERING FOR REPLACEMENT DISPOSITION!

emp emp

CHECK THE FIRST AID KITS FOR COMPLETENESS AND THE EXPIRY DATES 221 OF ITS CONTENT. IF ANY EXPIRATION DATE IS LESS THAN 6 MONTHS, 241 INFORM HHI-ENGINEERING FOR REPLACEMENT DISPOSITION. NOTE( I ) VENDOR RECOMMENDATION

emp emp

CHECK DOCTOR'S KIT (VENDOR MEDIFAN) EXPIRY DATE NOTED ON SEAL. 221 IF THE EXPIRATION DATE IS LESS THAN 6 MONTH INFORM 241 HHI-ENGINEERING FOR DISPLACEMENT DISPOSITION. NOTE( I ) VENDOR RECOMMENDATION (IF INSTALLED)

emp emp

ITEMS

THRESHOLD INTERVAL

REFERENCES MPD MRB

25-390-00 MSI 25-390-00 RTE:9

AMTOSS

25-64-00-90

MPD MRB

25-400-00 MSI 25-400-00 RTE:8

AMTOSS

25-64-00-200-801

MPD MRB

25-420-00 MSI 25-420-00 RTE:8

AMTOSS

25-64-00-90

MPD MRB

25-430-00 MSI 25-430-00 RTE:8

AMTOSS

25-64-00-90

TSK

EFF

R L ITEM BY E E REVISION P V DATE

I: 2 YRS

S

HHI 737-700

2 30-nov-05

I: 24 MTH

S

HHI 737-700

4 22-mar-07

I: 6 MTH

S

HHI 737-700

2 23-jul-08

I: 6 MTH

S

HHI 737-700

2 23-jul-08

ATA: 25 - 64

Page 2 of 2


HHI R E V

ITEM 25 - 66 256600 71000

256601 00000

256601 20000

D

737-6

MAINTENANCE SCHEDULE

256601 40000

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

EFF

R L ITEM BY E E REVISION P V DATE

DOOR-MOUNTED ESCAPE SYSTEM OPERATIONALLY CHECK, ON A SAMPLING BASIS, ONE DIFFERENT ESCAPE SLIDE DOOR UNTIL 10% OF ALL THE DOORS IN THE FLEET ARE COMPLETE WITHIN 12 YEARS. NO PARTICULAR DOOR CAN BE TESTED MORE THAN ONCE WITHIN THIS 12 YEAR PERIOD. CONTINUING MAINTENANCE REQUIREMENTS ARE TO BE DETERMINED BY EACH OPERATOR AND REGULATORY AGENCY.

221 222 241 242

831 834 841 844

MPD MRB

25-220-00 MSI 25-220-00 RTE:8

AMTOSS

25-66-00-71

VISUALLY CHECK THE EMERGENCY ESCAPE SLIDE PRESSURE BOTTLES 231 FOR PROPER PRESSURE 232 241 242

emp emp emp emp

MPD MRB

25-250-00 MSI 25-250-00 RTE:8

AMTOSS

25-66-01-20

INSPECT (DETAILED) THE ENTRY AND SERVICE DOOR EMERGENCY ESCAPE SYSTEM (AT ALL 4 DOORS) INCLUDING THE DOOR OPENINGS, THE EMERGENCY ESCAPE SLIDE COMPARTMENTS AND THE ESCAPE SLIDE COMPONENTS WITHOUT REMOVING THE ESCAPE SLIDE FOR CONDITION AND SECURITY.

831 834 841 844

MPD MRB

25-230-00 MSI 25-230-00 RTE:8

AMTOSS

25-66-01-20

221 222 241 242

I: 3 YRS

F1 HHI 737-700

3 30-nov-05

I: 90 DAY

E1 HHI 737-700

4 22-mar-07

I: 2 YRS

E3 HHI 737-700

1 03-jun-04

ITEM DELETED.

D

Date: 23-jul-08

TSK

2 23-jul-08

ITEMS

ATA: 25 - 66

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 25 - 71

257100 21000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

ACCESSORY COMPARTMENTS INSPECT THE ELECTRONIC COMPARTMENT MOISTURE SHROUDS FOR 117 OBVIOUS CRACKS/TEARS, CLOGGED DRAINS, CONDITION AND SECURITY. 118

emp emp

ITEMS

MPD MRB

25-150-00 MSI 25-150-00 RTE:9

AMTOSS

25-71-00-21

I: 2 YRS

ATA: 25 - 71

E1 HHI 737-700

1 03-jun-04

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 26 26 - 00

260000 01000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

FIRE PROTECTION FIRE EXTINGUISHING SYSTEM VISUALLY CHECK THAT ALL PORTABLE FIRE EXTINGUISHERS, HALON 200 AND WATER ARE ON BOARD, PROPERLY STOWED, HANDLES SAFETIED AND THE POINTER OF THE PRESSURE GOUGE, IF INSTALLED, IS WITHIN THE GREEN RANGE.

emp

empty

AAR AAR AAR

ITEMS

NFL II 139/99 NFL II 96/79 NFL II 92/99

I: 1 Z

ATA: 26 - 00

E1 HHI 737-700

FC

1 13-apr-00

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 26 - 14

261400 73000

261401 10000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

LAVATORY SMOKE DETECTION OPERATIONAL CHECK OF THE LAVATORY SMOKE DETECTORS.

RESTORE LAVATORY SMOKE DETECTOR GRILL BY CLEANING.

221 241 242

221 241 242

emp emp emp

emp emp emp

ITEMS

MPD MRB

26-010-00 MSI 26-010-00 RTE:8

AMTOSS

26-14-00-73

MPD MRB

26-020-00 MSI 26-020-00 RTE:9

AMTOSS

26-14-01-10

I: 6000 FLH

F1 HHI 737-700

3 18-mar-05

I: 6000 FLH

S

3 18-mar-05

ATA: 26 - 14

HHI 737-700

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 26 - 15

261500 71000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

APU FIRE DETECTION SYSTEM OPERATIONAL CHECK OF THE APU REMOTE FIRE DETECTION SYSTEM 117 (M279 FIRE DETECTION CONTROL MODULE AND P28 REMOTE APU 134 CONTROL PANEL). 210

117A emp emp

ITEMS

MPD MRB

26-030-00 MSI 26-030-00 RTE:8

AMTOSS

26-15-00-71

I: 12000 FLH

ATA: 26 - 15

F1 HHI 737-700

6 22-mar-07

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 26 - 20

262000 01000

262000 02000

262000 21000

262001 72000

262001 72100

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

FIRE EXTINGUISHING SYSTEM CHECK ENGINE FIRE EXTINGUISHER SQUIBS FOR EXPIRATION DATE IS 133 REACHED DURING THE NEXT 6 MONTH, REPLACE THE SQUIB. THE EXPIRATION DATE IS THE MANUFACTURING DATE PLUS THE LIFE LIMIT. THE MANUFACTURING DATE IS STAMPED ON THE HEXHEAD OF THE SQUIB. THE LIFE LIMIT IS SHOWN IN THE CMS.

emp

CHECK APU FIRE EXTINGUISHER SQUIBS FOR EXPIRATION DATE. IF THE 311 EXPIRATION DATE IS REACHED DURING THE NEXT 6 MONTH, REPLACE THE SQUIB. THE EXPIRATION DATE IS THE MANUFACTURING DATE PLUS THE LIFE LIMIT. THE MANUFACTURING DATE IS STAMPED ON THE HEXHEAD OF THE SQUIB. THE LIFE LIMIT IS SHOWN IN THE CMS.

311BL

VISUALLY CHECK ENGINE FIRE BOTTLES PRESSURE GAUGE FOR CORRECT PRESSURE (AND APU FIRE BOTTLE PRESSURE GAUGE IF INSTALLED).

emp 311BL

133 311

OPERATIONAL CHECK OF ENGINE FIRE EXTINGUISHER SYSTEM CHECK 133 VALVES FOR FREEDOM OF MOVEMENT. NOTE( I ) AT BOTTLE CHANGE

emp

FUNCTIONAL CHECK THE ENGINE FIRE EXTINGUISHER DISTRIBUTION SYSTEM (PRESSURE CHECK).

emp 413 414 415 416 423 424 425 426

133 411 emp emp emp 421 emp emp emp

ITEMS

MPD MRB

26-070-00 MSI 26-070-00 RTE:8

AMTOSS AMTOSS MS AMM

26-21-02-40 26-21-02-00 CM2621 00020 26-21-00

MPD MRB

26-210-00 MSI 26-210-00 RTE:8

AMTOSS AMTOSS MS AMM

26-22-02-40 26-22-02-00 CM2622 00020 26-22-00

MPD MRB

26-050-00 MSI 26-050-00 RTE:8

AMTOSS

26-20-00-21

MPD MRB

26-090-00 MSI 26-090-00 RTE:8

AMTOSS

26-21-00-720-801

MPD MRB

26-150-00 MSI 26-150-00 RTE:8

AMTOSS

26-21-00-730-803

I: 6 MTH

E1 HHI 737-700

3 03-jun-04

I: 6 MTH

E1 HHI 737-700

4 03-jun-04

I: 1800 FLH

E1 HHI 737-700

5 25-apr-06

I: 6000 FLH

F1 HHI 737-700

5 18-mar-05

I: 6000 FLH

F2 HHI 737-700

3 03-jun-04

ATA: 26 - 20

Page 1 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

262001 72200

262001 73000

262002 21000

262003 21000

Date: 23-jul-08

DESCRIPTION GENERAL VISUAL INSPECTION OF ENGINE FIRE EXTINGUISHER DISTRIBUTION SYSTEM.

ZONE ACCESS

STRUCTURE

133 411 emp emp emp 421 emp emp emp

emp 413 414 415 416 423 424 425 426

MPD MRB

26-170-00 MSI 26-170-00 RTE:8

AMTOSS

26-21-01-21

FUNCTIONALLY TEST THE ENGINE AND APU FIRE CONTROL MODULE. THE FUNCTIONAL CHECK INCLUDES CHECKOUT OF THE FOLLOWING: ENGINE: - FUEL SHUTOFF VALVE - HYDRAULIC SUPPLY SHUTOFF VALVE - BLEED AIR VALVE - GENERATOR CONTROL RELAY - THRUST REVERSER VALVE, SQUIB FIRING CIRCUITS - FIRE HANDLE LOCK OVERRIDE APU: - FUEL SHUTOFF VALVE - GENERATOR CONTROL RELAY - SQUIB FIRING CIRCUITS - FIRE HANDLE LOCK OVERRIDE - P28 REMOTE APU CONTROL PANEL

133 134 210 212 311 emp 411 421

emp emp emp emp 311BL 315A 415 425

MPD MPD MPD MPD MRB

26-080-00 26-110-00 26-220-00 26-230-00 MSI 26-080-00 RTE:8 MSI 26-110-00 RTE:8 MSI 26-220-00 RTE:8 MSI 26-230-00 RTE:8

PERFORM A GENERAL VISUAL INSPECTION OF THE APU REMOTE CONTROL PANEL. CHECK FOR CONDITION AND SECURITY OF INSTALLATION.

134

MRB MRB MRB

PERFORM A DETAILED VISUAL INSPECTION OF THE APU FIRE 311 EXTINGUISHER DISTRIBUTION SYSTEM AND APU FIRE BOTTLE. 315 CHECK FOR CONDITION, SECURITY OF INSTALLATION, KINKED, CRACKED AND OBSTRUCTED TUBING.

emp

311BL 315A

ITEMS

THRESHOLD INTERVAL

REFERENCES

AMTOSS AMTOSS AMTOSS AMTOSS

26-21-00-730-801 25-21-00-720-802 26-22-00-730-801 26-22-00-720-801

MPD MRB

26-250-00 MSI 26-250-00 RTE:8

AMTOSS

26-22-03-21

MPD MRB

26-280-00 MSI 26-280-00 RTE:8

AMTOSS

26-22-01-21

TSK

EFF

R L ITEM BY E E REVISION P V DATE

I: 6000 FLH

E2 HHI 737-700

2 03-jun-04

I: 6000 FLH

F2 HHI 737-700

7 05-sep-06

I: 6000 FLH

E2 HHI 737-700

2 03-jun-04

I: 6000 FLH

E3 HHI 737-700

4 03-jun-04

ATA: 26 - 20

Page 2 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 26 - 23

262300 00650

262300 01000

262300 02000

262300 03000

262300 04000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

EXTINGUISHING SYSTEM - CARGO COMPARTMENT CHECK THE EXPIRATION DATE OF THE FIRE EXTINGUISHER SQUIBS. 125 EXPIRATION DATE IS THE MANUFACTURING DATE PLUS 10 YEARS. 126 MANUFACTURING DATE IS STAMPED ON THE HEX FLAT OF THE SQUIB. IF THE EXPIRATION TIME IS LESS THAN 6 MONTH, REPLACE SQUIB. ACCESS REMOVAL OF AIR CONDITIONING DUCTING MAY BE REQUIRED.

121HW emp

OPERATIONALLY CHECK THE CARGO FIRE EXTINGUISHING ARM AND DISCHARGE SWITCHES TO VERIFY CIRCUITRY. ACCESS SPECIAL ACCESS REQUIRED REMOVAL OF AIR CONDITIONING DUCTING MAY BE REQUIRED.

125 126 210

121HW emp emp

FUNCTIONALLY CHECK THE CARGO FIRE EXTINGUISHING 60-MINUTE TIMER. NOTE( J ) IF SECOND HALON BOTTLE INSTALLED ACCESS SPECIAL ACCESS REQUIRED REMOVAL OF AIR CONDITIONING DUCTING MAY BE REQUIRED.

125 126 210

REPLACE THE CARGO COMPARTMENT FIRE EXTINGUISHER SYSTEM (FILTER/DRYER) NOTE( I ) AT FIRE EXTINGUISHER BOTTLE DISCHARGE ACCESS SPECIAL ACCESS REQUIRED REMOVAL OF AIR CONDITIONING DUCTING MAY BE REQUIRED.

121 125 126

FUNCTIONALLY CHECK THE CARGO FIRE EXTINGUISHER DISTRIBUTION SYSTEM (PRESSURE CHECK). ACCESS REMOVAL OF AIR CONDITIONING DUCTING MAY BE REQUIRED

121 122 125 141 142 145 146

121HW emp emp

121HW emp emp

121HW emp emp emp emp emp emp

ITEMS

MPD MRB

26-330-00 MSI 26-330-00 RTE:8

AMTOSS AMTOSS

26-23-02-000-801 26-23-02-400-801

MPD MRB

26-370-00 MSI 26-370-00 RTE:8

AMTOSS AMTOSS

26-23-00-730-801 26-23-00-730-802

MPD MRB

26-400-00 MSI 26-400-00 RTE:8

AMTOSS

26-23-00-730-801

MPD MRB

26-390-00 MSI 26-390-00 RTE:8

AMTOSS AMTOSS

26-23-04-40 26-23-04-00

MPD MRB

26-340-00 MSI 26-340-00 RTE:8

AMTOSS AMTOSS

26-23-00-73 26-23-00-72

I: 6 MTH

E1 HHI 737-700

2 05-sep-06

I: 6000 FLH

F1 HHI 737-700

6 05-sep-06

I: 6000 FLH

F2 HHI 737-700

6 05-sep-06

I: 1 s.N

S

HHI 737-700

5 05-sep-06

I: 12000 FLH

F2 HHI 737-700

4 22-mar-07

ATA: 26 - 23

Page 1 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

262300 05000

Date: 23-jul-08

DESCRIPTION FUNCTIONALLY CHECK THE CARGO FIRE EXTINGUISHER BOTTLE PRESSURE SWITCH. NOTE( I ) AT HYDROSTATIC TEST. ACCESS REMOVAL OF AIR CONDITIONING DUCTING MAY BE REQUIRED.

ZONE ACCESS 125 126

STRUCTURE

121HW emp

ITEMS

REFERENCES MPD MRB

26-360-00 MSI 26-360-00 RTE:9

AMTOSS

26-23-00-73

THRESHOLD INTERVAL

I: 1 s.N

ATA: 26 - 23

TSK

EFF

F2 HHI 737-700

R L ITEM BY E E REVISION P V DATE

3 05-sep-06

Page 2 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 26 - 24

262401 00000

262401 01000

262401 90000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

LAVATORY WASTE COMPARTMENT FIRE EXTINGUISHING DETAILED VISUAL INSPECTION OF THE LAVATORY FIRE BOTTLE FUSIBLE 221 TIPS AND DISCHARGE TUBES 241 242

VISUAL CHECK OF LAVATORY WASTE COMPARTMENT TEMPERATURE 221 INDICATOR STRIP FOR HEAT EXPOSURE. 241 242

REMOVE LAVATORY FIRE BOTTLE FOR WEIGHT CHECK. NOTE( I ) VENDOR RECOMMENDATION

221 241 242

emp emp emp

emp emp emp

emp emp emp

ITEMS

MPD MRB

26-300-00 MSI 26-300-00 RTE:9

AMTOSS

26-24-01-20

MPD MRB

26-320-00 MSI 26-320-00 RTE:9

AMTOSS

26-24-01-21

MPD MRB

26-290-00 MSI 26-290-00 RTE:9

AMTOSS

26-24-01-90

I: 3600 FLH

E3 HHI 737-700

4 25-apr-06

I: 1200 FLH

E1 HHI 737-700

4 25-apr-06

I: 5 YRS

S

3 03-jun-04

ATA: 26 - 24

HHI 737-700

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 26 - 25

262500 01000

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

PORTABLE FIRE EXTINGUISHER CHECK THAT ALL PORTABLE FIRE EXTINGUISHERS ARE PROPERLY 200 STOWED, HANDLES SAFETIED, PRESSURE GAUGE (IF INSTALLED) IS IN GREEN RANGE AND THE INSCRIBTION IS LEGIBLE. VISUALLY INSPECT THE STOWAGE BRACKET FOR CONDITION AND SECURITY OF INSTALLATION. REMOVE THE CONTROL AND PASSENGER CABIN FIRE EXTINGUISHERS FOR WEIGHT CHECK. NOTE( J ) THIS INCLUDES ALL TYPES OF PORTABLE FIRE EXTINGUISHERS.

emp

MPD MPD MPD MPD MRB MRB MRB MRB AAR AAR AAR AMM

Date: 23-jul-08

THRESHOLD INTERVAL

ITEMS

26-450-00 26-470-00 26-490-00 26-510-00 MSI 26-450-00 RTE:8 MSI 26-470-00 RTE:8 MSI 26-490-00 RTE:8 MSI 26-510-00 RTE:8 NFL II 139/99 NFL II 96/79 NFL II 92/99 26-26-01

I: 12 MTH

ATA: 26 - 25

E3 HHI 737-700

4 03-jun-04

Page 1 of 1


HHI R E V

ITEM 27 27 - 00

R

737-6

MAINTENANCE SCHEDULE

270000 00000

DESCRIPTION

ZONE ACCESS

STRUCTURE

LUBRICATE THE STABILIZER TRIM ACTUATOR AND ACTUATOR GIMBAL 311 PINS AND BALLNUT. 312

311BL emp

MPD MRB

R L ITEM BY E E REVISION P V DATE

LUBRICATE THE LEFT AND RIGHT WING FLAP TRANSMISSION UNIVERSAL JOINTS AND BALLSCREW ACTUATORS. ACCESS FLAPS DEPLOYED

27-102-00 MSI 27-102-00 RTE:6 MSI 27-102-00 RTE:8

SB AMTOSS

737-27A1277 R1 12-22-41-600-801 27-144-00 27-146-00 MSI 27-144-00 RTE:6 MSI 27-146-00 RTE:6

133 134 210 541 542 543 544 553 641 642 643 644 653

emp emp emp emp emp emp emp emp emp emp emp emp emp

MPD MPD MRB

AMTOSS AMTOSS AMTOSS AMTOSS

12-22-51-640-805 12-22-51-640-804 12-22-51-640-803 12-22-51-640-802

LUBRICATE THE #4 AND #5 FLAP TRANSMISSION ANGLE/TEE GEARBOX 133 UNIVERSAL JOINTS. 134 553 653

emp emp emp emp

MPD MPD MRB

27-152-01 27-152-02 MSI 27-152-01 RTE:6 MSI 27-152-02 RTE:6

MRB

MRB AMTOSS

Date: 23-jul-08

EFF

GENERAL

R

270000 02000

TSK

FLIGHT CONTROL

MRB

270000 01000

THRESHOLD INTERVAL

REFERENCES

ITEMS

12-22-51-640-806

I: 1600 FLH I: 8 MTH

S

HHI 737-700

8 23-jul-08

I: 1000 CYC

S

HHI 737-700

4 03-jun-04

I: 12 MTH I: 2000 CYC

S

HHI 737-700

4 03-jun-04

ATA: 27 - 00

Page 1 of 10


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

270000 03000

270000 04000

Date: 23-jul-08

DESCRIPTION LUBRICATE THE LEFT AND RIGHT TRAILING EDGE FLAP ACTUATION MECHANISM. ACCESS FLAPS DEPLOYED

LUBRICATE THE RIGHT AND LEFT WING AILERON MECHANICAL CONTROL PATH AND AILERON POWER CONTROL UNITS. NOTE( R ) ACCOMPLISH THE LUBRICATION OF THE AILERON TAB HINGES IN ACCORDANCE WITH AD 2006-21-01 AND SB 737-27-1273 (EO 154339).

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

133 134 emp 541 542 543 544 553 561 567 641 642 643 644 653 661 667

emp 194BL 194BR emp emp emp emp emp emp emp emp emp emp emp emp emp emp

MPD MPD MRB

AMTOSS AMTOSS AMTOSS AMTOSS AMTOSS AMTOSS

12-22-51-640-811 12-22-51-640-812 12-22-51-640-813 12-22-51-640-814 12-22-51-640-815 12-22-51-640-816

133 134 572 emp emp emp emp emp 672 emp emp emp emp emp

571BB 671BB 572AB 572CB 572DB 572FB 572GB 572HB 672AB 672CB 672DB 672FB 672GB 672HB

MPD MPD MRB

27-026-01 27-026-02 MSI 27-026-01 RTE:6 MSI 27-026-01 RTE:8 MSI 27-026-02 RTE:6

ITEMS

MRB

MRB MRB AAR EO SB AMTOSS AMTOSS AMTOSS AMTOSS AMTOSS

TSK

EFF

R L ITEM BY E E REVISION P V DATE

27-170-01 27-170-02 MSI 27-170-01 RTE:6 MSI 27-170-02 RTE:6

AD 2006-21-01 154339 737-27-1273 12-22-11-640-804 12-22-11-640-803 12-22-11-640-802 12-22-11-600-801 12-22-11-640-801

I: 8 MTH I: 1250 CYC

S

HHI 737-700

6 03-jun-04

I: 4000 FLH I: 12 MTH

S

HHI 737-700

6 22-mar-07

ATA: 27 - 00

Page 2 of 10


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

270000 05000

270000 06000

DESCRIPTION

ZONE ACCESS

LUBRICATE THE LEFT WING #S 1, 2 AND 3 AND THE RIGHT WING #S 6, 7 542 AND 8 TRAILING EDGE FLAP TRACK FORWARD ATTACHMENT POINT PINS. 543 544 642 643 644

LUBRICATE THE LEFT WING #4 AND THE RIGHT WING #5 INBOARD FLAP 553 TRACK ATTACHMENT FITTINGS. 653

STRUCTURE

542AB 543AB 544AB 642AB 643AB 644AB

emp emp

MPD MPD MRB MRB

Date: 23-jul-08

LUBRICATE THE SPOILER MIXER, THE LEFT WING AND RIGHT WING SPOILER MECHANICAL CONTROL PATH. ACCESS FLAPS DEPLOYED

134 552 562 563 564 565 566 652 662 663 664 665 666

emp emp emp emp emp emp emp emp emp emp emp emp emp

12-22-51-640-816 12-22-51-640-815 12-22-51-640-814

MPD MPD MRB

27-176-01 27-176-02 MSI 27-176-01 RTE:5 MSI 27-176-02 RTE:5

ITEMS

AMTOSS

12-22-51-640-813

MPD MPD MPD MRB

27-182-00 27-182-01 27-182-02 MSI 27-182-00 RTE:6 MSI 27-182-01 RTE:6 MSI 27-182-02 RTE:6

MRB MRB AMTOSS AMTOSS AMTOSS

TSK

EFF

R L ITEM BY E E REVISION P V DATE

27-174-01 27-174-02 MSI 27-174-01 RTE:6 MSI 27-174-02 RTE:6

AMTOSS AMTOSS AMTOSS

MRB

270000 07000

THRESHOLD INTERVAL

REFERENCES

12-22-61-600-802 12-22-61-640-801 12-22-61-600-801

I: 4000 CYC

S

HHI 737-700

3 03-jun-04

I: 1000 CYC

S

HHI 737-700

3 03-jun-04

I: 4000 FLH

S

HHI 737-700

3 03-jun-04

ATA: 27 - 00

Page 3 of 10


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

270000 08000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

LUBRICATE THE LEFT AND RIGHT WING LEADING EDGE SLAT ROLLERS. 522 523 ACCESS 524 LEADING EDGES EXTENDED 525 emp emp emp emp emp emp emp 622 623 624 625 emp emp emp emp emp emp emp

STRUCTURE

emp emp emp 521CB 521FB 521JB 521MB 521QB 521TB 521WB 521ZB emp emp emp 621CB 621FB 621HB 621LB 621PB 621SB 621VB 621YB

ITEMS

THRESHOLD INTERVAL

REFERENCES MPD MPD MRB MRB AMTOSS

TSK

EFF

R L ITEM BY E E REVISION P V DATE

27-220-01 27-220-02 MSI 27-220-01 RTE:6 MSI 27-220-02 RTE:6 12-22-71-600-801

I: 1250 CYC I: 8 MTH

ATA: 27 - 00

S

HHI 737-700

5 03-jun-04

Page 4 of 10


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

270000 09000

270000 10000

270000 11000

DESCRIPTION

ZONE ACCESS

STRUCTURE

LUBRICATE THE LEFT AND RIGHT WING LEADING EDGE SLAT TRACKS. 522 523 ACCESS 524 LEADING EDGES EXTENDED 525 emp emp emp emp emp emp emp 622 623 624 625 emp emp emp emp emp emp emp

emp emp emp 521CB 521FB 521JB 521MB 521QB 521TB 521WB 521ZB emp emp emp 621CB 621FB 621HB 621LB 621PB 621SB 621VB 621YB

MPD MPD MRB

AMTOSS

12-22-71-640-801

LUBRICATE THE RUDDER FEEL AND CENTERING UNIT SPRING SLIDER. 211 212 324

emp emp 324CL

MPD MRB

27-040-00 MSI 27-040-00 RTE:5

AMTOSS

12-22-21-600-802

MPD MRB

27-046-00 MSI 27-046-00 RTE:8 MSI 27-046-00 RTE:9

LUBRICATE THE MAIN AND STANDBY RUDDER POWER CONTROL UNIT 324 ROD ENDS AND RUDDER HINGES.

324DL

MRB

MRB AMTOSS AMTOSS

Date: 23-jul-08

THRESHOLD INTERVAL

REFERENCES

ITEMS

TSK

EFF

R L ITEM BY E E REVISION P V DATE

27-222-01 27-222-02 MSI 27-222-01 RTE:6 MSI 27-222-02 RTE:6

12-22-21-640-801 12-22-21-600-801

I: 2500 CYC I: 16 MTH

S

HHI 737-700

6 03-jun-04

I: 6000 FLH

S

HHI 737-700

3 18-mar-05

I: 6000 FLH

S

HHI 737-700

4 18-mar-05

ATA: 27 - 00

Page 5 of 10


HHI

737-6

MAINTENANCE SCHEDULE

R E V

ITEM

R

270000 12000

R

270000 13000

DESCRIPTION LUBRICATE THE ELEVATOR MECHANICAL CONTROL PATH.

ZONE ACCESS 334 emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp 344

LUBRICATE THE FORWARD STABILIZER TRIM MECHANISM (STABILIZER 112 CHAIN AND FLEXIBLE SHAFT).

STRUCTURE

315A 333AT 333BB 333CB 333DB 333EB 334AB 334BB 334GB 334HB 334JB 334KB 334MB 334NB 343AT 343BB 343CB 343DB 343EB 344AB 344BB 344GB 344HB 344KB 344MB 344NB 344JB

MPD MRB

AMTOSS AMTOSS AMTOSS

12-22-31-640-802 12-22-31-640-801 12-22-31-600-801

112A

MPD MRB

27-104-00 MSI 27-104-00 RTE:6 MSI 27-104-00 RTE:9

MPD MRB

MRB AMTOSS

Date: 23-jul-08

THRESHOLD INTERVAL

REFERENCES

ITEMS

TSK

EFF

R L ITEM BY E E REVISION P V DATE

27-070-00 MSI 27-070-00 RTE:6 27-070-00 MSI 27-070-00 RTE:6

12-22-41-600-802

I: 6000 FLH

S

HHI 737-700

5 23-jul-08

I: 25000 FLH

S

HHI 737-700

2 03-jun-04

ATA: 27 - 00

Page 6 of 10


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

270000 14000

270000 15000

270000 16000

DESCRIPTION

ZONE ACCESS

CHECK FLAP POWER DRIVE UNIT OIL LEVEL AND SERVICE AS REQUIRED. 133 134

REPLACE THE FLAP POWER DRIVE UNIT OIL.

LUBRICATE LEFT AND RIGHT WING FLAP SKEW SENSOR MECHANISM. ACCESS FLAPS DEPLOYED

133 134

553 567 653 667

STRUCTURE

emp emp

emp emp

emp emp emp emp

MPD MRB

27-132-00 MSI 27-132-00 RTE:6

AMTOSS

12-22-51-610-801

MPD MRB

27-134-00 MSI 27-134-00 RTE:6

AMTOSS

12-22-51-610-802

MPD MPD MRB

27-136-01 27-136-02 MSI 27-136-01 RTE:6 MSI 27-136-02 RTE:6

MRB

270000 17000

LUBRICATE THE FLAP DRIVE TORQUE TUBES COUPLINGS AND TORQUE TUBE SUPPORTS. ACCESS FLAPS DEPLOYED

133 134 553 567 653 667

emp emp emp emp emp emp

AMTOSS AMTOSS AMTOSS AMTOSS

12-22-51-640-810 12-22-51-640-809 12-22-51-640-808 12-22-51-640-807

MPD MPD MRB

27-138-00 27-150-00 MSI 27-138-00 RTE:6 MSI 27-150-00 RTE:6

MRB AMTOSS

Date: 23-jul-08

ITEMS

THRESHOLD INTERVAL

REFERENCES

12-22-51-640-801

TSK

EFF

R L ITEM BY E E REVISION P V DATE

I: 5000 CYC

S

HHI 737-700

2 03-jun-04

I: 25000 CYC

S

HHI 737-700

2 03-jun-04

I: 24 MTH I: 4000 FLH

S

HHI 737-700

2 03-jun-04

I: 24 MTH I: 4800 CYC

S

HHI 737-700

5 22-mar-07

ATA: 27 - 00

Page 7 of 10


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

270000 18000

270000 19000

270000 20000

270000 21000

Date: 23-jul-08

DESCRIPTION CHECK THE LEFT AND RIGHT WING FLAP DRIVE TRANSMISSION OIL LEVEL AND SERVICE AS REQUIRED. ACCESS FLAPS DEPLOYED

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

133 134 210 541 542 543 544 641 642 643 644

emp emp emp emp emp emp emp emp emp emp emp

MPD MPD MRB

AMTOSS

12-22-51-610-803

REPLACE THE LEFT AND RIGHT WING FLAP DRIVE TRANSMISSION OIL. 133 134 ACCESS 211 FLAPS DEPLOYED 212 541 542 543 544 553 641 642 643 644 653

emp emp emp emp emp emp emp emp emp emp emp emp emp emp

MPD MPD MRB

27-142-01 27-142-02 MSI 27-142-01 RTE:6 MSI 27-142-01 RTE:8 MSI 27-142-02 RTE:6 MSI 27-142-02 RTE:8

AMTOSS

12-22-51-610-804

CHECK ALTERNATE FLAP DRIVE GEARBOX OIL LEVEL AND SERVICE AS 133 REQUIRED. 134

emp emp

MPD MRB

27-178-00 MSI 27-178-00 RTE:9

AMTOSS

12-22-51-610-805

MPD MRB

27-186-00 MSI 27-186-00 RTE:6

AMTOSS

12-22-81-600-801

LUBRICATE THE SPEEDBRAKE LEVER NO-BACK BRAKE.

112

112A

ITEMS

MRB MRB MRB

MRB MRB MRB

TSK

EFF

R L ITEM BY E E REVISION P V DATE

27-140-01 27-140-02 MSI 27-140-01 RTE:6 MSI 27-140-01 RTE:8 MSI 27-140-02 RTE:6 MSI 27-140-02 RTE:8 I: 5000 CYC

S

HHI 737-700

3 03-jun-04

I: 25000 CYC

S

HHI 737-700

2 03-jun-04

I: 6000 FLH

S

HHI 737-700

3 18-mar-05

I: 6000 FLH

S

HHI 737-700

3 18-mar-05

ATA: 27 - 00

Page 8 of 10


HHI R E V

R

737-6

MAINTENANCE SCHEDULE DESCRIPTION

270000 22000

PERFORM A DETAIL VISUAL INSPECTION OF ALL EXPOSED PORTIONS OF THE FLIGHT CONTROL CABLES RUNS. ACCESS EXTEND FLAPS

133 134 210 550 emp 561 571 660 emp 661 671

emp emp emp 551CT 551DB emp 571BB 651CT 651DB emp 671BB

MPD MRB

27-226-00 MSI 27-226-00 RTE:6

AMTOSS AMTOSS AMTOSS

20-20-31-200-805 20-20-31-200-802 20-20-31-200-801

PERFORM A DETAIL VISUAL INSPECTION OF ALL INTERNAL PORTIONS OF THE FLIGHT CONTROL CABLE RUNS. ACCESS PASSENGER CABIN FLOOR PANELS BETWEEN B.S. 663.75 AND B.S. 727 FORWARD CARGO COMPARTMENT AFT BULKHEAD. FORWARD CARGO COMPARTMENT CEILING PANELS OR FLOOR PANELS BETWEEN B.S.396 TO B.S. 540. AFT CARGO COMPARTMENT CEILING PANELS AFT CARGO COMPARTMENT AFT BULKHEAD PANELS AND WATER TANK, OR THE PRESSURIZATION AFT OUTFLOW VALVE ASSEMBLY.

112 113 emp emp 114 emp emp 117 118 121 122 125 126 137 138 141 142 145 146 300 311 312 313 314 317 318 323

112A 113AC 113AW 113BW 114AC 114AW 114BW 117A emp 821 emp emp emp emp emp 822 emp emp emp emp 311BL emp emp emp 317AL 318BR 323FL

MPD MRB

27-228-00 MSI 27-228-00 RTE:6

AMTOSS AMTOSS AMTOSS

20-20-31-200-802 20-20-31-200-805 20-20-31-200-801

270000 25000

R

Date: 23-jul-08

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

ITEM

ITEMS

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

I: 4800 CYC I: 24 MTH

E3 HHI 737-700

6 23-jul-08

I: 21600 CYC I: 6 YRS

E3 HHI 737-700

5 23-jul-08

ATA: 27 - 00

Page 9 of 10


HHI R E V

ITEM

DESCRIPTION

R

270000 32000

PERFORM A DETAIL VISUAL INSPECTION OF ALL FLIGHT CONTROL CABLES THAT ARE OVER THE CENTER WING SECTION B.S. 540 TO B.S. 663.75 AND CABLES WITHIN PILOT'S CONTROL QUADRANT. ACCESS PASSENGER CABIN FLOOR PANELS BETWEEN B.S. 540 TO B.S. 663.75.

ZONE ACCESS 135 136 211 emp 212

STRUCTURE

emp emp 211A 211B emp

R

N

737-6

MAINTENANCE SCHEDULE

270000 35000

INSPECT (DETAILED) INBOARD TRAILING EDGE AFT FLAP DRIVE CABLE. 553 653

553BB 653BB

N

Date: 23-jul-08

ITEMS

THRESHOLD INTERVAL

REFERENCES MRB MPD MRB

TSK

EFF

R L ITEM BY E E REVISION P V DATE

MSI 27-230-00 RTE:6 27-230-00 MSI 27-230-00 RTE:6

AMTOSS AMTOSS AMTOSS

20-20-31-200-801 20-20-31-200-802 20-20-31-200-805

MPD MRB

27-229-00 MSI 27-229-00 FEC:6

AMM AMM AMM

20-20-31-200-801 20-20-31-200-802 20-20-31-200-805

I: 36000 CYC I: 12 YRS

E3 HHI 737-700

6 23-jul-08

T: 21600 CYC T: 6 YRS I: 21600 CYC I: 6 YRS

E3 HHI 737-700

0 23-jul-08

ATA: 27 - 00

Page 10 of 10


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 27 - 11

271100 21000

271100 21100

DESCRIPTION

ZONE ACCESS

STRUCTURE

271100 71100

Date: 23-jul-08

TSK

EFF

R L ITEM BY E E REVISION P V DATE

AILERON AND FLAPERON CONTROL SYSTEM PERFORM A GENERAL VISUAL INSPECTION OF THE FORWARD AILERON 112 MECHANICAL COMPONENTS FROM CONTROL WHEEL TO AILERON BUS 211 DRUMS. 212

PERFORM A GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT WING AILERON MECHANICAL COMPONENTS FROM THE AILERON PCU'S TO THE AILERON AND THE FLIGHT SPOILER MECHANICAL CONTROL PATH.

133 134 572 672

112A emp emp

emp emp 572BB 672BB

MPD MRB

27-011-00 MSI 27-011-00 RTE:6

AMTOSS

27-11-00-210-801

MPD MPD MRB

27-013-01 27-013-02 MSI 27-013-01 RTE:6 MSI 27-013-02 RTE:6

MRB

271100 71000

THRESHOLD INTERVAL

REFERENCES

OPERATIONALLY CHECK THE AILERON SPRING CARTRIDGE AND TRANSFER MECHANISM.

130 211 212

FUNCTIONALLY CHECK THE AILERON SPRING CARTRIDGE AND TRANSFER 133 MECHANISM. 134 211 212

emp emp emp

emp emp emp emp

ITEMS

AMTOSS

27-11-00-210-802

MPD MRB

27-016-00 MSI 27-016-00 RTE:8

AMTOSS

27-11-00-710-802

MPD MRB

27-018-00 MSI 27-018-00 RTE:8

AMTOSS

27-11-00-700-806

I: 4000 FLH

E1 HHI 737-700

4 03-jun-04

I: 4000 FLH

E1 HHI 737-700

5 03-jun-04

I: 6000 FLH

F1 HHI 737-700

4 18-mar-05

I: 25000 FLH

F2 HHI 737-700

3 03-jun-04

ATA: 27 - 11

Page 1 of 4


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

271100 73000

271100 82000

271101 70000

271101 70100

271101 71000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

FUNCTIONALLY CHECK THE LEFT AND RIGHT WING AILERON SURFACE 210 AND AILERON TAB FREEPLAY. 572 672 NOTE( R ) ACCOMPLISH THE AILERON TAB FREEPLAY CHECK IN ACCORDANCE WITH AD 2006-21-01 AND SB 737-27-1273 (EO 154339).

PERFORM A DETAILED VISUAL INSPECTION OF THE AILERON FEEL AND 133 CENTERING SPRINGS.

STRUCTURE

emp emp emp

MPD MPD MRB MRB

emp

THRESHOLD INTERVAL

REFERENCES

EFF

R L ITEM BY E E REVISION P V DATE

27-033-00 27-035-00 MSI 27-033-00 RTE:8 MSI 27-035-00 RTE:8

AAR EO SB AMTOSS

AD 2006-21-01 154339 737-27-1273 27-09-91-200-801

MPD MRB

27-028-00 MSI 27-028-00 RTE:6

AMTOSS

27-11-81-210-801

OPERATIONALLY CHECK (HYDRAULIC POWER OFF) THE AILERON 133 CONTROL SURFACES FOR FULL RANGE OF TRAVEL AND FREEDOM OF 134 MOVEMENT. 211 212

emp emp emp emp

MPD MRB

27-030-00 MSI 27-030-00 RTE:8

AMTOSS

27-11-00-700-807

FUNCTIONALLY CHECK THE AILERON SYSTEM CONTROL WHEEL FORCES. 133 134 211 212

emp emp emp emp

MPD MRB

27-032-00 MSI 27-032-00 RTE:8

AMTOSS

27-11-00-700-803

FUNCTIONALLY CHECK THE FORCE REQUIRED TO EXTEND AND 133 COLLAPSE THE A AND B SYSTEM AILERON POWER CONTROL UNIT INPUT 134 POGO'S. 211 212

emp emp emp emp

MPD MRB

27-022-00 MSI 27-022-00 RTE:8

AMTOSS

27-11-00-720-801

ITEMS

TSK

I: 8000 FLH I: 24 MTH

F2 HHI 737-700

3 22-mar-07

I: 6000 FLH

E3 HHI 737-700

4 18-mar-05

I: 6000 FLH

F1 HHI 737-700

3 18-mar-05

I: 25000 FLH

F2 HHI 737-700

2 03-jun-04

I: 12500 FLH

F2 HHI 737-700

3 03-jun-04

ATA: 27 - 11

Page 2 of 4


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

271101 72000

271131 21000

DESCRIPTION

ZONE ACCESS

FUNCTIONALLY CHECK THE A AND B SYSTEM AILERON POWER CONTROL 133 UNIT INTERNAL LEAKAGE IN A LOADED CONDITION. 134 211 212

PERFORM A DETAILED VISUAL INSPECTION OF THE LEFT AND RIGHT WING AILERON BALANCE BAY SEALS.

572 emp emp 672 emp emp

STRUCTURE

emp emp emp emp

571BB 571CB 571DB 671BB 671CB 671DB

MPD MRB MRB

29-00-00-790-804

MPD MPD MRB

27-034-01 27-034-02 MSI 27-034-01 RTE:8 MSI 27-034-02 RTE:8

MRB

Date: 23-jul-08

CHECK UPPER AND LOWER SIDE OF LEFT AND RIGHT AILERON BALANCE PANELS FOR DEICING / ANTI-ICING FLUID RESIDUE AND CLEAN IF NECESSARY. METHOD 1 USE A SUITABLE FLEXISCOPE AND CHECK UPPER AND LOWER SIDE OF ALL BALANCE PANELS AND AFT PANEL HINGE AREA THROUGH GAPS BETWEEN AILERON AND FIXED TRAILING EDGE AS FAR AS POSSIBLE; OR METHOD 2 OPEN LOWER ACCESS PANELS 571BB/671BB TO BALANCE BAY 4, DISCONNECT AFT END OF BALANCE PANEL AND CHECK UPPER AND LOWER SIDE OF BALANCE PANEL. IF NO CONTAMINATION IS FOUND NO OTHER BALANCE PANELS HAVE TO BE CHECKED. IF CONTAMINATION IS EVIDENT OPEN OTHER ACCESS PANELS TO REMAINING BALANCE BAYS FOR INSPECTION. NOTE( J ) THIS ITEM IS EFFECTIVE FROM OCT01 UNTIL MAR 31.

572 emp emp 672 emp emp

571BB 571CB 571DB 671BB 671CB 671DB

ITEMS

TSK

EFF

R L ITEM BY E E REVISION P V DATE

27-024-00 MSI 27-024-00 RTE:6 MSI 27-024-00 RTE:9

AMM

AMTOSS 271131 22000

THRESHOLD INTERVAL

REFERENCES

I: 12500 FLH

F2 HHI 737-700

0 30-nov-05

27-11-31-210-801

I: 8000 FLH I: 3 YRS

E3 HHI 737-700

3 03-jun-04

737-SL-12-014

I: 450 FLH

E3 HHI S 737-700

2 29-apr-03

empty

SIL

ATA: 27 - 11

Page 3 of 4


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

271161 21000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

PERFORM A GENERAL VISUAL INSPECTION OF THE AILERON TRANSFER 112 MECHANISM.

STRUCTURE

112A

ITEMS

THRESHOLD INTERVAL

REFERENCES MPD MRB

27-012-00 MSI 27-012-00 RTE:8

AMTOSS

27-11-61-210-801

I: 6000 FLH

ATA: 27 - 11

TSK

EFF

E1 HHI 737-700

R L ITEM BY E E REVISION P V DATE

3 18-mar-05

Page 4 of 4


HHI R E V

ITEM 27 - 21

R

737-6

MAINTENANCE SCHEDULE

272100 03000

R

272100 60000

272100 65000

272100 80000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

RUDDER CONTROL SYSTEM FUNCTIONALLY CHECK THE RUDDER POWER CONTROL UNIT INTERNAL LEAKAGE IN A LOADED CONDITION. NOTE( I, R, E ) NOTE (R): THIS TASK ACCOMPLISHES CERTIFICATION MAINTENANCE REQUIREMENT TASK 27-CMR-03. NOTE (E): APPLICABLE TO AIRPLANE LINE NUMBERS 1-595 AND 597-1267 THAT HAVE NOT INCORPORATED SB 737-27-1253. NOTE (I): MSG-3 ANALYSIS FOR THIS ATSK IS 12500 FLH. CMR INTERVAL FOR THIS TASK IS 8000 FLH (SEE MPD SECTION9).

117 133 134 211 212 325

emp emp emp 117A emp 324DR

AAR

AMTOSS AMTOSS

27-21-00-700-822-001 I: 8000 FLH 27-21-00-700-821-001

REMOVE RUDDER PCU AND TEST PCU ACCORDING PARKER SB 381500-27-01. NOTE( J ) ITEM FOR COMPLETENESS ONLY COVERED BY COSL. P/N S251A301-1 P/N S251A301-2

324

emp

AAR

AD 99-11-05

AAR SB

LTA 1999-278 737-27A1222

OPERATIONAL CHECK OF THE MAIN RUDDER PCU FORCE FIGHT 210 MONITOR. 325 emp NOTE( E ) APPLICABLE TO AIRPLANE LINE NUMBERS 596, 1268 AND ON AND LINE NUMBERS 1 -595 AND 597 - 1267 THAT HAVE INCORPORATED SB 737-27-1253.

emp 324CL 324EL

OPERATIONAL CHECK OF THE RUDDER PCU OVERRIDES. 210 325 NOTE( E ) APPLICABLE TO AIRPLANE LINE NUMBERS 596, 1268 AND ON AND LINE emp NUMBERS 1 - 595 AND 597 - 1267 THAT HAVE INCORPORATED SB 737-27-1253.

emp 324BL 324DL

ITEMS

MPD MRB

27-CMR-03 ONE STAR 27-044-00 MSI 27-044-00 RTE:8 F2 HHI 737-700

7 23-jul-08

I: 24000 FLH

M1 HHI 737-700

1 29-apr-03

MPD MRB

27-041-00 MSI 27-041-00 RTE:9

AMTOSS

27-21-00-700-824-002 I: 10000 FLH

F1 HHI 737-700

2 18-mar-05

MPD MRB

27-043-00 MSI 27-043-00 RTE:8

AMTOSS

27-21-00-700-823-002 I: 12500 FLH

F1 HHI 737-700

1 03-jun-04

ATA: 27 - 21

Page 1 of 4


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

272100 85000

272100 86000

272100 87000

272101 70000

272102 70000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

FUNCTIONAL CHECK OF THE RUDDER POWER CONTROL UNIT INTERNAL 133 LEAKAGE IN A LOADED CONDITION. 134 325 NOTE( I, E ) NOTE (E): APPLICABLE TO AIRPLANES LINE NUMBER 596 AND 1268 AND ON AND LINE NUMBERS 1-595 AND 597-1267 THAT HAVE INCORPORATED SB 737-27-1253. NOTE (I): MSG-3 ANALYSIS FOR THIS TASK IS 12500 FLH. CMR INTERVAL FOR THIS TASK IS 10000 FLH (SEE MPD SECTION 9).

emp emp 324DL

OPERATIONALLY CHECK THE RUDDER PCU PRESSURE REDUCING VALVE. 134 AIRPLANE NOTE: APPLICABLE TO AIRPLANES L/N 1-595 AND 597-1267 135 THAT HAVE NOT INCORPORATED SB737-27-1253. 325 NOTE( E ) APPLICABLE TO AIRPLANES L/N 1-595 AND 597-1267 THAT HAVE NOT INCORPORATED SB737-27-1253.

emp emp emp

FUNCTIONALLY CHECK THE RUDDER PCU RELIEF VALVE (AUTHORITY 131 LIMITER) DURING RUDDER PCU INTERNAL LEAKAGE. 134 325 NOTE( R, E ) NOTE: (R) THIS TASK IS SATISFIED BY ACCOMPLISHMENT OF TASK 27-047-00. NOTE: (E) APPLICABLE TO AIRPLANES LINE NUMBER 596; AND 1268 AND ON; AND L/N 1-595 AND 597-1267 WITH INCORPORATION OF SB 737-27-1253.

emp emp 324DL

OPERATIONALLY CHECK THE WHEEL TO RUDDER INTERCONNECT SYSTEM (WTRIS).

emp emp

211 212

OPERATIONALLY CHECK THE RUDDER TRIM THROUGH THE FULL RANGE 211 OF MOVEMENT.

STRUCTURE

THRESHOLD INTERVAL

REFERENCES AAR MPD MRB

ITEMS

EFF

R L ITEM BY E E REVISION P V DATE

27-CMR-10 ONE STAR 27-047-00 MSI 27-047-00 RTE:8

AMTOSS

27-21-00-700-822-002 I: 10000 FLH

MPD MRB

27-050-00 MSI 27-050-00 RTE:8

AMM

27-21-00-700-821-001 I: 8000 FLH

MPD MRB

27-048-00 MSI 27-048-00 RTE:8 I: 10000 FLH

emp

TSK

MPD MRB

27-060-00 MSI 27-060-00 RTE:8

AMTOSS AMTOSS

27-21-00-700-820-002 I: 6000 FLH 27-21-00-700-820-001

MPD MRB

27-062-00 MSI 27-062-00 RTE:9

AMTOSS AMTOSS

27-21-00-700-819-002 I: 6000 FLH 27-21-00-700-819-001

ATA: 27 - 21

F2 HHI 737-700

4 25-apr-06

F1 HHI 737-700

3 05-sep-06

F2 HHI 737-700

0 05-sep-06

F1 HHI 737-700

4 18-mar-05

F1 HHI 737-700

4 18-mar-05

Page 2 of 4


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

272103 70000

272124 21000

272124 22000

272151 21000

272161 21000

Date: 23-jul-08

DESCRIPTION FUNCTIONALLY CHECK THE RUDDER SURFACE FREEPLAY.

ZONE ACCESS 325

PERFORM A GENERAL VISUAL INSPECTION OF THE STANDBY RUDDER 211 POWER CONTROL UNIT WITH HYDRAULIC POWER ON. 325

PERFORM A DETAILED VISUAL INSPECTION OF THE STANDBY RUDDER 325 POWER CONTROL UNIT FORE AND AFT ATTACHMENT POINTS (STRUCTURE TO PCU TO RUDDER SURFACE).

GENERAL VISUAL INSPECTION OF THE RUDDER FORWARD MECHANICAL 112 CONTROL PATH.

DETAILED INSPECTION OF AFT RUDDER QUADRANT, TORQUE TUBE 320 ASSEMBLY, FEEL AND CENTERING UNIT AND ASSOCIATED INPUT/OUTPUT 325 RODS. emp - AFT QUADRANT - AFT QUADRANT OUTPUT ROD - AFT QUADRANT BEARINGS - AFT QUADRANT SHAFT - RUDDER TORQUE TUBE - RUDDER TORQUE TUBE BEARINGS - RUDDER TORQUE TUBE CRANKS - RUDDER TORQUE TUBE INPUT RODS - FEEL AND CENTERING UNIT - FEEL AND CENTERING UNIT OUTPUT ROD

STRUCTURE

emp

emp 324DL

emp

112A

324CL 323FL 324DL

ITEMS

THRESHOLD INTERVAL

REFERENCES MPD MRB

27-064-00 MSI 27-064-00 RTE:8

AMTOSS

27-21-00-700-814

MPD MRB

27-056-00 MSI 27-056-00 RTE:8

AMTOSS

27-21-24-210-801

MPD MRB

27-058-00 MSI 27-058-00 RTE:8

AMTOSS

27-21-24-210-802

MPD MRB

27-038-00 MSI 27-038-00 RTE:5

AMTOSS

27-21-51-210-801

MPD MRB

27-036-00 MSI 27-036-00 RTE:8

AMTOSS

27-21-61-210-801

TSK

EFF

R L ITEM BY E E REVISION P V DATE

I: 8000 FLH

F2 HHI 737-700

3 03-jun-04

I: 5000 FLH

E1 HHI 737-700

2 03-jun-04

I: 6000 FLH

E3 HHI 737-700

4 18-mar-05

I: 6000 FLH

E1 HHI 737-700

3 18-mar-05

I: 6000 FLH

E3 HHI 737-700

6 05-sep-06

ATA: 27 - 21

Page 3 of 4


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

272171 00000

272182 00000

Date: 23-jul-08

DESCRIPTION PERFORM A DETAILED VISUAL INSPECTION OF THE RUDDER SINGLE ELEMENT DUAL LOAD PATH RUDDER PCU INPUT COMPONENTS.

PERFORM A DETAILED VISUAL INSPECTION OF THE RUDDER SINGLE ELEMENT DUAL LOAD PATH FEEL AND CENTERING COMMAND AND GROUND PATH COMPONENTS.

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

324 emp emp emp

323CL 323FL 324BL 324DL

MPD MRB

27-066-00 MSI 27-066-00 RTE:8

AMTOSS

27-21-61-210-801

324 emp emp 325

323CL 323FL 324DL emp

MPD MRB

27-065-00 MSI 27-065-00 RTE:8

AMTOSS

27-21-61-210-801

ITEMS

TSK

EFF

R L ITEM BY E E REVISION P V DATE

I: 6 YRS

E3 HHI 737-700

5 03-jun-04

I: 6 YRS

E3 HHI 737-700

5 03-jun-04

ATA: 27 - 21

Page 4 of 4


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 27 - 31

273100 01000

273100 70000

DESCRIPTION

ZONE ACCESS

STRUCTURE

273100 72000

273100 73000

Date: 23-jul-08

TSK

EFF

R L ITEM BY E E REVISION P V DATE

ELEVATOR CONTROL SYSTEM PERFORM A BITE CHECK OF THE ELEVATOR AUTOPILOT SERVO PRESSURE REGULATOR.

211 212

OPERATIONALLY CHECK, HYDRAULIC POWER OFF, THE ELEVATOR 211 CONTROL SURFACES FOR FULL RANGE OF TRAVEL AND FREEDOM OF 212 MOVEMENT.

emp emp

311BL emp

MPD MRB

27-094-00 MSI 27-094-00 RTE:9

AMTOSS

22-11-26-710-801

MPD MRB

27-074-00 MSI 27-074-00 RTE:6 MSI 27-074-00 RTE:9

MRB

273100 71000

THRESHOLD INTERVAL

REFERENCES

FUNCTIONALLY CHECK THE ELEVATOR SURFACE FREEPLAY.

FUNCTIONALLY CHECK THE FORCE NECESSARY TO BREAKOUT THE ELEVATOR CONTROL COLUMN OVERRIDE ASSEMBLY.

334 344

211 212

FUNCTIONALLY CHECK THE ELEVATOR FREEPLAY AND THE ELEVATOR 334 TAB FREEPLAY. 344 NOTE( E ) APPLICABLE TO AIRPLANE LINE NUMBER 1-595 AND 597-1174 THAT HAVE NOT INCORPORATED SB 737-55A1080.

311BL emp

emp emp

311BL emp

ITEMS

AMTOSS

27-31-00-700-807

MPD MRB

27-098-01 MSI 27-098-01 RTE:9

MPD MRB

27-084-00 MSI 27-084-00 RTE:8

AMTOSS

27-31-00-720-801

MPD MRB

27-096-00 MSI 27-096-00 RTE:9

AMTOSS

27-09-91-200-803

I: 6000 FLH

F1 HHI 737-700

4 18-mar-05

I: 6000 FLH

F1 HHI 737-700

4 18-mar-05

T: 8000 FLH I: 8000 FLH

F2 HHI 737-700

0 18-mar-05

I: 25000 FLH

F2 HHI 737-700

2 03-jun-04

I: 8000 FLH

F2 HHI 737-700

2 18-mar-05

ATA: 27 - 31

Page 1 of 4


HHI R E V

ITEM 273100 82000

273101 70000

R

737-6

MAINTENANCE SCHEDULE

273101 75000

DESCRIPTION FUNCTIONALLY CHECK THE FORCE NECESSARY TO COLLAPSE AND EXTEND THE ELEVATOR INPUT ROD POGO'S.

ZONE ACCESS

STRUCTURE

211 212 317 318

311BL emp emp emp

MPD MRB

27-092-00 MSI 27-092-00 RTE:8

AMTOSS

27-31-00-820-809

211 212 334 344

emp emp emp emp

MPD MRB

27-086-00 MSI 27-086-00 RTE:9

AMTOSS

27-31-00-700-815

PERFORM A FUNCTIONAL CHECK OF THE ELEVATOR TAB FREEPLAY. 334 344 NOTE( E ) APPLICABLE TO AIRPLANES LINE NUMBERS 596, 1175 AND ON AND LINE NUMBERS 1 - 595 AND 597 - 1174 THAT HAVE INCORPORATED SB 737-55A1080.

emp emp

AAR

OPERATIONALLY CHECK THE ELEVATOR TAB CONTROL SYSTEM.

MPD MRB

R

Date: 23-jul-08

CHECK UPPER AND LOWER SIDE OF LEFT AND RIGHT ELEVATOR BALANCE PANELS FOR DEICING / ANTI-ICING FLUID RESIDUE AND CLEAN IF NECESSARY. METHOD 1 USE A SUITABLE FLEXISCOPE AND CHECK UPPER AND LOWER SIDE OF ALL BALANCE PANELS AND AFT PANEL HINGE AREA THROUGH GAPS BETWEEN ELEVATOR AND FIXED TRAILING EDGE AS FAR AS POSSIBLE; OR METHOD 2 OPEN LOWER ACCESS PANELS 333CB/343CB TO BALANCE BAY 5, DISCONNECT AFT END OF BALANCE PANEL AND CHECK UPPER AND LOWER SIDE OF BALANCE PANEL. IF NO CONTAMINATION IS FOUND NO OTHER BALANCE PANELS HAVE TO BE CHECKED. IF CONTAMINATION IS EVIDENT OPEN OTHER ACCESS PANELS TO REMAINING BALANCE BAYS FOR INSPECTION. NOTE( J ) THIS ITEM IS EFFECTIVE FROM OCT01 UNTIL MAR 31.

334 emp emp emp 344 emp emp emp

333BB 333CB 333DB 333EB 343BB 343CB 343DB 343EB

ITEMS

TSK

EFF

R L ITEM BY E E REVISION P V DATE

I: 12500 FLH

F2 HHI 737-700

3 03-jun-04

I: 6000 FLH

F1 HHI 737-700

3 18-mar-05

27-31-32-200-802

I: 2000 CYC I: 4000 FLH

F2 HHI 737-700

3 23-jul-08

737-SL-12-014

I: 450 FLH

E3 HHI S 737-700

0 03-jun-04

27-CMR-08 ONE STAR 27-099-00 MSI 27-099-00 RTE:9

AMTOSS 273102 01000

THRESHOLD INTERVAL

REFERENCES

empty

SIL

ATA: 27 - 31

Page 2 of 4


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

273111 00000

273114 21000

273114 21100

273114 22000

273117 20000

273120 00000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

PERFORM A DETAILED VISUAL INSPECTION OF THE ELEVATOR PUSH 334 RODS (BETWEEN OUTPUT TORQUE TUBE AND CONTROL SURFACE) AND 344 ATTACHMENT BOLTS.

PERFORM A GENERAL VISUAL INSPECTION OF THE ELEVATOR POWER 317 CONTROL UNIT WITH HYDRAULIC POWER ON. 318

FUNCTIONALLY CHECK THE A AND B SYSTEM ELEVATOR POWER CONTROL UNIT FOR INTERNAL LEAKAGE IN A LOADED CONDITION.

STRUCTURE

318BR emp

emp 318BR

THRESHOLD INTERVAL

REFERENCES MPD MRB

27-100-00 MSI 27-100-00 RTE:8

AMTOSS

27-31-00-200-801

MPD MRB

27-076-00 MSI 27-076-00 RTE:8

AMTOSS

27-31-14-210-801

133 134 211 212

emp emp emp emp

MPD MRB

27-078-00 MSI 27-078-00 RTE:8

AMTOSS

29-00-00-790-804

OPERATIONALLY CHECK THE ELEVATOR CONTROL COLUMN OVERRIDE 211 ASSEMBLY. 212

emp emp

MPD MRB

27-082-00 MSI 27-082-00 RTE:8

AMTOSS

27-31-00-710-802

MPD MRB

27-080-00 MSI 27-080-00 RTE:6

AMTOSS AMTOSS

27-31-17-790-801 27-31-17-200-801

MPD MRB

27-068-00 MSI 27-068-00 RTE: 9

AMTOSS

27-31-20-740-801

DRAIN AND LEAK CHECK THE ELEVATOR PITOT-STATIC SYSTEM.

OPERATIONALLY CHECK THE ELEVATOR FEEL SHIFT FUNCTION. (IF INSTALLED)

311 312 320

117 118 211 212

311BL emp 323FL

117A emp emp emp

ITEMS

TSK

EFF

R L ITEM BY E E REVISION P V DATE

I: 6 YRS

E3 HHI 737-700

3 03-jun-04

I: 6000 FLH

E1 HHI 737-700

3 18-mar-05

I: 12500 FLH

F2 HHI 737-700

0 30-nov-05

I: 12500 FLH

F1 HHI 737-700

2 03-jun-04

I: 6000 FLH

F2 HHI 737-700

4 18-mar-05

I: 6000 FLH

F1 HHI 737-700

4 18-mar-05

ATA: 27 - 31

Page 3 of 4


HHI R E V

ITEM 273134 21000

R

737-6

MAINTENANCE SCHEDULE

273134 21500

R

273161 21000

273164 90000

Date: 23-jul-08

DESCRIPTION PERFORM A GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT ELEVATOR BALANCE WEIGHT INSTALLATION AND ELEVATOR TAB CONTROL MECHANISM.

ZONE ACCESS

STRUCTURE

334 emp emp emp 344 emp emp emp

333BB 333CB 333DB 334PT 343BB 343CB 343DB 344PT

MPD MPD MRB

PERFORM A DETAILED VISUAL INSPECTION OF THE ELEVATOR TAB RODS AND TAB MECHANISM FOR CONDITION AND SECURITY OF INSTALLATION. THIS TASK ACCOMPLISHES CERTIFICATION MAINTENANCE REQUIREMENT TASK 27-CMR-07. NOTE( E ) APPLICABLE TO AIRPLANES LINE NUMBER 596 AND 1175 AND ON AND LINE NUMBERS 1-595 AND 597-1174 THAT HAVE INCORPORATED SB 737-55A1080.

333 334 343 344

333BB 334PT 343BB 344PT

AAR

PERFORM A GENERAL VISUAL INSPECTION OF THE ELEVATOR MECHANICAL CONTROL PATH.

112 334 344

PERFORM A DETAILED VISUAL INSPECTION OF THE SINGLE ELEMENT DUAL LOAD PATH FEEL AND CENTERING UNIT OUTPUT ROD.

313 314

112A 318BR emp

emp 318BR

ITEMS

THRESHOLD INTERVAL

REFERENCES

EFF

R L ITEM BY E E REVISION P V DATE

27-075-01 27-075-02 MSI 27-075-01 RTE:9 MSI 27-075-02 RTE:9

MRB AMTOSS

MPD MRB

TSK

27-31-34-210-801

I: 6000 FLH

E1 HHI 737-700

3 18-mar-05

I: 2000 CYC I: 4000 FLH

E3 HHI 737-700

3 23-jul-08

I: 6000 FLH

E1 HHI 737-700

4 18-mar-05

I: 6 YRS

E3 HHI 737-700

4 18-mar-05

27-CMR-07 ONE STAR 27-093-00 MSI 27-093-00 RTE:8

AMTOSS

27-31-00-220-802

MPD MRB

27-073-00 MSI 27-073-00 RTE:6

AMTOSS

27-31-61-210-801

MPD MRB

27-101-00 MSI 27-101-00 RTE:8

AMTOSS

27-31-00-200-802

ATA: 27 - 31

Page 4 of 4


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 27 - 32

273200 71000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

STALL WARNING FUNCTIONALLY CHECK THE STALL WARNING SYSTEM.

117 118 211 212

117A emp emp emp

ITEMS

MPD MRB

27-088-00 MSI 27-088-00 RTE:9

AMTOSS AMTOSS

27-32-00-740-803 27-32-00-710-801

I: 6000 FLH

ATA: 27 - 32

F2 HHI 737-700

4 18-mar-05

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 27 - 41

274100 70000

274101 70000

274102 70000

274103 70000

274141 21000

274181 00000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

HORIZONTAL STABILIZER CONTROL SYSTEM FUNCTIONALLY CHECK THE SECONDARY STABILIZER TRIM BRAKE. NOTE( E ) APPLICABLE TO 251A4510-6 AND ON ACTUATORS.

211 212 311 312

emp emp 311BL emp

MPD MRB

27-106-00 MSI 27-106-00 RTE:8

AMTOSS

27-41-00-700-808

OPERATIONALLY CHECK THE STABILIZER TRIM LIMIT SWITCHES (FLAPS 211 UP AND FLAPS DOWN). 311 312

emp 311BL emp

MPD MRB

27-112-00 MSI 27-112-00 RTE:9

AMTOSS

27-41-00-700-805

MPD MRB

27-114-00 MSI 27-114-00 RTE:9

AMTOSS

27-41-00-700-810

MPD MRB

27-118-00 MSI 27-118-00 RTE:8

AMTOSS

27-41-00-700-807

MPD MRB

27-120-00 MSI 27-120-00 RTE:8

AMTOSS

27-41-41-210-801

MPD MRB

27-107-00 MSI 27-107-00 RTE:8

AMTOSS

12-22-41-610-802

OPERATIONALLY CHECK THE STABILIZER TRIM CONTROL COLUMN SWITCHING MODULE.

112 210

OPERATIONALLY CHECK THE AISLE STAND STABILIZER TRIM OVERRIDE 211 SWITCH. 212

DETAILED VISUAL INSPECTION OF THE UPPER AND LOWER STABILIZER 112 TRIM FORWARD MECHANISM RETENTION TURNBUCKLES AND TURNBUCKLE ATTACHMENT POINTS.

SERVICE THE HORIZONTAL TRIM ACTUATOR BRAKE. 311 312 NOTE( E ) APPLICABLE TO LINE NUMBER 350 AND ON. APPLICABLE TO AIRPLANES LINE NUMBER 1 TO 349 THAT HAVE INCORPORATED SB 737-27-1210.

112A emp

emp emp

112A

emp emp

ITEMS

I: 6000 FLH

F2 HHI 737-700

6 18-mar-05

I: 6000 FLH

F1 HHI 737-700

4 18-mar-05

I: 6000 FLH

F1 HHI 737-700

4 18-mar-05

I: 6000 FLH

F1 HHI 737-700

3 18-mar-05

I: 6000 FLH

E3 HHI 737-700

4 18-mar-05

I: 6000 FLH

S

2 05-sep-06

ATA: 27 - 41

HHI 737-700

Page 1 of 2


HHI R E V

ITEM

R

274181 01000

R

R

737-6

MAINTENANCE SCHEDULE

274181 21000

DESCRIPTION

ZONE ACCESS

REMOVE THE STABILIZER TRIM ACTUATOR FOR RESTORATION. NOTE( J, E ) NOTE (J): TASK IS A TIME CONTROLLED ITEM, IT IS INCLUDED IN MS FOR COMPLETENESS. NOTE (E): FOR 251A4510-6 AND ON ACTUATORS ONLY.

311 emp 312

PERFORM A DETAILED VISUAL INSPECTION OF THE STABILIZER TRIM JACKSCREW, BALLNUT, BALLNUT RETURN TUBES AND UPPER AND LOWER GIMBAL PINS.

311 312

STRUCTURE

112A 311BL emp

274197 70000

Date: 23-jul-08

OPERATIONALLY CHECK THE MAIN CONTROL COLUMN CUTOUT SWITCHES.

MPD MRB MRB

311BL emp

211 212

OPERATIONALLY CHECK THE CONTROL COLUMN STABILIZER TRIM ARM 211 AND DIRECTIONAL SWITCHES FOR MOVEMENT OF A SINGLE SWITCH TO 212 CAUSE STABILIZER MOVEMENT.

emp emp

emp emp

ITEMS

TSK

EFF

R L ITEM BY E E REVISION P V DATE

27-108-00 MSI 27-108-00 RTE:8 MSI 27-108-00 RTE:9

MS CM2740 00020 AMTOSS 27-41-81-400-801 AMTOSS 27-41-81-000-801 SB 737-27A1277 R1 SB CONTAINS A REQUIREMENT FOR OVERHAUL OF THE HORIZONTAL STABILIZER.

R

274191 70000

THRESHOLD INTERVAL

REFERENCES

MPD MRB

27-110-00 MSI 27-110-00 RTE:8

SB AMTOSS

737-27A1277 R1 27-41-81-210-801

MPD MRB

27-116-00 MSI 27-116-00 RTE:8

AMTOSS

27-41-91-700-801

MPD MRB

27-122-00 MSI 27-122-00 RTE:9

AMTOSS

27-41-97-700-801

I: 25000 FLH

S

HHI 737-700

4 23-jul-08

I: 1 YRS I: 1600 FLH I: 8 MTH

E3 HHI 737-700

8 23-jul-08

I: 6000 FLH

F1 HHI 737-700

3 18-mar-05

I: 6000 FLH

F1 HHI 737-700

3 18-mar-05

ATA: 27 - 41

Page 2 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 27 - 51

275100 21000

275100 71000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

FLAP/SLAT SYSTEM PERFORM A GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT WING FLAP DRIVE SEAL RIB ANGLE GEAR BOX, FLAP DRIVE TORQUE TUBES, TORQUE TUBE COUPLINGS AND SUPPORTS AND FLAP TRANSMISSIONS. ACCESS FLAPS DEPLOYED

OPERATIONALLY CHECK THE LEFT AND RIGHT WING TRAILING EDGE FLAP TRANSMISSION NO-BACK BRAKES. ACCESS FLAPS DEPLOYED

133 134 541 542 543 544 550 553 560 561 562 565 641 642 643 644 650 653 660 661 662 665

emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp

MPD MPD MRB

AMTOSS

27-51-00-210-801

133 134 210 541 542 543 544 553 641 642 643 644 653

emp emp emp emp emp emp emp emp emp emp emp emp emp

MPD MPD MRB

27-168-01 27-168-02 MSI 27-168-01 RTE:8 MSI 27-168-02 RTE:8

ITEMS

MRB

MRB AMTOSS

27-171-01 27-171-02 MSI 27-171-01 RTE:6 MSI 27-171-02 RTE:6

27-51-00-710-802

I: 6000 FLH

E1 HHI 737-700

5 22-mar-07

I: 25000 CYC

F1 HHI 737-700

4 03-jun-04

ATA: 27 - 51

Page 1 of 4


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

275100 72000

275100 73000

275100 74000

275100 74100

DESCRIPTION FUNCTIONALLY CHECK THE FLAP LOAD RELIEF SYSTEM.

FUNCTIONALLY CHECK THE ALTERNATE FLAP DRIVE SYSTEM.

OPERATIONALLY CHECK THE FLAP LOAD RELIEF SYSTEM.

ZONE ACCESS 117 118

133 134 212

117 118 210

OPERATIONALLY CHECK THE FLAP SKEW AND ASYMMETRY SYSTEM BY 117 INITIATING A BITE CHECK AT THE FLAP/SLAT ELECTRONICS UNIT (FSEU). 118 211 212

STRUCTURE

117A emp

emp emp emp

117A emp emp

117A emp emp emp

MPD MRB

27-156-00 MSI 27-156-00 RTE:9

AMTOSS

27-51-00-720-804

MPD MRB

27-158-00 MSI 27-158-00 RTE:9

AMTOSS

27-51-00-720-803

MPD MRB

27-154-00 MSI 27-154-00 RTE:9

AMTOSS

27-51-00-740-803

MPD MPD MRB

27-160-00 27-162-00 MSI 27-160-00 RTE:8 MSI 27-162-00 RTE:8

MRB AMTOSS

Date: 23-jul-08

ITEMS

THRESHOLD INTERVAL

REFERENCES

27-51-00-740-802

TSK

EFF

R L ITEM BY E E REVISION P V DATE

I: 10000 FLH

F2 HHI 737-700

2 03-jun-04

I: 6000 FLH

F2 HHI 737-700

3 18-mar-05

I: 2500 FLH

F1 HHI 737-700

2 03-jun-04

I: 750 FLH

F1 HHI 737-700

3 03-jun-04

ATA: 27 - 51

Page 2 of 4


HHI R E V

ITEM 275101 21000

275101 74000

R

737-6

MAINTENANCE SCHEDULE

275106 21000

DESCRIPTION PERFORM A DETAILED VISUAL INSPECTION OF THE LEFT AND RIGHT WING TRAILING EDGE FLAP ACTUATION MECHANISM TO INCLUDE: - AFT FLAP DRIVE RODS - AFT FLAP PUSH RODS - INBOARD CARRIAGE ROLLERS - OUTBOARD CARRIAGE ROLLERS - BELLCRANKS - INBOARD CARRIAGE FORWARD ATTACH FITTING - INBOARD CARRIAGE ATTACH LINK - OUTBOARD CARRIAGE FWD ATTACH FITTING - OUTBOARD CARRIAGE ATTACH LINK - INBOARD FLAP PROGRAMMING ROLLERS - AFT FLAP TRACK ATTACH FITTING - AFT FLAP PROGRAMMING ROLLER - OUTBOARD FLAP PROGRAMMING ROLLERS ACCESS FLAPS DEPLOYED

ZONE ACCESS 542 543 544 553 561 562 564 567 642 643 644 653 661 667

STRUCTURE

emp emp emp emp emp emp emp emp emp emp emp emp emp emp

MPD MPD MRB

AMTOSS

27-51-00-210-802

OPERATIONALLY CHECK THE FLAP UNCOMMANDED MOTION PROTECTION 117 SYSTEM BY INITIATING A BITE CHECK OF THE FLAP SLAT ELECTRONICS 118 UNIT. 211 212

117A emp emp emp

MPD MRB

27-164-00 MSI 27-164-00 RTE:8

AMTOSS

27-51-00-740-801

PERFORM A DETAILED VISUAL INSPECTION OF THE TRAILING EDGE FLAP 112 LEVER SENSOR, LINKAGE, ROD AND ROD ENDS. 117 118 211 emp 212

emp emp emp 211A 211B emp

MPD MRB

27-166-00 MSI 27-166-00 RTE:8 27-166-00 MSI 27-166-00 RTE:8

R

Date: 23-jul-08

THRESHOLD INTERVAL

REFERENCES

MRB

MPD MRB AMTOSS

ITEMS

TSK

EFF

R L ITEM BY E E REVISION P V DATE

27-172-01 27-172-02 MSI 27-172-01 RTE:6 MSI 27-172-02 RTE:6

27-51-06-210-801

I: 12000 CYC

E3 HHI 737-700

3 03-jun-04

I: 6000 FLH

F1 HHI 737-700

2 18-mar-05

I: 25000 FLH

E3 HHI 737-700

4 23-jul-08

ATA: 27 - 51

Page 3 of 4


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

275132 22000

Date: 23-jul-08

DESCRIPTION FUNCTIONALLY CHECK THE LEFT AND RIGHT WING TRAILING EDGE FLAPS BALLSCREW ACTUATOR BACKLASH. ACCESS FLAPS DEPLOYED

ZONE ACCESS 133 134 210 541 542 543 544 553 641 642 643 644 653

STRUCTURE

emp emp emp emp emp emp emp emp emp emp emp emp emp

ITEMS

THRESHOLD INTERVAL

REFERENCES MPD MPD MRB MRB AMTOSS AMTOSS AMTOSS AMTOSS

TSK

EFF

R L ITEM BY E E REVISION P V DATE

27-148-01 27-148-02 MSI 27-148-01 RTE:6 MSI 27-148-02 RTE:6 27-51-42-220-801 27-51-32-220-801 27-51-42-220-802 27-51-32-220-802

I: 25000 CYC

ATA: 27 - 51

F2 HHI 737-700

3 03-jun-04

Page 4 of 4


HHI R E V

ITEM 27 - 61

N

737-6

MAINTENANCE SCHEDULE

276100 21000

DESCRIPTION

ZONE ACCESS

STRUCTURE

276100 72000

276100 73000

276100 82000

Date: 23-jul-08

TSK

EFF

R L ITEM BY E E REVISION P V DATE

SPOILER AND SPEEDBRAKE CONTROL SYSTEM PERFORM A GENERAL VISUAL INSPECTION OF THE SPOILER MECHANICAL 134 CONTROL PATH.

emp

N 276100 71000

THRESHOLD INTERVAL

REFERENCES

MPD MRB

27-215-03 MSI 27-215-03 FEC:6

AMM

27-61-00-210-801

OPERATIONALLY CHECK THE SPOILER MIXER CENTERING MECHANISM. 133 134 NOTE( I ) 210 CMR-INTERVAL 20000 FLH 550 562 563 564 565 650 662 663 664 665

emp emp emp emp emp emp emp emp emp emp emp emp emp

AAR MPD MRB

27-CMR-04 27-194-00 MSI 27-194-00 RTE:8

AMTOSS

27-61-00-710-802

FUNCTIONALLY CHECK THE INTERNAL LEAKAGE OF LEADING EDGE SLAT 133 ACTUATORS. 134 211 212

emp emp emp emp

MPD MRB

27-210-00 MSI 27-210-00 RTE:6

AMM

29-00-00-790-804

FUNCTIONALLY CHECK THE INTERNAL LEAKAGE OF LEADING EDGE FLAP 133 ACTUATORS. 134 211 212

emp emp emp emp

MPD MRB

27-212-00 MSI 27-212-00 RTE:6

AMM

29-00-00-790-804

FUNCTIONALLY CHECK THE TORQUE OF THE SPOILER MIXER NO-BACK 133 ASSEMBLY. 134

112A emp

MPD MRB

27-184-00 MSI 27-184-00 RTE:8

AMTOSS

27-61-00-820-809

ITEMS

T: 4000 FLH I: 4000 FLH

E2 HHI 737-700

0 23-jul-08

I: 12000 FLH

F1 HHI 737-700

4 22-mar-07

I: 12500 FLH

F2 HHI 737-700

0 30-nov-05

I: 12500 FLH

F2 HHI 737-700

0 30-nov-05

I: 22400 FLH

F2 HHI 737-700

3 03-jun-04

ATA: 27 - 61

Page 1 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

276101 82000

Date: 23-jul-08

DESCRIPTION PERFORM AN OPERATIONAL CHECK OF EACH LEFT AND RIGHT WING FLIGHT SPOILER ACTUATOR OVERRIDE QUADRANT. ACCESS FLAPS DEPLOYED

ZONE ACCESS 562 563 564 565 566 662 663 664 665 666

STRUCTURE

emp emp emp emp emp emp emp emp emp emp

ITEMS

THRESHOLD INTERVAL

REFERENCES MPD MPD MRB MRB AMTOSS

TSK

EFF

R L ITEM BY E E REVISION P V DATE

27-192-01 27-192-02 MSI 27-192-01 RTE:8 MSI 27-192-02 RTE:8 27-61-00-820-810

I: 25000 FLH

ATA: 27 - 61

F1 HHI 737-700

2 03-jun-04

Page 2 of 2


HHI R E V

ITEM 27 - 62

R

737-6

MAINTENANCE SCHEDULE

276200 21000

DESCRIPTION

276201 82000

276202 82000

Date: 23-jul-08

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

AUTO SPEEDBRAKE CONTROL PERFORM A GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT WING FLIGHT SPOILER AND SPEEDBRAKE ACTUATORS.

emp emp emp emp emp emp emp emp emp emp emp emp emp emp

MPD MPD MRB

AMTOSS

27-62-00-210-802

PERFORM A GENERAL VISUAL INSPECTION OF THE FORWARD STABILIZER 112 TRIM MECHANISM AND THE SPEEDBRAKE LEVER ASSEMBLY AND AUTO SPEEDBRAKE ELECTRIC ACTUATOR, ACTUATOR ROD END, AND FORWARD ATTACHMENT POINTS.

112A

MPD MRB

27-121-00 MSI 27-121-00 RTE:6

AMTOSS

27-62-00-210-801

OPERATIONALLY CHECK THE SPEEDBRAKE REFUSED TAKEOFF (RTO) 117 SYSTEM. 118 210 211 212

117A emp emp emp emp

MPD MRB

27-188-00 MSI 27-188-00 RTE:9

AMTOSS AMTOSS

27-61-00-820-809 27-62-00-820-809

OPERATIONALLY CHECK THE SPEEDBRAKES EXTENDED LIGHT.

117A emp emp

MPD MRB

27-190-00 MSI 27-190-00 RTE:8

AMTOSS

27-62-00-820-810

R

276201 21000

ZONE ACCESS

210 552 562 563 564 565 566 652 653 662 663 664 665 666

117 118 210

ITEMS

MRB MPD MPD MRB

27-215-01 27-215-02 MSI 27-215-01 RTE:6 MSI 27-215-02 RTE:6 27-215-01 27-215-02 MSI 27-215-01 RTE:6 I: 4000 FLH

E1 HHI 737-700

6 23-jul-08

I: 6000 FLH

E1 HHI 737-700

4 18-mar-05

I: 6000 FLH

F1 HHI 737-700

5 05-sep-06

I: 6000 FLH

F1 HHI 737-700

4 18-mar-05

ATA: 27 - 62

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 27 - 81

278100 21000

278100 70000

278100 71000

278100 86000

DESCRIPTION

ZONE ACCESS

STRUCTURE

TSK

EFF

R L ITEM BY E E REVISION P V DATE

LEADING EDGE SLAT SYSTEM PERFORM A GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT WING LEADING EDGE FLAP AND SLAT ACTUATORS AND THE LEFT AND RIGHT WING LEADING EDGE FLAP SLAT ACTUATION MECHANISMS. ACCESS LEADING EDGES EXTENDED

512 513 522 523 524 525 612 613 622 623 624 625

OPERATIONALLY CHECK THE LEADING EDGE UNCOMMANDED MOTION 211 PROTECTION SYSTEM. 212

OPERATIONALLY CHECK THE LEADING EDGE DEVICES UNCOMMANDED 211 MOTION PROTECTION USING THE STANDBY HYDRAULIC SYSTEM. 212

OPERATIONALLY CHECK THE LEADING EDGE STANDBY ACTUATION SYSTEM.

211 212 510 610

emp emp emp emp emp emp emp emp emp emp emp emp

MPD MPD MRB

AMTOSS

27-81-00-210-801

117A emp

MPD MRB

27-218-00 MSI 27-218-00 RTE:8

AMTOSS

27-81-00-700-804

MPD MRB

27-224-00 MSI 27-224-00 RTE:8

AMTOSS

27-81-00-710-802

MPD MPD MRB

27-214-00 29-240-00 MSI 27-214-00 RTE:9 MSI 29-240-00 RTE:9

emp emp

emp emp emp emp

MRB

MRB AMTOSS

Date: 23-jul-08

THRESHOLD INTERVAL

REFERENCES

ITEMS

27-225-01 27-225-02 MSI 27-225-01 RTE:6 MSI 27-225-02 RTE:6

27-81-00-710-801

I: 6000 FLH

E1 HHI 737-700

3 18-mar-05

I: 3600 FLH

F1 HHI 737-700

4 25-apr-06

I: 1250 FLH

F1 HHI 737-700

5 18-mar-05

I: 6000 FLH

F1 HHI 737-700

3 18-mar-05

ATA: 27 - 81

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 27 - 83

278300 71000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

LEADING EDGE AUTOSLAT SYSTEM FUNCTIONALLY CHECK THE AUTOSLAT SYSTEM TO INCLUDE A BITE 117 CHECK OF THE STALL MANAGEMENT/YAW DAMPER (SMYD) COMPUTER. 118 211 212

117A emp emp emp

ITEMS

MPD MRB

27-216-00 MSI 27-216-00 RTE:8

AMTOSS

27-83-00-710-801

I: 1250 FLH

ATA: 27 - 83

F2 HHI 737-700

5 03-jun-04

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

28

FUEL

28 - 00

FUEL

280000 03000

280000 04000

280000 05000

Date: 23-jul-08

DRAIN ALL TANKS (EXCEPT SURGE TANKS)

CHECK THAT FUELING STATION DOOR IS SECURED

VISUALLY CHECK DRAIN MAST AREAS AND DRAINS FOR LEAKAGE OF FUEL AND/OR HYDRAULIC FLUID

ZONE ACCESS

STRUCTURE

REFERENCES

530 630

emp emp

empty

630

emp

empty

100 434 444 500 600

emp emp emp emp emp

ITEMS

AMM

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

12-11-00 SERVICE EXPERIENCE

I: 4 Z

S

HHI 737-700

SM

2 11-dec-01

SERVICE EXPERIENCE

I: 1 T

S

HHI 737-700

SM

3 11-dec-01

SERVICE EXPERIENCE

I: 1 T

E1 HHI 737-700

SM

1 11-dec-01

empty

ATA: 28 - 00

Page 1 of 3


HHI

737-6

MAINTENANCE SCHEDULE

R E V

ITEM

DESCRIPTION

R

280000 06000

INSPECT (DETAILED) IN-TANK TUBING AND EQUIPMENT STATIC GROUND STRAPS AND CLAMPS FOR CONDITION, SECURITY AND OTHER DEGRADATION. (SFAR 88) NOTE( I ) PERFORM TASK CONCURRENTLY WITH OTHER FUEL TANK INSPECTION TASKS TO MINIMIZE TANK ENTRIES AND POSSIBLE ACCIDENTAL DAMAGE.

R

Date: 23-jul-08

ZONE ACCESS 131 emp 132 531 emp 532 emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp 533 emp emp emp emp 631 emp 632 emp emp emp emp emp emp emp emp

STRUCTURE

131AB 434CL 444CR 531AB 531BB 532AB 532AZ 532BB 532BZ 532CB 532DB 532EB 532FB 532GB 532HB 532JB 532KB 532LB 532MB 532NB 532PB 532QB 532RB 533AB 533BB 533CB 534AB 534BB 631AB 631BB 632AB 632AZ 632BB 632BZ 632CB 632DB 632EB 632FB 632GB

ITEMS

THRESHOLD INTERVAL

REFERENCES MRB MPD MRB AMTOSS AMTOSS AMTOSS

TSK

EFF

R L ITEM BY E E REVISION P V DATE

MSI 28-140-00 RTE:9 28-140-00 MSI 28-140-00 RTE:8 28-00-00-280-803 28-00-00-280-802 28-00-00-280-801

I: 10 YRS

ATA: 28 - 00

E3 HHI 737-700

4 23-jul-08

Page 2 of 3


HHI R E V

R

737-6

MAINTENANCE SCHEDULE ITEM

280000 76000

DESCRIPTION

FUNCTIONAL CHECK (RESISTANCE MEASUREMENT) OF THE EQUIPMENT FAULT CURRENT GROUND STRAP (S). (SFAR 88) NOTE( J, E ) NOTE (J): PUMP FAULT CURRENT GROUND STRAPS ARE EXTERNAL OF FUEL TANK. NOTE (E): IF THE APU FUEL BOOST PUMP IS INSTALLED

ZONE ACCESS emp emp emp emp emp emp emp emp emp 633 emp emp emp emp

632HB 632JB 632KB 632LB 632MB 632NB 632PB 632QB 632RB 633AB 633BB 633CB 634AB 634BB

131 132 531 551 631

emp emp emp 551DB emp

STRUCTURE

REFERENCES

MRB MRB MPD MPD MRB MRB

R

Date: 23-jul-08

AMM

ITEMS

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

MSI 28-150-00 RTE:9 MSI 28-160-00 RTE:9 28-150-00 28-160-00 MSI 28-150-00 RTE:8 MSI 28-160-00 RTE:8 28-00-00-76

I: 5 YRS I: 6 YRS

ATA: 28 - 00

F2 HHI 737-700

3 23-jul-08

Page 3 of 3


HHI R E V

ITEM 28 - 11

R

737-6

MAINTENANCE SCHEDULE

281100 01000

R

281100 21000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

FUEL TANKS EXTERNAL WIRES OVER CENTER FUEL TANK 211 (DETAILED INSPECTION) CONCERN: POTENTIAL FOR WIRE CHAFING AND ARCING TO CENTER FUEL TANK UPPER PANEL. PERFORM A DETAILED INSPECTION OF THE WIRE BUNDLES ROUTED ON MAIN DECK OVER THE CENTER FUEL TANK AND UNDER THE MAIN DECK FLOOR BOARDS PER AMM 28-11-00 TO DETECT DAMAGED CLAMPS, WIRE CHAFING, AND THAT THE WIRE BUNDLE IS NOT IN CONTACT WITH SURFACE OF THE CENTER FUEL TANK. IF DISCREPANCIES ARE FOUND, REPAIR PER THE STANDARD WIRING PRACTICES MANUAL D6-54446. NOTE( )

emp

INSPECT THE MAIN AND CENTER FUEL TANK (WING) EXTERNAL LOWER 531 SURFACES INCLUDING TANK VENTS, SUMP DRAIN VALVES, SKIN LAP 532 JOINTS FOR OBVIOUS LEAKS, CONDITION AND SECURITY. 533 631 632 633

emp emp emp emp emp emp

ITEMS

AAR AAR

28-AWL-01 ALI 28-AWL-01

AMM AMM

28-11-00-211-801 28-11-00-211-801

MPD MRB

28-010-00 MSI 28-010-00 RTE:9

AMTOSS

28-11-00-21

T: 10 YRS I: 10 YRS I: 36000 CYC

E3 HHI 737-700

1 23-jul-08

I: 4000 FLH

E1 HHI 737-700

1 03-jun-04

ATA: 28 - 11

Page 1 of 1


HHI R E V

ITEM 28 - 13 281331 10000

DESCRIPTION

ZONE ACCESS

STRUCTURE

281331 20000

DETAILED INSPECTION OF THE LEFT AND RIGHT SURGE TANK VENT FLAME ARRESTOR FOR CLOGGING, CONDITION AND SECURITY.

533 633

emp emp

MPD MPD MRB

281341 21000

FUNCTIONALLY CHECK (RESISTANCE MEASUREMENT) THE BONDING BETWEEN THE LOWER AIR VENT STACK AND THE DOOR STRUCTURE. (SFAR 88)

533 633

533BB 633BB

OPERATIONALLY CHECK THE LEFT AND RIGHT SURGE TANK RELIEF VALVES.

533 633

emp emp

FUNCTIONALLY CHECK (RESISTANCE MEASUREMENT) THE BONDING 533 BETWEEN THE PRESSURE RELIEF VALVE AND THE STRUCTURE. (SFAR 633 88)

533BB 633BB

N

Date: 23-jul-08

EFF

R L ITEM BY E E REVISION P V DATE

ITEMS

28-030-01 28-030-02 MSI 28-030-01 RTE:8 MSI 28-030-02 RTE:8

AMTOSS

28-13-31-100-801

MPD MRB

28-204-00 MSI 28-204-00 RTE:9

AMM

28-13-31-200

MPD MPD MRB

28-020-01 28-020-02 MSI 28-020-01 RTE:9 MSI 28-020-02 RTE:9

MRB

N

TSK

FUEL VENT SYSTEM

N 281341 20000

THRESHOLD INTERVAL

REFERENCES

MRB

N

737-6

MAINTENANCE SCHEDULE

AMTOSS

28-13-41-20

MPD MRB

28-205-00 MSI 28-205-00 RTE:9

AMM

28-13-41-200

I: 3 YRS

E3 HHI 737-700

2 03-jun-04

T: 12 YRS I: 12 YRS

F2 HHI 737-700

0 23-jul-08

I: 3 YRS

F1 HHI 737-700

1 03-jun-04

T: 12 YRS I: 12 YRS

F2 HHI 737-700

0 23-jul-08

ATA: 28 - 13

Page 1 of 1


HHI R E V

ITEM 28 - 21

N

282111 20000

DESCRIPTION

ZONE ACCESS

STRUCTURE

282151 20000

FUNCTIONALLY CHECK (RESISTANCE MEASUREMENT) THE BONDING 621 BETWEEN THE FUELING RECEPTACLE (MANIFOLD) AND THE STRUCTURE. (SFAR 88)

621GB

FUNCTIONALLY CHECK (RESISTANCE MEASUREMENT) THE BONDING OF THE FUELING SHUTOFF VALVE ACTUATOR (SOLENOID) TO THE ADJOINING STRUCTURE. (SFAR 88)

621

621GB

N

Date: 23-jul-08

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

PRESSURE FUELING SYSTEM

N N

737-6

MAINTENANCE SCHEDULE

ITEMS

MPD MRB

28-208-00 MSI 28-208-00 RTE:9

AMM

28-21-11-200

MPD MRB

28-207-00 MSI 28-207-00 RTE:9

AMM

28-21-51-200-801

T: 12 YRS I: 12 YRS

F2 HHI 737-700

0 23-jul-08

T: 12 YRS I: 12 YRS

F2 HHI 737-700

0 23-jul-08

ATA: 28 - 21

Page 1 of 1


HHI R E V

ITEM 28 - 22

R

282200 20000

R

R

737-6

MAINTENANCE SCHEDULE

282200 21000

R

282200 71000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

ENGINE FUEL FEED SYSTEM PERFORM A DETAILED VISUAL INSPECTION OF THE FOLLOWING ITEMS ON ALL THE FUEL PUMPS FOR SIGNS OF FUEL LEAKS, HEAT DISCOLORATION OR DAMAGE: - WIRE TERMINAL ASSEMBLY - ELECTRICAL CONNECTOR - WIRE INSULATION NOTE: THIS TASK ACCOMPLISHES CERTIFICATION MAINTENANCE REQUIREMENT 28-CMR-01. IF ANY DISCREPANCY IS DETECTED, PRIOR TO FURTHER FLIGHT, REPLACE THE FUEL PUMP WITH A NEW OR SERVICEABLE FUEL PUMP AND PERFORM AN INSULATION RESISTANCE TEST PER 28-CMR-02 NOTE( E ) THIS CMR TASK IS ONLY APPLICABLE TO THE FOLLOWING 737NG MAIN TANK FUEL BOOST PUMPS PARTNUMBERS: 60B92404-6 AND 60B92404-7, AND CENTER WING TANK OVERRIDE FUEL PUMPS PARTNUMBERS: 60B89004-10 AND 60B89004-12.

131 132 531 631

emp emp emp emp

AAR

PERFORM AN INSULATION RESISTANCE TEST ON ALL OF THE FUEL PUMPS. NOTE : THIS TASK ACCOMPLISHES CERTIFICATION MAINTENANCE REQUIREMENT 28-CMR-02. IF ANY RESISTANCE MEASUREMENT IS LESS THAN 5 MEGAOHM, PRIOR TO FURTHER FLIGHT, REPLACE THE FUEL PUMP WITH A NEW OR SERVICEABLE FUEL PUMP AND REPEAT INSULATION RESISTANCE TEST. NOTE( E ) THIS CMR TASK IS ONLY APPLICABLE TO THE FOLLOWING 737NG MAIN TANK FUEL BOOST PUMP PARTNUMBERS: 60B92404-6 AND 60B92404-7, AND CENTER WING TANK OVERRIDE FUEL PUMP PARTNUMBERS: 60B89004-10 AND 60B89004-12

131 132 531 631

emp emp emp emp

AAR

AMTOSS

28-22-00-200-801

OPERATIONALLY CHECK ENGINE FUEL SUCTION FEED SYSTEM

211 212

emp emp

MPD MRB

28-050-00 MSI 28-050-00 RTE:8

AMM AMM

28-22-15-710-801 28-22-00-710

ITEMS

MPD

28-CMR-01 ONE STAR 28-100-00

AMTOSS

MPD

28-22-00-210-801

I: 5000 FLH I: 18 MTH

E3 HHI I1 737-700 W1

8 23-jul-08

I: 5000 FLH I: 18 MTH

M2 HHI 737-700

6 23-jul-08

I: 7500 FLH

F1 HHI 737-700

1 05-sep-06

28-CMR-02 ONE STAR 28-110-00

ATA: 28 - 22

Page 1 of 4


HHI R E V

ITEM 282200 72000

282200 72100

N

737-6

MAINTENANCE SCHEDULE

282211 20000

N

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

OPERATIONALLY CHECK THE CENTER TANK FUEL SCAVENGE SYSTEM 211 (JET PUMP, INDUCED PORT CHECK VALVE, FLOAT VALVE AND LINE). 212

OPERATIONALLY CHECK THE FUEL SHUTOFF VALVE BATTERY

FUNCTIONALLY CHECK (RESISTANCE MEASUREMENT) THE BONDING BETWEEN MOTOR OPERATED VALVE ACTUATOR AND ADJOINING STRUCTURE. (SFAR 88) NOTE( J ) THIS TASK IS PERFORMED FROM OUTSIDE OF TANK.

212 551 651

132 521 621

STRUCTURE

emp emp

emp emp emp

emp 521BB 621BB

ITEMS

REFERENCES MPD MRB

28-040-00 MSI 28-040-00 RTE:9

AMTOSS

28-22-00-72

MPD MRB

28-125-00 MSI 28-125-00 RTE:9

AMTOSS

28-22-00-72

MPD MRB

28-211-00 MSI 28-211-00 RTE:9

AMM AMM

28-22-11-200 28-22-21-200

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

I: 10000 FLH

F1 HHI 737-700

1 03-jun-04

I: 6000 FLH

F1 HHI 737-700

2 18-mar-05

T: 12 YRS I: 12 YRS

F2 HHI 737-700

0 23-jul-08

ATA: 28 - 22

Page 2 of 4


HHI

737-6

MAINTENANCE SCHEDULE

R E V

ITEM

N

282211 72000

N

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

LIGHTNING AND FAULT CURRENT PROTECTION - MOTOR OPERATED 521 VALVE (MOV) ACTUATOR 621 CONCERN: POTENTIAL FOR ARCING OR SPARKING INSIDE THE FUEL TANK AT A CONDUCTIVE METAL-TO-GROUND STRUCTURE INTERFACE AS A RESULT OF LIGHTNING OR ELECTRICAL FAULT CURRENT EVENT. PERFORM THE FOLLOWING FUNCTIONAL CHECK (PER BOEING AMM 28-22-11) TO ENSURE THE INTEGRITY OF THE SPAR VALVE ACTUATOR ELECTRICAL BONDING PATH: 1. DISCONNECT THE ELECTRICAL CONNECTOR. 2. DISCONNECT THE BONDING JUMPER. 3. WITH THE ACTUATOR ELECTRICAL CONNECTOR AND THE BONDING JUMPER DISCONNECTED, VERIFY ELECTRICAL BONDING RESISTANCE BETWEEN THE CONNECTOR FLANGE AND THE SPAR WEB IS 0.010 OHMS (10 MILLIOHMS) OR LESS. 4. ATTACH THE BONDING JUMPER TO THE ACTUATOR UPPER HOUSING USING A SEALED ELECTRICAL FAY SURFACE BOND AND VERIFY ELECTRICAL BONDING RESISTANCE BETWEEN THE HOUSING AND THE ATTACHED BONDING JUMPER TERMINAL IS 0.001 OHMS (1 MILLIOHM) OR LESS. 5. WITH THE ACTUATOR ELECTRICAL CONNECTOR DISCONNECTED, VERIFY ELECTRICAL BONDING RESISTANCE BETWEEN THE OUTERMOST FQIS SHIELD GROUND TERMINAL AND THE SPAR WEB IS 0.014 OHMS (14 MILLIOHMS) OR LESS. NOTE( E, T ) NOTE(E) ALL AIRPLANES LINE NUMBER 1877-1980, 1982, AND AIRPLANES THAT HAVE INC. SB 737-28A1207. NOTE(T) T: DATE OF EMBODIMENT SB 737-28A1207.

STRUCTURE

emp emp

ITEMS

THRESHOLD INTERVAL

REFERENCES AAR AAR

28-AWL-24 FAA AD 2008-06-03

AMM AMM EO

28-22-11-720-801 28-00-00-910-801 155334

T: 1 s.N I: 6 YRS

ATA: 28 - 22

TSK

EFF

FC HHI 737-700

R L ITEM BY E E REVISION P V DATE

0 23-jul-08

Page 3 of 4


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

282213 20000

DESCRIPTION RESTORE (CLEAN) THE LEFT AND RIGHT MAIN FUEL TANK AND BOTH CENTER WING FUEL TANK WATER SCAVENGE JET PUMPS (WITHOUT DEFUELING THE TANK).

ZONE ACCESS 133 134 532 632

STRUCTURE

emp emp emp emp

REFERENCES MPD MPD MPD MRB MRB MRB

282214 00000

Date: 23-jul-08

REPLACE THE FUEL SHUT-OFF VALVE BATTERY NOTE( R ) FOR COMPLETENESS ONLY, COVERED BY CMS

212

emp

ITEMS

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

28-060-01 28-060-02 28-060-03 MSI 28-060-01 RTE:9 MSI 28-060-02 RTE:9 MSI 28-060-03 RTE:9

AMTOSS

28-22-13-20

MPD MRB

28-130-00 MSI 28-130-00 RTE:9

AMTOSS AMTOSS

28-22-14-40 28-22-14-00

I: 4000 FLH

S

HHI 737-700

5 18-mar-05

I: 7 YRS

S

HHI 737-700

2 03-jun-04

ATA: 28 - 22

Page 4 of 4


HHI R E V

ITEM 28 - 25

N

737-6

MAINTENANCE SCHEDULE

282502 20000

DESCRIPTION

ZONE ACCESS

STRUCTURE

Date: 23-jul-08

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

APU FUEL FEED SYSTEM FUNCTIONALLY CHECK (RESISTANCE MEASUREMENT) THE BONDING RESISTANCE BETWEEN THE APU SHUTOFF VALVE ACTUATOR AND ADJOINING STRUCTURE. (SFAR 88)

133

emp

N 282505 79000

REFERENCES

FUNCTIONALLY (PRESSURE DECAY) CHECK THE APU FUEL LINE SHROUD. 145

emp

ITEMS

MPD MRB

28-213-00 MSI 28-213-00 RTE:9

AMM

28-25-02-200

MPD MRB

28-070-00 MSI 28-070-00 RTE:8

AMTOSS

28-25-05-79

T: 12 YRS I: 12 YRS

F2 HHI 737-700

0 23-jul-08

I: 12000 FLH

F2 HHI 737-700

1 03-jun-04

ATA: 28 - 25

Page 1 of 1


HHI R E V

ITEM 28 - 41

R

737-6

MAINTENANCE SCHEDULE

284100 01000

R

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

FUEL QUANTITY INDICATING SYSTEM (FQIS) DETAILED INSPECTION (VISUAL) OF THE FQIS IN TANK WIRE HARNESS, COMPENSATOR AND TANK UNITS FOR SIGNS OF CHAFING OR RUBBING. (SFAR 88) (EZAP) NOTE( I ) PERFORM TASK CONCURRENTLY WITH OTHER FUEL TANK INSPECTION TASKS TO MINIMIZE TANK ENTRIES AND POSSIBLE ACCIDENTAL DAMAGE.

131 132 531 emp 532 emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp 631 emp 632 emp emp emp emp emp emp emp emp emp emp emp emp

434CL 444CR 531AB 531BB 532AB 532AZ 532BB 532BZ 532CB 532DB 532EB 532FB 532GB 532HB 532JB 532KB 532LB 532MB 532NB 532PB 532QB 532RB 631AB 631BB 632AB 632AZ 632BB 632BZ 632CB 632DB 632EB 632FB 632GB 632HB 632JB 632KB 632LB

ITEMS

MPD MRB

28-170-00 MSI 28-170-00 RTE:8

AMTOSS AMTOSS AMTOSS

28-41-44-280-803 28-41-44-280-802 28-41-44-280-801

I: 10 YRS

ATA: 28 - 41

E3 HHI 737-700

5 23-jul-08

Page 1 of 6


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

ZONE ACCESS emp emp emp emp emp

Date: 23-jul-08

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

632MB 632NB 632PB 632QB 632RB

ITEMS

ATA: 28 - 41

Page 2 of 6


HHI

737-6

MAINTENANCE SCHEDULE

R E V

ITEM

N

284100 28000

N

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

INSPECT (DETAILED) THE IN-TANK FQIS COMPONENTS FOR CHAFING, 131 RUBBING, ADEQUATE SEPARATION FROM STRUCTURE AND CONDITION emp FOR SECURITY. (SFAR 88) 132 531 emp 532 emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp 631 emp 632 emp emp emp emp emp emp emp emp emp emp emp emp emp

STRUCTURE

131AB 434CL 444CR 531AB 531BB 532AB 532AZ 532BB 532BZ 532CB 532DB 532EB 532FB 532GB 532HB 532JB 532KB 532LB 532MB 532NB 532PB 532QB 532RB 631AB 631BB 632AB 632AZ 632BB 632BZ 632CB 632DB 632EB 632FB 632GB 632HB 632JB 632KB 632LB 632MB

ITEMS

REFERENCES MPD MRB

28-171-00 MSI 28-171-00 RTE:8

AMM

28-41-44-280

THRESHOLD INTERVAL

T: 10 YRS I: 10 YRS

ATA: 28 - 41

TSK

EFF

E3 HHI 737-700

R L ITEM BY E E REVISION P V DATE

0 23-jul-08

Page 3 of 6


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

ZONE ACCESS emp emp emp emp

Date: 23-jul-08

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

632NB 632PB 632QB 632RB

ITEMS

ATA: 28 - 41

Page 4 of 6


HHI

737-6

MAINTENANCE SCHEDULE

R E V

ITEM

DESCRIPTION

N

284100 29000

FUNCTIONALLY CHECK (RESISTANCE MEASUREMENT) OUT TANK FQIS WIRE BUNDLE LIGHTNING SHIELD TO GROUND TERMINATION. (SFAR 88) CONCERN: POTENTIAL FOR LIGHTNING INDUCED VOLTAGES ON THE FQIS WIRING TO ENTER THE FUEL TANK. PERFORM THE FOLLOWING FUNCTIONAL CHECK TO ENSURE THE INTEGRITY OF THE FQIS WIRING SHIELD TO GROUND TERMINATION: 1. VERIFY THE RESISTANCE OF THE SHIELD TO GROUND TERMINATIONS AT SIDE OF BODY, AND AT THE SPAR PENETRATION IN THE UNPRESSURIZED AREA BY MAKING THE FOLLOWING MEASUREMENTS USING A LOOP RESISTANCE TESTER P/N 906-10246-2 OR 906-10246-3 PER BOEING AMM 05-55-54. RESTORE THE BONDS PER THE BOEING AMM IF REQUIRED. PERFORM A LOOP RESISTANCE MEASUREMENT WHERE THE WIRE BUNDLE ENTERS THE FUEL TANK: 1. THE LOOP RESISTANCE SHALL NOT EXCEED 138 MILLIOHMS FOR CONNECTOR D11312 (LEFT MAIN TANK WITHOUT DENSITOMETER) WIRE BUNDLE W1140. 2. THE LOOP RESISTANCE SHALL NOT EXCEED 63 MILLIOHMS FOR CONNECTOR D11312 (LEFT MAIN TANK WITH DENSITOMETER) WIRE BUNDLE W1140. 3. THE LOOP RESISTANCE SHALL NOT EXCEED 138 MILLIOHMS FOR CONNECTOR D11314 (RIGHT MAIN TANK WITHOUT DENSITOMETER) WIRE BUNDLE W1138. 4. THE LOOP RESISTANCE SHALL NOT EXCEED 63 MILLIOHMS FOR CONNECTOR D11314 (RIGHT MAIN TANK WITH DENSITOMETER) WIRE BUNDLE W1138. 5. THE LOOP RESISTANCE SHALL NOT EXCEED 40 MILLIOHMS FOR CONNECTOR D11316 (CENTER TANK WITHOUT DENSITOMETER) WIRE BUNDLE W7580. 6. THE LOOP RESISTANCE SHALL NOT EXCEED 40 MILLIOHMS FOR CONNECTOR D11316 (CENTER TANK WITH DENSITOMETER) WIRE BUNDLE W7580. NOTE( T ) (1)WITHIN 120 MONTHS SINCE THE DATE OF ISSUANCE OF THE ORIGINAL STANDARD AIRWORTHINESS CERTIFICATION OR THE DATE OF ISSUANCE OF THE ORIGINAL EXPORT CERTIFICATION OF AIRWORTHINESS. (2) WITHIN 24 MONTHS AFTER THE EFFECTIVE DATE OF AD 2008-10-09 (12-JUN-08), THEREFORE 12-JUN-10. WHICHEVER OCCURS LATER!

N

Date: 23-jul-08

ZONE ACCESS 133 510 emp 610 emp

STRUCTURE

emp 511AT 521BB 611AT 621BB

ITEMS

REFERENCES AAR MPD MRB

ALI 28-AWL-03 28-173-00 MSI 28-173-00 RTE:8

AMM

05-55-54-200

THRESHOLD INTERVAL

T: 1 s.N I: 10 YRS

ATA: 28 - 41

TSK

EFF

F2 HHI 737-700

R L ITEM BY E E REVISION P V DATE

0 23-jul-08

Page 5 of 6


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

284100 71000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

OPERATIONALLY (BITE) CHECK THE FUEL QUANTITY INDICATING SYSTEM. 210 632

STRUCTURE

emp 621GB

ITEMS

REFERENCES MPD MRB

28-080-00 MSI 28-080-00 RTE:9

AMTOSS

28-41-00-71

THRESHOLD INTERVAL

I: 6000 FLH

ATA: 28 - 41

TSK

EFF

F1 HHI 737-700

R L ITEM BY E E REVISION P V DATE

1 03-jun-04

Page 6 of 6


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

29

HYDRAULIC POWER

29 - 00

HYDRAULIC POWER

290000 01000

290000 01100

290000 06000

290011 01000

Date: 23-jul-08

ZONE ACCESS

STRUCTURE

113 134

emp emp

empty

113 134

emp emp

empty

OPERATIONALLY CHECK THE STANDBY HYDRAULIC ELECTRIC MOTOR 211 DRIVEN PUMP TO INCLUDE OBSERVING LOW PRESSURE LIGHT 212 ILLUMINATION AND THEN GOING OUT.

emp emp

HYDRAULIC FLUID SAMPLING A- AND B-SYSTEM

HYDRAULIC FLUID SAMPLING STANDBY-SYSTEM

PTU OPERATIONAL CHECK. 139 PERFORM AN OPERATIONALLY CHECK OF THE POWER TRANSFER UNIT 211 CONTROL SYSTEM TO INCLUDE A VISUAL CHECK OF THE CONTROL 212 VALVE FOR PROPER POSITION.

emp emp emp

ITEMS

THRESHOLD INTERVAL

REFERENCES

AMM

TSK

EFF

R L ITEM BY E E REVISION P V DATE

29-11-00-200-801

I: 25000 FLH

S

HHI 737-700

0 11-dec-01

AMM

29-11-00-200-801

I: 25000 FLH

S

HHI 737-700

0 11-dec-01

MPD MRB

29-200-00 MSI 29-200-00 RTE:8

AMTOSS

29-34-31-400-801PAR.E I: 5000 FLH

F1 HHI 737-700

5 03-jun-04

MPD MRB

29-250-00 MSI 29-250-00 RTE:8

AMTOSS

29-22-00-710-801

F1 HHI E1 737-700

5 18-mar-05

I: 6000 FLH

ATA: 29 - 00

Page 1 of 1


HHI R E V

ITEM 29 - 11 291100 20000

291100 30000

291102 00000

291103 00000

N

737-6

MAINTENANCE SCHEDULE

291104 20000

DESCRIPTION

ZONE ACCESS

STRUCTURE

TSK

EFF

R L ITEM BY E E REVISION P V DATE

MAIN HYDRAULIC POWER SYSTEM GROSS HYDRAULIC SYSTEM LEAKAGE CHECK.

133 134 211 212

emp emp emp emp

MPD MRB

29-010-00 MSI 29-010-00 RTE:6

AMM AMM AMM AMM

29-00-00-790-802 29-00-00-790-803 29-00-00-790-804 29-00-00-790-808

OPERATIONALLY CHECK THE A & B SYSTEM ENGINE DRIVEN PUMP (EDP) 133 SHUTOFF VALVES. 134 210

emp emp emp

MPD MRB

29-100-00 MSI 29-100-00 RTE:8

AMM

29-11-81-710-801

emp emp 192CL 192CR

MPD MRB

29-070-00 MSI 29-070-00 RTE:6

AMTOSS AMTOSS AMTOSS AMTOSS

29-11-02-400-802 29-11-02-000-802 29-09-01-000-801 29-09-01-400-801

DETAILED INSPECTION AND CHECK FOR CLOGGED CONDITION OF THE 133 RESERVOIR PRESSURIZATION MODULE VENT CAP 134 NOTE( E ) APPLICABLE TO AIRPLANES THAT HAVE NOT INCORPORATED SB 737-29-1106

emp emp

MPD MRB

29-060-00 MSI 29-060-00 RTE:6

AMTOSS

29-11-03-220-801

FUNCTIONALLY CHECK (RESISTANCE MEASUREMENT) THE BONDING RESISTANCE BETWEEN THE HYDRAULIC LINE FITTING AT FUEL TANK WALL PENETRATIONS AND THE ADJOINING STRUCTURE. (SFAR 88)

551DB

MPD MRB

28-201-00 MSI 28-201-00 RTE:9

AMM

29-11-04-200

CLEAN THE RESERVOIR PRESSURIZATION MODULE FILTER

133 134 192 emp

532

N

Date: 23-jul-08

THRESHOLD INTERVAL

REFERENCES

ITEMS

I: 12000 FLH

F2 HHI 737-700

5 25-apr-06

I: 6000 FLH

F1 HHI 737-700

4 22-mar-07

I: 4000 FLH

S

HHI 737-700

3 30-nov-05

I: 4000 FLH

E3 HHI 737-700

4 25-apr-06

T: 12 YRS I: 12 YRS

F2 HHI 737-700

0 23-jul-08

ATA: 29 - 11

Page 1 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

291121 00000

291141 00000

DESCRIPTION

ZONE ACCESS

STRUCTURE

OPERATIONAL CHECK OF EMDP GROUND FAULT PROTECTION SYSTEM 133 134 211 212

emp emp 117A emp

MPD MRB

29-080-00 MSI 29-080-00 RTE:6

AMTOSS

29-11-21-700-802

REPLACE THE "A" AND "B" HYDRAULIC SYSTEM ELECTRIC MOTOR DRIVEN 133 PUMP (EMDP) CASE DRAIN FILTER 134

emp emp

MPD MPD MRB

29-030-01 29-030-02 MSI 29-030-01 RTE:6 MSI 29-030-02 RTE:6

MRB

291151 00000

REPLACE "A" AND "B" SYSTEM EDP CASE DRAIN FILTERS

411 421

413 423

AMTOSS AMTOSS

29-11-41-400-801 29-11-41-000-801

MPD MPD MRB

29-050-01 29-050-02 MSI 29-050-01 RTE:6 MSI 29-050-02 RTE:6

MRB

291161 00000

291171 40000

INSPECT (GENERAL VISUAL) THE DELTA "P" INDICATION OF A & B SYSTEM 133 RETURN FILTER MODULE. 134

REPLACE A & B SYSTEM ENGINE DRIVEN PUMP (EDP) AND ELECTRIC MOTOR DRIVEN PUMP (EMDP) PRESSURE FILTERS.

133 134

emp emp

emp emp

AMTOSS AMTOSS

29-11-51-400-801 29-11-51-000-801

MPD MRB

29-090-00 MSI 29-090-00 RTE:9

AMTOSS

29-11-61-210-801

MPD MPD MRB

29-020-00 29-040-00 MSI 29-020-00 RTE:6 MSI 29-040-00 RTE:6

MRB AMTOSS AMTOSS

Date: 23-jul-08

THRESHOLD INTERVAL

REFERENCES

ITEMS

29-11-71-000-802 29-11-71-400-802

TSK

EFF

R L ITEM BY E E REVISION P V DATE

I: 4000 FLH

F1 HHI 737-700

1 03-jun-04

I: 600 FLH

S

HHI 737-700

4 18-mar-05

I: 2400 FLH

S

HHI 737-700

4 25-apr-06

I: 600 FLH

E2 HHI 737-700

2 18-mar-05

I: 8000 FLH

S

3 03-jun-04

ATA: 29 - 11

HHI 737-700

Page 2 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 29 - 18

291811 00000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

GROUND SERVICING SYSTEM REPLACE THE GROUND HYDRAULIC RESERVOIR FILL FILTER.

133 134

emp emp

ITEMS

MPD MRB

29-180-00 MSI 29-180-00 RTE:9

AMTOSS AMTOSS

29-18-11-400-802 29-18-11-000-802

I: 16000 FLH

ATA: 29 - 18

S

HHI 737-700

2 03-jun-04

Page 1 of 1


HHI R E V

ITEM 29 - 21 292100 60000

292100 61000

R

737-6

MAINTENANCE SCHEDULE

292100 70000

DESCRIPTION

ZONE ACCESS

STRUCTURE

FUNCTIONALLY CHECK STANDBY HYDRAULIC SYSTEM FOR INTERNAL 133 LEAKAGE. NOTE: THIS TASK IS SATISFIED BY ACCOMPLISHMENT OF TASK 134 27-054-00. 211 212

emp emp emp emp

MPD MRB

29-190-00 MSI 29-190-00 RTE:8

AMM

29-00-00-790-808

FUNCTIONALLY CHECK THE STANDBY RUDDER POWER CONTROL UNIT 133 FOR INTERNAL LEAKAGE IN A LOADED CONDITION. 134 211 212

emp emp emp emp

MPD MRB

27-054-00 MSI 27-054-00 RTE:8

AMM

29-00-00-790-808

OPERATIONALLY CHECK THE STANDBY RUDDER SYSTEM. TO INCLUDE OBSERVING LOW PRESSURE LIGHT ILLUMINATION AND THEN EXTINGUISHING. NOTE( )

emp emp emp emp

MPD MPD MPD MRB

27-052-00 29-200-00 29-230-00 MSI 27-052-00 RTE:8 MSI 29-200-00 RTE:8 MSI 29-230-00 RTE:8

133 134 211 212

MRB R

292151 00000

Date: 23-jul-08

TSK

EFF

R L ITEM BY E E REVISION P V DATE

STANDBY HYDRAULIC SYSTEM

MRB

292141 00000

THRESHOLD INTERVAL

REFERENCES

REPLACE THE STANDBY HYDRAULIC SYSTEM CASE DRAIN FILTER.

REPLACE THE STANDBY HYDRAULIC SYSTEM PRESSURE FILTER

139

139

emp

emp

ITEMS

AMTOSS

29-21-00-700-803

MPD MRB

29-220-00 MSI 29-220-00 RTE:8

AMTOSS AMTOSS

29-21-41-400-801 29-21-41-000-801

MPD MRB

29-210-00 MSI 29-210-00 RTE:8

AMTOSS AMTOSS

29-21-51-400-802 29-21-51-000-802

I: 25000 FLH

F2 HHI 737-700

1 22-mar-07

I: 12500 FLH

F2 HHI 737-700

0 30-nov-05

I: 1 s.N I: 180 DAY I: 1200 FLH

F1 HHI 737-700

7 23-jul-08

I: 12000 FLH

S

HHI 737-700

4 22-mar-07

I: 12000 FLH

S

HHI 737-700

4 22-mar-07

ATA: 29 - 21

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 29 - 22

292200 73000

292201 71000

292221 02000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

POWER TRANSFER SYSTEM FUNCTIONALLY CHECK THE POWER TRANSFER UNIT.

211 212

OPERATIONALLY CHECK THE POWER TRANSFER UNIT ISOLATION CHECK 139 VALVE. 211 212

REPLACE THE POWER TRANSFER UNIT PRESSURE FILTER.

133 134

emp emp

emp emp emp

emp emp

ITEMS

MPD MRB

29-260-00 MSI 29-260-00 RTE:8

AMTOSS

29-22-00-730-801

MPD MRB

29-280-00 MSI 29-280-00 RTE:8

AMTOSS

29-22-00-710-801

MPD MRB

29-270-00 MSI 29-270-00 RTE:8

AMTOSS AMTOSS

29-22-21-400-802 29-22-21-020-801

I: 25000 FLH

F2 HHI 737-700

1 03-jun-04

I: 25000 FLH

F1 HHI 737-700

2 22-mar-07

I: 12000 FLH

S

5 22-mar-07

ATA: 29 - 22

HHI 737-700

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 29 - 32

293200 73000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

HYDRAULIC FLUID TEMPERATURE INDICATING SYSTEM FUNCTIONALLY CHECK THE A & B HYDRAULIC SYSTEM CASE DRAIN WARNING SWITCHES.

133 134 210

emp emp emp

ITEMS

MPD MRB

29-310-00 MSI 29-310-00 RTE:9

AMTOSS

29-32-00-730-802

I: 25000 FLH

ATA: 29 - 32

F2 HHI 737-700

3 03-jun-04

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 31 31 - 31

313100 97000

313109 70000

DESCRIPTION

ZONE ACCESS

STRUCTURE

TSK

EFF

R L ITEM BY E E REVISION P V DATE

INDICATING & RECORDING SYSTEMS FLIGHT DATA RECORDER SYSTEM FUNCTIONAL CHECK OF REQUIRED PARAMETERS (FDR, DFDAU OUTPUT, 118 INTERFACING SYSTEMS) BY 242 DOWNLOADING FDR DATA. (CHECK OF DATA IS DONE OFF AIRCRAFT) NOTE( I ) MRB INTERVAL IS 6000 FLH

OPERATIONAL CHECK OF THE ULB AT BATTERY REPLACEMENT. NOTE( I ) AT BATTERY REPLACEMENT

242

emp emp

MPD MPD MRB MRB

emp

NFL II-56/01 2.3.7 31-31-00-97

MPD MPD MRB

31-140-00 31-150-00 MSI 31-140-00 RTE:9 MSI 31-150-00 RTE:9

MS AMTOSS AMTOSS AMTOSS AMTOSS

ITEMS

31-120-00 31-130-00 MSI 31-120-00 RTE:7 MSI 31-130-00 RTE:7

AAR AMTOSS

MRB

Date: 23-jul-08

THRESHOLD INTERVAL

REFERENCES

CM3131 00010 31-31-09-00 31-31-09-96 31-31-09-40 31-31-09-70

I: 24 MTH I: 1 s.N

F2 HHI 737-700

3 18-mar-05

I: 1 s.N

F1 HHI 737-700

2 03-jun-04

ATA: 31 - 31

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 31 - 51

315100 73000

315100 74000

315101 73000

315102 73000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

CENTRAL WARNING SYSTEMS OPERATIONAL CHECK OF MACH / AIRSPEED SYSTEMS 1 AND 2 DISCRETE 210 OUTPUTS FOR AURAL WARNING SYSTEM.

FUNCTIONAL CHECK OF THE AURAL WARNING MODULE (AWM) USING BITE CHECK.

211 212

OPERATIONAL CHECK OF LANDING GEAR LOGIC MODULE OUTPUT TO 211 THE AWM SYSTEMS 1 & 2. 212

FUNCTIONAL CHECK OF THE TRAILING EDGE AND LEADING EDGE FLAP, 211 THRUST LEVER, UPPER AND LOWER STABILIZER TRIM LIMIT, GROUND 212 SPOILER PRESSURE, SPEED BRAKE, PARK BRAKE AND GROUND SPOILER BYPASS VALVE SWITCHES FOR THE AURAL WARNING MODULE (AWM).

emp

emp emp

emp emp

emp emp

ITEMS

MPD MRB

31-030-00 MSI 31-030-00 RTE:9

AMTOSS

34-16-00-730-802

MPD MRB

31-010-00 MSI 31-010-00 RTE:6

AMTOSS

31-51-00-740-801

MPD MRB

31-040-00 MSI 31-040-00 RTE:8

AMTOSS

31-51-00-730-802

MPD MRB

31-050-00 MSI 31-050-00 RTE:8

AMTOSS

31-51-00-730-803

I: 6000 FLH

F1 HHI 737-700

4 18-mar-05

I: 6000 FLH

F2 HHI 737-700

3 18-mar-05

I: 6000 FLH

F1 HHI 737-700

4 18-mar-05

I: 6000 FLH

F2 HHI 737-700

3 18-mar-05

ATA: 31 - 51

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 31 - 62

316200 00000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

COMMON DISPLAY SYSTEM COMMON DISPLAY SYSTEMS INSPECT AND CLEAN THE F/O AND CENTER UPPER DISPLAY UNIT AIR INLET SCREEN ACCORDING AMM SECTION 31-62-11

211 212

emp emp

ITEMS

MPD MRB

31-160-00 MSI 31-160-00 RTE:6

AMM

31-62-11-100

I: 12 MTH

ATA: 31 - 62

S HHI E2 737-700 F1

2 22-mar-07

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 32 32 - 00

320000 01000

DESCRIPTION

ZONE ACCESS

STRUCTURE

LUBRICATE THE LEFT AND RIGHT MAIN LANDING GEAR ASSEMBLY.

734 744

551DB 651DB

MPD MPD MRB

MRB

Date: 23-jul-08

R L ITEM BY E E REVISION P V DATE

LUBRICATE THE NOSE LANDING GEAR ASSEMBLY.

713

emp

CHECK BRAKE ACCUMULATOR PRECHARGE PRESSURE, SERVICE AS REQUIRED.

133 211 212

CHECK NOSE AND MAIN LANDING GEAR TIRES FOR PROPER INFLATION. 713 SERVICE AS REQUIRED. 733 744 NOTE( I ) 48 ELAPSED CLOCK HOURS

emp emp emp

emp emp emp

ITEMS

32-030-01 32-030-02 MSI 32-030-01 RTE:6 MSI 32-030-01 RTE:8 MSI 32-030-02 RTE:6 MSI 32-030-02 RTE:8

AMTOSS AMTOSS

12-25-07-06 12-21-11-64

MPD MRB

32-080-00 MSI 32-080-00 RTE:6 MSI 32-080-00 RTE:8

MRB

320000 05000

EFF

GENERAL

MRB

320000 04000

TSK

LANDING GEAR

MRB

320000 03000

THRESHOLD INTERVAL

REFERENCES

AMTOSS

12-21-21-64

MPD MRB

32-300-00 MSI 32-300-00 RTE:9

AMTOSS AMTOSS

12-15-11-420-801 12-15-11-610-801

MPD MRB

32-350-00 MSI 32-350-00 RTE:9

AMTOSS AMTOSS AMTOSS

12-15-51-42 12-15-51-78 12-15-51-61

I: 560 CYC I: 90 DAY

S

HHI 737-700

4 22-mar-07

I: 560 CYC I: 90 DAY

S

HHI 737-700

3 22-mar-07

I: 1200 FLH

S

HHI 737-700

4 25-apr-06

I: 1 Z

S

HHI 737-700

4 22-mar-07

ATA: 32 - 00

Page 1 of 8


HHI R E V

ITEM 320000 08000

320000 09000

DESCRIPTION SERVICE THE NOSE LANDING GEAR SHOCK STRUT.

SERVICE THE LEFT AND RIGHT MLG SHOCK STRUT.

ZONE ACCESS 115 116

734 744

STRUCTURE

emp emp

emp emp

REFERENCES MPD MRB

32-070-00 MSI 32-070-00 RTE:9

AMTOSS

12-15-41-61

MPD MPD MRB

32-020-01 32-020-02 MSI 32-020-01 RTE:9 MSI 32-020-02 RTE:9

MRB AMTOSS 320000 11000

320000 21000

R

737-6

MAINTENANCE SCHEDULE

320000 31000

713 734 744

emp emp emp

empty

BRAKES FOR WEAR, DAMAGE AND LEAKAGE (PARKING BRAKE NOT SET)

734 744

emp emp

empty

INSPECT TIRES FOR WEAR AND DAMAGE

713 734 744

emp emp emp

empty

713 734 744

emp emp emp

empty

NLG AND MLG STRUCTURE AND COMPONENTS

R 320000 41000

Date: 23-jul-08

WHEELS FOR DAMAGE AND PARTICULAR FOR MISSING OR DEFECT TIEBOLTS

ITEMS

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

I: 3000 CYC

S

HHI 737-700

1 03-jun-04

12-15-31-61

I: 4000 CYC

S

HHI 737-700

2 22-mar-07

SERVICE EXPERIENCE

I: 1 T

E1 HHI 737-700

FC

0 24-mar-99

SERVICE EXPERIENCE

I: 1 T

E1 HHI 737-700

FC

0 24-mar-99

SERVICE EXPERIENCE

I: 1 T

E1 HHI 737-700

FC

1 23-jul-08

SERVICE EXPERIENCE

I: 1 T

E1 HHI 737-700

FC

0 24-mar-99

ATA: 32 - 00

Page 2 of 8


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

320000 60000

320000 61000

320000 62000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

PERFORM A DETAILED VISUAL INSPECTION OF THE CONTROL CABLES 115 IN THE NLG WHEEL WELL FOR BROKEN WIRES. CHECK ASSOCIATED 116 PULLEYS AND BRACKETS FOR CONDITION AND SECURITY OF INSTALLATION. THE FOLLOWING CABLES ARE LOCATED IN THE NLG WHEEL WELL: - NLG MANUAL EXTENSION CABLES - NLG STEERING CABLES NOTE( J ) THE CONTROL CABLE SYSTEM MUST BE DISPLACED FULL TRAVEL IN EACH DIRECTION FOR COMPLETE INSPECTION AT SEALS, PULLEYS AND FAIRLEAD AREAS. ACCESS COVERS P/N 273A4520-1 OR -2 NEED TO BE REMOVED TO PERFORM THIS TASK.

emp emp

PERFORM A DETAILED VISUAL INSPECTION OF THE CONTROL CABLES 133 IN THE LEFT AND RIGHT MAIN LANDING GEAR WHEEL WELL FOR BROKEN 134 WIRES. CHECK ASSOCIATED PULLEYS, BRACKETS AND MECHANISMS FOR CONDITION AND SECURITY OF INSTALLATION. THE FOLLOWING CABLES ARE LOCATED IN THE LEFT AND RIGHT MLG WHEEL WELL: - MLG MANUAL EXTENSION CABLES NOTE( J ) THE CONTROL CABLE SYSTEM MUST BE DISPLACED FULL TRAVEL IN EACH DIRECTION FOR COMPLETE INSPECTION AT SEALS, PULLEYS AND FAIRLEAD. MLG MANUAL EXTENSION CABLES DO NOT REQUIRE DISPLACEMENT FOR COMPLETE INSPECTION.

emp emp

PERFORM A DETAILED VISUAL INSPECTION OF THE CONTROL CABLES 210 WITHIN THE CONTROL CABIN FOR BROKEN WIRES. CHECK ASSOCIATED PULLEYS, BRACKETS AND MECHANISMS FOR CONDITION AND SECURITY OF INSTALLATION. THE FOLLOWING CABLES ARE LOCATED IN THE CONTROL CABIN: - LANDING GEAR CONTROL LEVER CABLES - NOSE WHEEL STEERING CABLES NOTE( J ) THE CONTROL CABLES MUST BE DISPLACED FULL TRAVEL IN EACH DIRECTION FOR COMPLETE INSPECTION AT SEALS, PULLEYS AND FAIRLEAD.

S2113

STRUCTURE

REFERENCES MPD MRB MRB

20-20-31-20

MPD MRB

32-440-00 MSI 32-440-00 RTE:6 MSI 32-440-00 RTE:8

AMTOSS

20-20-31-20

MPD MRB

32-460-00 MSI 32-460-00 RTE:6 MSI 32-460-00 RTE:8

MRB AMTOSS

ITEMS

TSK

EFF

R L ITEM BY E E REVISION P V DATE

32-440-00 MSI 32-440-00 RTE:6 MSI 32-440-00 RTE:8

AMTOSS

MRB

THRESHOLD INTERVAL

20-20-31-20

I: 4800 CYC I: 24 MTH

E3 HHI 737-700

3 22-mar-07

I: 4800 CYC I: 24 MTH

E3 HHI 737-700

3 22-mar-07

I: 36000 CYC I: 12 YRS

E3 HHI 737-700

3 18-mar-05

ATA: 32 - 00

Page 3 of 8


HHI

737-6

MAINTENANCE SCHEDULE

R E V

ITEM

R

320000 63000

R

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

PERFORM A DETAILED VISUAL INSPECTION OF THE CONTROL CABLES 137 WITHIN THE OVERWING CENTER SECTION AND WHEEL WELLS FROM BS 138 663 TO BS 727 FOR BROKEN WIRES. CHECK ASSOCIATED PULLEYS, BRACKETS AND MECHANISMS FOR CONDITION AND SECURITY OF INSTALLATION. THE FOLLOWING CABLES ARE LOCATED WITHIN THE AFT PASSENGER CABIN OVERWING CENTER SECTION: - MLG CONTROL CABLES - MLG MANUAL EXTENSION CABLES - MLG BRAKE CONTROL CABLES NOTE( J ) THE CONTROL CABLE SYSTEM MUST BE DISPLACED FULL TRAVEL IN EACH DIRECTION FOR COMPLETE INSPECTION AT SEALS, PULLEYS AND FAIRLEAD. ACCESS PASSENGER CABIN FLOOR PANELS BETWEEN B.S. 663.75 AND B.S. 727 FORWARD CARGO COMPARTMENT AFT BULKHEAD PANELS FORWARD CARGO COMPARTMENT CEILING PANELS OR FLOOR PANELS BETWEEN B.S.396 TO B.S. 540.

STRUCTURE

emp emp

MPD MRB MRB AMTOSS AMTOSS AMTOSS

ITEMS

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

32-450-00 MSI 32-450-00 RTE:6 MSI 32-450-00 RTE:8 20-20-31-200-801 20-20-31-200-802 20-20-31-200-805

I: 21600 CYC I: 6 YRS

ATA: 32 - 00

E3 HHI 737-700

5 23-jul-08

Page 4 of 8


HHI

737-6

MAINTENANCE SCHEDULE

R E V

ITEM

R

320000 64000

R

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

PERFORM A DETAILED VISUAL INSPECTION OF THE CONTROL CABLES 112 WITHIN THE LOWER NOSE COMPARTMENT FOR BROKEN WIRES. CHECK 113 ASSOCIATED PULLEYS, BRACKETS AND MECHANISMS FOR CONDITION 114 AND SECURITY OF INSTALLATION. THE FOLLOWING CABLES ARE LOCATED WITHIN THE LOWER NOSE COMPARTMENT: - MLG CONTROL CABLES - MLG MANUAL EXTENSION CABLES - MLG BRAKE CONTROL CABLES - NLG MANUAL EXTENSION CABLES - NLG STEERING CABLES NOTE( J ) THE CONTROL CABLE SYSTEM MUST BE DISPLACED FULL TRAVEL IN EACH DIRECTION FOR COMPLETE INSPECTION AT SEALS, PULLEYS AND FAIRLEAD. ACCESS PASSENGER CABIN FLOOR PANELS BETWEEN B.S. 663.75 AND B.S. 727 FORWARD CARGO COMPARTMENT AFT BULKHEAD PANELS FORWARD CARGO COMPARTMENT CEILING PANELS OR FLOOR PANELS BETWEEN B.S.396 TO B.S. 540.

STRUCTURE

112A emp emp

MPD MRB MRB AMTOSS AMTOSS AMTOSS

ITEMS

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

32-450-00 MSI 32-450-00 RTE:6 MSI 32-450-00 RTE:8 20-20-31-200-801 20-20-31-200-802 20-20-31-200-805

I: 21600 CYC I: 6 YRS

ATA: 32 - 00

E3 HHI 737-700

5 23-jul-08

Page 5 of 8


HHI R E V

ITEM

R

320000 65000

R

R

737-6

MAINTENANCE SCHEDULE

320000 66000

R

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

PERFORM A DETAILED VISUAL INSPECTION OF THE CONTROL CABLES 117 WITHIN THE ELECTRONICS COMPARTMENT FOR BROKEN WIRES. CHECK 118 ASSOCIATED PULLEYS, BRACKETS AND MECHANISMS FOR CONDITION AND SECURITY OF INSTALLATION. THE FOLLOWING CABLES ARE LOCATED WITHIN THE ELECTRONICS COMPARTMENT: - MLG CONTROL CABLES - MLG MANUAL EXTENSION CABLES - MLG BRAKE CONTROL CABLES NOTE( J ) THE CONTROL CABLE SYSTEM MUST BE DISPLACED FULL TRAVEL IN EACH DIRECTION FOR COMPLETE INSPECTION AT SEALS, PULLEYS AND FAIRLEAD. ACCESS PASSENGER CABIN FLOOR PANELS BETWEEN B.S. 663.75 AND B.S. 727 FORWARD CARGO COMPARTMENT AFT BULKHEAD PANELS FORWARD CARGO COMPARTMENT CEILING PANELS OR FLOOR PANELS BETWEEN B.S.396 TO B.S. 540.

117A emp

PERFORM A DETAILED VISUAL INSPECTION OF THE CONTROL CABLES 125 WITHIN THE AIR CONDITIONING DISTRIBUTION BAY FOR BROKEN WIRES. 126 CHECK ASSOCIATED PULLEYS, BRACKETS AND MECHANISMS FOR CONDITION AND SECURITY OF INSTALLATION. THE FOLLOWING CABLES ARE LOCATED WITHIN THE AIR CONDTIONING DISTRIBUTION BAY: - MLG CONTROL CABLES - MLG MANUAL EXTENSION CABLES - MLG BRAKE CONTROL CABLES NOTE( J ) THE CONTROL CABLE SYSTEM MUST BE DISPLACED FULL TRAVEL IN EACH DIRECTION FOR COMPLETE INSPECTION AT SEALS, PULLEYS AND FAIRLEAD. ACCESS PASSENGER CABIN FLOOR PANELS BETWEEN B.S. 663.75 AND B.S. 727 FORWARD CARGO COMPARTMENT AFT BULKHEAD PANELS FORWARD CARGO COMPARTMENT CEILING PANELS OR FLOOR PANELS BETWEEN B.S.396 TO B.S. 540.

emp 821

STRUCTURE MPD MRB MRB

20-20-31-200-801 20-20-31-200-802 20-20-31-200-805

MPD MRB

32-450-00 MSI 32-450-00 RTE:6 MSI 32-450-00 RTE:8

AMTOSS AMTOSS AMTOSS

TSK

EFF

R L ITEM BY E E REVISION P V DATE

32-450-00 MSI 32-450-00 RTE:6 MSI 32-450-00 RTE:8

AMTOSS AMTOSS AMTOSS

MRB

ITEMS

THRESHOLD INTERVAL

REFERENCES

20-20-31-200-801 20-20-31-200-802 20-20-31-200-805

I: 21600 CYC I: 6 YRS

E3 HHI 737-700

5 23-jul-08

I: 21600 CYC I: 6 YRS

E3 HHI 737-700

5 23-jul-08

ATA: 32 - 00

Page 6 of 8


HHI R E V

ITEM

R

320000 67000

R

R

737-6

MAINTENANCE SCHEDULE

320000 68000

R

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

PERFORM A DETAILED VISUAL INSPECTION OF THE CONTROL CABLES 121 WITHIN THE FORWARD CARGO COMPARTMENT FOR BROKEN WIRES. 122 CHECK ASSOCIATED PULLEYS, BRACKETS AND MECHANISMS FOR CONDITION AND SECURITY OF INSTALLATION. THE FOLLOWING CABLES ARE LOCATED WITHIN THE FORWARD CARGO COMPARTMENT: - MLG CONTROL CABLES - MLG MANUAL EXTENSION CABLES - MLG BRAKE CONTROL CABLES NOTE( J ) THE CONTROL CABLE SYSTEM MUST BE DISPLACED FULL TRAVEL IN EACH DIRECTION FOR COMPLETE INSPECTION AT SEALS, PULLEYS AND FAIRLEAD. ACCESS PASSENGER CABIN FLOOR PANELS BETWEEN B.S. 663.75 AND B.S. 727 FORWARD CARGO COMPARTMENT AFT BULKHEAD PANELS FORWARD CARGO COMPARTMENT CEILING PANELS OR FLOOR PANELS BETWEEN B.S.396 TO B.S. 540.

821 emp

PERFORM A DETAILED VISUAL INSPECTION OF THE CONTROL CABLES 135 WITHIN THE PASSENGER COMPARTMENT OVER THE WING CENTER 136 SECTION FROM BS 540 TO BS 663.75 FOR BROKEN WIRES. CHECK ASSOCIATED PULLEYS, BRACKETS AND MECHANISMS FOR CONDITION AND SECURITY OF INSTALLATION. THE FOLLOWING CABLES ARE LOCATED WITHIN THE PASSENGER COMPARTMENT ABOVE THE WING CENTER SECTION: - MLG CONTROL CABLES - MLG MANUAL EXTENSION CABLES - MLG BRAKE CONTROL CABLES NOTE( J ) THE CONTROL CABLE SYSTEM MUST BE DISPLACED FULL TRAVEL IN EACH DIRECTION FOR COMPLETE INSPECTION AT SEALS, PULLEYS AND FAIRLEAD.

131AB emp

STRUCTURE MPD MRB MRB

20-20-31-200-801 20-20-31-200-802

MPD MRB

32-460-00 MSI 32-460-00 RTE:6 MSI 32-460-00 RTE:8

AMTOSS AMM AMM AMM AMM

TSK

EFF

R L ITEM BY E E REVISION P V DATE

32-450-00 MSI 32-450-00 RTE:6 MSI 32-450-00 RTE:8

AMTOSS AMTOSS

MRB

ITEMS

THRESHOLD INTERVAL

REFERENCES

20-20-31-20 32-31-22-211-801 20-20-31-200-801 20-20-31-200-802 20-20-31-200-805

I: 21600 CYC I: 6 YRS

E3 HHI 737-700

5 23-jul-08

I: 36000 CYC I: 12 YRS

E3 HHI 737-700

4 23-jul-08

ATA: 32 - 00

Page 7 of 8


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

320010 00000

DESCRIPTION CLEAN EXPOSED SURFACE OF THE LEFT AND RIGHT MAIN LANDING GEAR SHOCK STRUT

ZONE ACCESS 734 744

STRUCTURE

emp emp

MPD MPD MRB MRB AMTOSS

Date: 23-jul-08

ITEMS

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

32-010-01 32-010-02 MSI 32-010-01 RTE:9 MSI 32-010-02 RTE:9 32-00-10-100-801

I: 50 CYC

ATA: 32 - 00

S

HHI 737-700

3 03-jun-04

Page 8 of 8


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 32 - 11

321100 01000

321100 40000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

MAIN LANDING GEAR SHOCK STRUT PERFORM A DETAILED VISUAL INSPECTION OF THE LEFT AND RIGHT 734 MAIN LANDING GEAR EXTENSION AND RETRACTION MECHANISM ( 744 INCLUDING RETRACT ACTUATORS, UPLOCK ACTUATORS AND DOWNLOCK ACTUATORS, UPLOCK MECHANISM AND DOWNLOCK MECHANISM).

551DB 651DB

RESTORE THE LEFT AND RIGHT MAIN LANDING GEAR ASSEMBLY. NOTE( J ) FOR COMPLETENESS ONLY COVERED BY CMS.

551BB 551BT 551DB 551DT 551EB 551ET 551FB 651BB 651BT 651DB 651DT 651EB 651ET 651FB

734 emp emp emp emp emp emp 744 emp emp emp emp emp emp

ITEMS

MPD MRB

32-150-00 MSI 32-150-00 RTE:6

AMTOSS

32-11-00-20

MPD MPD MPD MPD MRB

MRB MRB

32-040-01 32-040-02 32-720-01 32-720-02 MSI 32-040-01 RTE:8 MSI 32-040-02 RTE:8 MSI 32-720-01 MSI 32-720-02

AMM AMM AMM AMM AMM AMM AMM AMM AMM AMM AMM AMM AMM AMM AMM AMM MS

32-11-00-000 32-11-00-400 32-11-61-000 32-11-61-400 32-11-71-000 32-11-71-420 32-11-83-000 32-11-83-400 32-11-89-000 32-11-89-420 32-32-11-000 32-32-11-400 32-32-31-000 32-32-31-400 57-16-02-000 57-16-02-400 CM3211 .....

MRB

I: 4000 CYC

E3 HHI 737-700

5 22-mar-07

I: 10 YRS I: 18000 CYC

S

5 22-mar-07

ATA: 32 - 11

HHI 737-700

Page 1 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

321100 50000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

DISCARD THE LEFT AND RIGHT MAIN LANDING GEAR LIFE LIMITED PARTS 734 emp NOTE( J ) emp FOR COMPLETENESS ONLY SEE CMS FOR AFFECTED PARTS. emp emp emp emp 744

STRUCTURE

551BB 551BT 551DB 551DT 551EB 551ET 551FB emp

ITEMS

THRESHOLD INTERVAL

REFERENCES MPD MPD MPD MRB MRB AMTOSS AMTOSS

TSK

EFF

R L ITEM BY E E REVISION P V DATE

32-050-01 32-050-02 CMR PAGE 9.0-50 MSI 32-050-01 RTE:8 MSI 32-050-02 RTE:8 32-11-00-00 32-11-00-40

I: 45000 CYC

ATA: 32 - 11

S

HHI 737-700

6 05-sep-06

Page 2 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 32 - 21

322100 00000

322100 21000

322100 22000

322100 60000

DESCRIPTION

ZONE ACCESS

STRUCTURE

TSK

EFF

R L ITEM BY E E REVISION P V DATE

NOSE LANDING GEAR SHOCK STRUT PERFORM A DETAILED VISUAL INSPECTION OF THE NOSE LANDING GEAR 713 EXTENSION AND RETRACTION MECHANISM (INCLUDING RETRACT ACTUATOR, LOCK ACTUATOR AND LOCK MECHANISM).

PERFORM A DETAILED VISUAL INSPECTION OF THE NOSE WHEEL STEERING MECHANICAL CONTROL PATH.

PERFORM A DETAILED VISUAL INSPECTION OF THE NOSE WHEEL STEERING ACTUATOR ROD ENDS AND ASSOCIATED HARDWARE.

REPLACE NLG AFT LOCK LINK (162A2115-2) NOTE( J ) FOR COMPLETENESS ONLY COVERED BY CMS.

115

713

713

emp

emp

emp

emp

MPD MRB

32-120-00 MSI 32-120-00 RTE:6

AMTOSS

32-11-00-00

MPD MRB

32-390-00 MSI 32-390-00 RTE:6

AMTOSS

32-51-00-200-801

MPD MRB

32-400-00 MSI 32-400-00 RTE:6

AMTOSS

32-21-00-20

MPD MPD

MRB

Date: 23-jul-08

THRESHOLD INTERVAL

REFERENCES

ITEMS

I: 4000 CYC

E3 HHI 737-700

4 22-mar-07

I: 4000 CYC

E3 HHI 737-700

7 22-mar-07

I: 4000 CYC

E3 HHI 737-700

4 22-mar-07

I: 4200 CYC

S

2 03-jun-04

32-100-00 PAGE 9.0-17 STRUCTURAL SAFE LIFE PARTS MSI 32-100-00 RTE:8

ATA: 32 - 21

HHI 737-700

Page 1 of 2


HHI R E V

ITEM 322110 00100

322110 00200

322110 10000

N

737-6

MAINTENANCE SCHEDULE

322171 20000

DESCRIPTION RESTORE THE NOSE LANDING GEAR ASSEMBLY. NOTE( J ) FOR COMPLETENESS ONLY COVERED BY CMS.

DISCARD THE NOSE LANDING GEAR LIFE LIMITED PARTS NOTE( J ) FOR COMPLETENESS ONLY SEE CMS FOR AFFECTED PARTS

ZONE ACCESS emp emp 113AC 113AW 113BW 114AC 114AW 114BW 711AL 712AR

MPD MPD MRB

115 116 713 emp emp emp emp emp emp emp

713

MRB

32-090-00 32-750-00 MSI 32-090-00 RTE:8 MSI 32-750-00

AMM AMM AMM AMM AMM AMM MS

32-21-00-000 32-21-00-400 32-21-21-000 32-21-21-400 32-33-51-000 32-33-51-400 CM3221 000..

emp emp 113AC 113AW 113BW 114AC 114AW 114BW 711AL 712AR

MPD MRB

32-100-00 MSI 32-100-00 RTE:8

AMTOSS AMTOSS

32-21-00-40 32-21-00-00

emp

MPD MRB

32-060-00 MSI 32-060-00 RTE:9

AMTOSS

32-00-10-10

MPD MRB

32-085-00 MSI 32-085-00 FEC:8

AMM TC

32-21-71-200-803 32-085-00-01

emp

N

Date: 23-jul-08

THRESHOLD INTERVAL

REFERENCES

115 116 713 emp emp emp emp emp emp emp

CLEAN EXPOSED SURFACE OF THE NOSE LANDING GEAR SHOCK STRUT. 713

INSPECT (DETAILED) NOSE LANDING GEAR AXLE.

STRUCTURE

ITEMS

TSK

EFF

R L ITEM BY E E REVISION P V DATE

I: 18000 CYC I: 10 YRS

S

HHI 737-700

5 22-mar-07

I: 75000 CYC

S

HHI 737-700

4 05-sep-06

I: 50 CYC

S

HHI 737-700

1 03-jun-04

T: 30 MTH I: 30 MTH

E3 HHI 737-700

0 23-jul-08

ATA: 32 - 21

Page 2 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 32 - 31

323100 00000

323151 20000

323171 40000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

LANDING GEAR CONTROL SYSTEM FUNCTIONAL CHECK / ADJUSTMENT OF CONTROL CABLE TENSION

PERFORM A DETAILED VISUAL INSPECTION OF THE LANDING GEAR SELECTOR VALVE.

OPERATIONALLY CHECK THE LANDING GEAR TRANSFER VALVE

112

133

133 134 211 212

112A

emp

112A emp emp emp

ITEMS

empty

AMM

32-31-00-820-801

MPD MRB

32-110-00 MSI 32-110-00 RTE:8

AMTOSS

32-31-51-20

MPD MRB

32-240-00 MSI 32-240-00 RTE:8

AMTOSS

32-31-71-40

I: 18000 CYC I: 5 YRS

F2 HHI 737-700

2 25-apr-06

I: 4000 CYC

E3 HHI 737-700

4 22-mar-07

I: 8000 FLH

F1 HHI 737-700

1 03-jun-04

ATA: 32 - 31

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 32 - 32

323221 00000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

MAIN LANDING GEAR EXTENSION AND RETRACTION REMOVE THE MAIN LANDING GEAR WHEEL WELL PROTECTION RETRACT 133 PRESSURE FUSE FOR FUNCTIONAL TEST 134 NOTE( J ) FOR COMPLETENESS ONLY, COVERED BY COSL.

emp emp

ITEMS

MPD MRB

32-230-00 MSI 32-230-00 RTE:6

AMM AMM AMTOSS

32-32-21-400 32-32-21-000 32-32-21-00

I: 25000 FLH

ATA: 32 - 32

S

HHI 737-700

4 05-sep-06

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 32 - 34

323400 70000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

NOSE LANDING GEAR EXTENSION AND RETRACTION PERFORM A FUNCTIONAL CHECK OF THE LEFT AND RIGHT MAIN LANDING 212 GEAR MANUAL EXTENSION SYSTEM AND ALTERNATE EXTENSION BYPASS 734 VALVE. 744

S2122 emp emp

ITEMS

MPD MRB

32-220-00 MSI 32-220-00 RTE:8

AMTOSS

32-34-00-730-801

I: 30 MTH

ATA: 32 - 34

F1 HHI F2 737-700

4 25-apr-06

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 32 - 35

323500 73000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

LANDING GEAR ALTERNATE EXTENSION SYSTEM PERFORM A FUNCTIONAL CHECK OF THE NOSE LANDING GEAR MANUAL 211 EXTENSION SYSTEM. 212 713

emp S2122 emp

ITEMS

MPD MRB

32-200-00 MSI 32-200-00 RTE:8

AMTOSS

32-35-00-730-801

I: 30 MTH

ATA: 32 - 35

F2 HHI 737-700

4 25-apr-06

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 32 - 41

324100 71000

324100 72000

324131 00000

324141 70000

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

Date: 23-jul-08

TSK

EFF

R L ITEM BY E E REVISION P V DATE

BRAKE CONTROL SYSTEM PERFORM AN OPERATIONAL CHECK OF THE ALTERNATE BRAKE SYSTEM 133 AND ALTERNATE BRAKE SELECTOR VALVE. 134 211 212

emp emp emp emp

MPD MRB

32-290-00 MSI 32-290-00 RTE:8

AMTOSS

32-41-00-71

OPERATIONALLY CHECK THE BRAKE ACCUMULATOR ISOLATION VALVE 133 134 211 212

emp emp emp emp

MPD MRB

32-310-00 MSI 32-310-00 RTE:9

AMTOSS

32-41-00-72

PERFORM A DETAILED VISUAL INSPECTION OF THE BRAKE METERING 133 VALVES.

emp

MPD MRB

32-260-00 MSI 32-260-00 RTE:6

AMTOSS

32-41-31-00

MPD MPD MRB

32-270-01 32-270-02 MSI 32-270-01 RTE:6 MSI 32-270-02 RTE:6

VISUALLY CHECK THE LEFT AND RIGHT BRAKE WEAR PINS FOR MINIMUM 211 EXTENSION. 734 (PARKING BRAKE SET) 744

emp emp emp

MRB

324181 00000

THRESHOLD INTERVAL

PERFORM A DETAILED VISUAL INSPECTION OF THE FORWARD AND AFT 133 BRAKE CONTROL LINKAGES AND CABLES QUADRANTS. 134 210

112A emp emp

ITEMS

AMTOSS AMM

32-41-41-70 32-41-41

MPD MRB

32-250-00 MSI 32-250-00 RTE:6

AMTOSS

32-41-81-00

I: 15000 CYC

F1 HHI 737-700

2 18-mar-05

I: 12500 CYC

F1 HHI 737-700

1 03-jun-04

I: 4000 CYC

E3 HHI 737-700

4 22-mar-07

I: 50 CYC

E2 HHI 737-700

1 03-jun-04

I: 4000 CYC

E3 HHI 737-700

5 22-mar-07

ATA: 32 - 41

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 32 - 44

324400 79000

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

Date: 23-jul-08

TSK

EFF

R L ITEM BY E E REVISION P V DATE

PARKING BRAKE SYSTEM PERFORM A FUNCTIONAL BLEED DOWN CHECK OF THE PARKING BRAKE 134 SYSTEM AND BRAKE ACCUMULATOR PRECHARGE PRESSURE. 211 212

emp emp emp

MPD MRB MRB

324411 00000

THRESHOLD INTERVAL

PERFORM A DETAILED VISUAL INSPECTION OF THE PARKING BRAKE MECHANICAL CONTROL PATH.

112 emp 211 212

112A 2111S emp emp

ITEMS

32-340-00 MSI 32-340-00 RTE:6 MSI 32-340-00 RTE:9

AMTOSS

32-44-00-79

MPD MRB

32-330-00 MSI 32-330-00 RTE:6

AMTOSS

32-44-11-00

I: 4000 CYC

F2 HHI 737-700

3 22-mar-07

I: 4000 CYC

E3 HHI 737-700

4 22-mar-07

ATA: 32 - 44

Page 1 of 1


HHI R E V

ITEM 32 - 45

R

737-6

MAINTENANCE SCHEDULE

324500 70000

R 324511 40000

324521 00000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

WHEELS, BRAKES, AND TIRES VISUALLY CHECK NOSE AND MAIN LANDING GEAR TIRES AND WHEELS 713 FOR CONDITION AND WEAR. 734 744 NOTE( I ) 48 ELAPSED CLOCK HOURS

emp emp emp

MPD MRB

32-360-00 MSI 32-360 RTE:9

AMTOSS

32-45-00-70

RESTORE THE LEFT AND RIGHT MAIN LANDING GEAR WHEEL ASSEMBLY 734 (IES) 744 NOTE( I, J ) NOTE (I): TIRE CHANGE NOTE (J): FOR COMPLETENESS ONLY COVERED BY CMS.

emp emp

MPD MPD MRB

32-380-01 32-380-02 MSI 32-380-01 RTE:9 MSI 32-380-02 RTE:9

RESTORE THE NOSE LANDING GEAR WHEEL ASSEMBLY (IES). NOTE( I, J ) NOTE (I): TIRE CHANGE NOTE (J): FOR COMPLETENESS ONLY COVERED BY CMS.

emp

713

MRB

ITEMS

AMTOSS AMTOSS

32-45-11-40 32-45-11-00

MPD MRB

32-380-00 MSI 32-380-00 RTE:9

AMTOSS AMTOSS

32-45-21-40 32-45-21-00

I: 48 HRS

VC HHI E1 737-700

5 23-jul-08

I: 1 s.N

S

HHI 737-700

2 03-jun-04

I: 1 s.N

S

HHI 737-700

2 03-jun-04

ATA: 32 - 45

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 32 - 51

325121 00000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

NOSE GEAR STEERING SYSTEM PERFORM A DETAILED VISUAL INSPECTION OF THE RUDDER PEDAL STEERING INTERCONNECT MECHANICAL CONTROL PATH.

112 113 emp emp emp

emp 113AC 113AW 113BW 114AC

ITEMS

MPD MRB

32-410-00 MSI 32-410-00 RTE:6

AMTOSS

32-51-21-00

I: 4000 CYC

ATA: 32 - 51

E3 HHI 737-700

3 22-mar-07

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 32 - 61

326100 71000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

LANDING GEAR POSITION INDICATING AND WARNING PERFORM AN OPERATIONAL CHECK ( BITE CHECK ) THE PROXIMITY SWITCH ELECTRONICS UNIT

112

emp

ITEMS

MPD MRB

32-420-00 MSI 32-420-00 RTE:8

AMM

32-09-10-710-801

I: 25000 FLH

ATA: 32 - 61

F1 HHI 737-700

2 30-nov-05

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 33 33 - 51

335100 72000

335103 96000

335105 96000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

LIGHTS EMERGENCY LIGHTS FUNCTIONAL CHECK OF THE FLIGHT DECK EMERGENCY LIGHTING SWITCH "ON" AND "ARMED" POSITION AND THE ATTENDANT PANEL EMERGENCY LIGHTING SWITCH "ON" POSITION.

OPERATIONAL CHECK OF THE EMERGENCY LIGHTS.

210 220 230 240

emp emp emp emp

MPD MRB

33-020-00 MSI 33-020-00 RTE:8

AMTOSS

33-51-00-720-801

200

emp

MPD MRB

33-010-00 MSI 33-010-00 RTE:8

AMTOSS

33-51-00-710-801

MPD MRB

33-055-00 MSI 33-055-00 RTE:8

AMTOSS

33-51-06-200-801

FUNCTIONAL CHECK OF THE EMERGENCY LIGHTS BATTERY PACKS FOR 220 CAPACITY (15MIN. MINIMUM) AND ONE COMPLETE DEEP CYCLE. 230 240 NOTE( J ) PERFORM THIS TEST NOT LESS THAN 120MIN. BEFORE DEPARTURE.

emp emp emp

ITEMS

I: 2 YRS

F2 HHI 737-700

6 03-jun-04

I: 300 FLH

F1 HHI 737-700

3 03-jun-04

I: 1 YRS

F2 HHI 737-700

5 03-jun-04

ATA: 33 - 51

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 34 34 - 11

341100 17000

341100 79000

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

NAVIGATION STATIC AND TOTAL AIR PRESSURE SYSTEM DETAILED INSPECTION FOR MOISTURE IN THE PITOT SYSTEMS

PERFORM A FUNCTIONAL PITOT STATIC SYSTEM LEAK CHECK

112

113 114 121 122 211 212 221 222

112A

emp emp emp emp emp emp emp emp

MPD MRB

34-090-00 MSI 34-090-00 RTE:6

AMTOSS

34-11-00-21

MPD MPD MPD MPD MPD MPD MRB

34-010-00 34-020-00 34-030-00 34-040-00 34-050-00 34-060-00 MSI 34-010-00 RTE:6 MSI 34-020-00 RTE:6 MSI 34-030-00 RTE:6 MSI 34-040-00 RTE:6 MSI 34-050-00 RTE:6 MSI 34-060-00 RTE:6

MRB MRB MRB MRB MRB AAR AAR AMTOSS AMTOSS AMTOSS AMTOSS AMTOSS AMTOSS

Date: 23-jul-08

THRESHOLD INTERVAL

ITEMS

I: 6000 FLH

NFL II - 2/00, PAGE I: 24 MTH 82 NFL II - 23/03 34-11-00-790-815 34-11-00-790-814 34-11-00-790-813 34-11-00-790-812 34-11-00-790-811 34-11-00-790-810

ATA: 34 - 11

E3 HHI 737-700

3 18-mar-05

F2 HHI 737-700

4 03-jun-04

Page 1 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

341101 17000

341101 20000

341102 20000

Date: 23-jul-08

DESCRIPTION DETAILED INSPECTION FOR MOISTURE IN THE STATIC SYSTEMS

DETAILED VISUAL INSPECTION OF THE PITOT PROBES

DETAILED VISUAL INSPECTION OF THE STATIC PROBES

ZONE ACCESS 112 118 122

113 114

113 114

STRUCTURE

112A 117A 821

emp emp

emp emp

ITEMS

THRESHOLD INTERVAL

REFERENCES MPD MRB

34-100-00 MSI 34-100-00 RTE:6

AMTOSS

34-11-00-210-802

MPD MRB

34-070-00 MSI 34-070-00 RTE:6

AMTOSS

34-11-01-200-803

MPD MRB

34-080-00 MSI 34-080-00 RTE:6

AMTOSS

34-11-02-200-801

TSK

EFF

R L ITEM BY E E REVISION P V DATE

I: 12000 FLH

E3 HHI 737-700

3 22-mar-07

I: 6000 FLH

E3 HHI 737-700

3 18-mar-05

I: 6000 FLH

E3 HHI 737-700

3 18-mar-05

ATA: 34 - 11

Page 2 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 34 - 24

342400 02000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

STANDBY MAGNETIC COMPASS STANDBY MAGNETIC COMPASS SWING.

200

emp

ITEMS

AAR

NFL II 56/01

AMM

34-23-00-820-802

I: 12 MTH

ATA: 34 - 24

F2 HHI 737-700

2 29-apr-03

Page 1 of 1


HHI R E V

ITEM 34 - 53

R

737-6

MAINTENANCE SCHEDULE

345300 73000

DESCRIPTION

ZONE ACCESS

STRUCTURE

TSK

EFF

R L ITEM BY E E REVISION P V DATE

AIR TRAFFIC CONTROL SYSTEM PERFORM A FUNCTIONAL CHECK OF THE AIRCRAFT´S ATC SYSTEM

210

emp

R

Date: 23-jul-08

THRESHOLD INTERVAL

REFERENCES

MPD MRB AAR

34-110-00 MSI 34-110-00 RTE:7

AAR FAR 91.413 PART 43 APPENDIX F AMTOSS 34-53-00-73 AMM 34-53-00-730-803

ITEMS

I: 24 MTH

ATA: 34 - 53

F2 HHI 737-700

3 23-jul-08

Page 1 of 1


HHI R E V

ITEM 34 - 60

R

737-6

MAINTENANCE SCHEDULE

346002 00001

DESCRIPTION

ZONE ACCESS

STRUCTURE

TSK

EFF

R L ITEM BY E E REVISION P V DATE

FLIGHT MANAGEMENT COMPUTING FMS NAVIGATION DATA BASE (NDB) REVISE NDB

205

emp

R

Date: 23-jul-08

THRESHOLD INTERVAL

REFERENCES

empty

AMM AMM

ITEMS

34-61-00-470-803 34-61-00-470-805

I: 28 DAY

ATA: 34 - 60

S

HHI 737-700

1 23-jul-08

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

35

OXYGEN

35 - 00

GENERAL

350000 01000

350000 02000

350000 04000

350000 05000

350000 06000

350000 09000

Date: 23-jul-08

CREW OXYGEN SYSTEM FOR MINIMUM DISPATCH PRESSURE

MASK ASSY, OPERATIONAL CHECK IN "SITU"

DISCHARGE DISC FOR DAMAGE

ZONE ACCESS

210

210

122

CHECK FOR PRESENCE AND PROPER STORAGE OF SMOKE GOGGLES 212

PORTABLE OXYGEN UNITS FOR MINIMUM DISPATCH PRESSURE

212

PROTECTIVE BREATHING EQUIPMENT, VENDOR SCOTT: IF INSTALLED 212 CHECK FOR HUMIDITY INDICATOR COLOR: IF COLOR HAS CHANGED FROM BLUE TO PINK, DISCARD UNIT

STRUCTURE

emp

emp

emp

emp

emp

emp

ITEMS

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

empty

SERVICE EXPERIENCE

I: 1 Z

M1 HHI 737-700

FC

1 11-dec-01

SERVICE EXPERIENCE

I: 1 Z

M1 HHI 737-700

FC

1 11-dec-01

SERVICE EXPERIENCE

I: 1 Z

E1 HHI 737-700

SM

3 03-jun-04

SERVICE EXPERIENCE

I: 1 Z

E1 HHI 737-700

FC

1 11-dec-01

SERVICE EXPERIENCE

I: 1 Z

M1 HHI 737-700

1 11-dec-01

SERVICE EXPERIENCE

I: 1 Z

E1 HHI 737-700

3 18-dec-02

empty

empty

empty

empty

empty

ATA: 35 - 00

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 35 - 12

351200 70000

351200 70001

351200 71000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

FLIGHT CREW OXYGEN SYSTEM OPERATIONALLY CHECK EACH FLIGHT CREW OXYGEN MASK/MICROPHONE.

210

OPERATIONALLY CHECK EACH FLIGHT CREW OXYGEN MASK/REGULATOR 122 (OUT OF THE BOX ASSEMBLY). 210

VISUALLY (CROSS) CHECK THE FLIGHT CREW OXYGEN CYLINDER 122 PRESSURE INDICATOR AND THE CONTROL COMPARTMENT FLIGHT CREW 210 OXYGEN INDICATOR.

821

821 emp

117A emp

ITEMS

MPD MRB

23-080-00 MSI 23-080-00 RTE:9

AMTOSS

35-12-00-70

MPD MRB

35-010-00 MSI 35-010-00 RTE:8

MPD MRB

35-050-00 MSI 35-050-00 RTE:8

AMTOSS

35-12-00-71

I: 4000 FLH

F1 HHI 737-700

3 05-sep-06

I: 4000 FLH

F1 HHI 737-700

0 03-jun-04

I: 2400 FLH

E2 HHI 737-700

3 25-apr-06

ATA: 35 - 12

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 35 - 21

352101 00000

352101 01000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

PASSENGER / LLAR OXYGEN SYSTEM-CHEMICAL CHEMICAL OXYGEN GENERATOR CHECK EXPIRATION DATE, IF AGE LIMIT 220 WILL BE REACHED DURING NEXT 15 MTH, CHANGE GENERATOR. 230 240

VISUALLY CHECK THE TEMPERATURE SENSITIVE TAPE AND POSITION 220 OF FIRING PINS ON EACH PASSENGER CABIN CHEMICAL OXYGEN 230 GENERATOR (INCLUDING EACH LAVATORY AND CABIN ATTENDANT'S 240 SERVICE UNIT).

emp emp emp

emp emp emp

ITEMS

MPD MRB

35-070-00 MSI 35-070-00 RTE:9

AMTOSS AMTOSS

35-22-11-40 35-22-11-00

MPD MRB

35-060-00 MSI 35-060-00 RTE:9

AMTOSS

35-22-00-21

I: 15 MTH

E2 HHI 737-700

1 03-jun-04

I: 4 YRS

E2 HHI 737-700

3 03-jun-04

ATA: 35 - 21

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 35 - 22

352200 70000

352231 21000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

PASSENGER OXYGEN SYSTEM-GASEOUS OPERATIONALLY CHECK THE PASSENGER OXYGEN SYSTEM AUTOMATIC 220 AND MANUAL MODES, ( THIS CHECK INCLUDES THE DOOR LATCH 230 ACTUATORS / SOLENOIDS ) 240

VISUALLY CHECK 10% ( ROTATIONAL INSPECTION ) OF THE PASSENGER, 220 LAVATORY, AND ATTENDANT OXYGEN MASKS FOR CONDITION AND 230 SECURITY. 240

emp emp emp

emp emp emp

ITEMS

MPD MRB

35-080-00 MSI 35-080-00 RTE: 9

AMTOSS

35-22-00-70

MPD MRB

35-090-00 MSI 35-090-00 RTE:9

AMTOSS

35-22-31-21

I: 8000 FLH

F1 HHI 737-700

1 03-jun-04

I: 8000 FLH

E2 HHI 737-700

1 03-jun-04

ATA: 35 - 22

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 35 - 31

353100 71000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

PORTABLE OXYGEN EQUIPMENT VISUALLY CHECK ALL THE PORTABLE OXYGEN CYLINDERS FOR PRESENCE, CONDITION AND SECURITY

221 241

emp emp

ITEMS

MPD MRB

35-100-00 MSI 35-100-00 RTE:9

AMTOSS

35-31-00-71

I: 8000 FLH

ATA: 35 - 31

E2 HHI 737-700

1 03-jun-04

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 36 36 - 14

361400 00000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

PNEUMATIC APU BLEED SYSTEM DISCARD APU BLEED AIR DUCT FLEXIBLE PRESSURE SEAL.

133 emp 141 143 145

193D 311BL emp emp emp

ITEMS

MPD MRB

21-190-00 MSI 21-190-00 RTE:6

AMM AMM

36-13-01-020 36-13-01-420

I: 6 YRS

ATA: 36 - 14

S

HHI 737-700

0 22-mar-07

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 38 38 - 11

381106 00000

381106 10000

381106 20000

DESCRIPTION

ZONE ACCESS

STRUCTURE

TSK

EFF

R L ITEM BY E E REVISION P V DATE

WATER & WASTE STORAGE AND DISTRIBUTION OPERATIONALLY CHECK THE FORWARD LAVATORY POTABLE WATER DRAIN VALVE FOR EVIDENCE OF LEAKAGE.

221

emp

ANNUAL INSPECTION AND CERTIFICATION OF POTABLE WATER SYSTEM. 146 IN CASE OF FINDINGS PERFORM CLEANING WITH HERISIL. NOTE( R ) TRINKWASSERVERORDNUNG § 18 UND 19 VOM 21.05.2001

146AR

PERFORM CLEANING OF POTABLE WATER SYSTEM.

146AR

146

MPD MRB

38-010-00 MSI 38-010-00 RTE:9

AMTOSS

38-11-06-00

AAR

SEE NOTE

ITEMS

I: 6500 FLH

F1 HHI 737-700

1 03-jun-04

I: 12 MTH

S

HHI 737-700

0 18-mar-05

I: 4 MTH

S

HHI 737-700

1 22-mar-07

empty

AMTOSS

Date: 23-jul-08

THRESHOLD INTERVAL

REFERENCES

38-10-00-600-801

ATA: 38 - 11

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 38 - 32

383200 10000

383202 00100

383203 00000

383205 96000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

VACUUM WASTE SYSTEM SERVICE THE TOILET WASTE LINES.

REPLACE THE WASTE TANK WATER SEPARATOR. NOTE( E ) APPLICABLE FOR L/N 138 AND ON, OR WITH SUPPLIER (EDO FIBER SCIENCE) S/B 01930-38-1 INSTALLED.

117 221 241

141 145 emp

RESTORE THE WASTE DRAIN BALL-VALVE BY REPLACING THE SEALS (2) 141 (OFF AIRCRAFT).

RESTORE (CLEAN) OR REPLACE THE VACUUM BLOWER FILTER.

141 145 emp

117A emp emp

emp 1401S 822

822

emp 1401S 822

ITEMS

MPD MRB

38-020-00 MSI 38-020-00 RTE:7

AMTOSS AMTOSS

38-32-00-100-802 38-32-00-100-801

MPD MRB

38-100-00 MSI 38-100-00 RTE:9

AMTOSS AMTOSS

38-32-02-40 38-32-02-00

MPD MRB

38-040-00 MSI 38-040-00 RTE:9

AMTOSS AMTOSS

38-32-03-40 38-32-03-00

MPD MRB

38-030-00 MSI 38-030-00 RTE:7

AMTOSS

38-32-05-96

I: 2400 FLH

S

HHI 737-700

6 05-sep-06

I: 6000 FLH

S

HHI 737-700

5 18-mar-05

I: 60 MTH

S

HHI 737-700

4 22-mar-07

I: 2500 FLH

S

HHI 737-700

2 03-jun-04

ATA: 38 - 32

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 38 - 33

383300 74000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

WASTE TANK QUANTITY INDICATION OPERATIONALLY ( BITE ) CHECK THE WASTE TANK QUANTITY INDICATION 241 SYSTEM FROM THE FLIGHT ATTENDANT´S PANEL.

emp

ITEMS

MPD MRB

38-050-00 MSI 38-050-00 RTE:9

AMTOSS

38-33-00-74

I: 6500 FLH

ATA: 38 - 33

F1 HHI 737-700

1 03-jun-04

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 38 - 42

384210 96000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

WATER TANK PRESSURIZATION SYSTEM DISCARD AND REPLACE THE BLEED AIR IN-LINE FILTER.

146 emp

1401S 822

ITEMS

MPD MRB

38-060-00 MSI 38-060-00 RTE:9

AMTOSS

38-42-10-96

I: 6500 FLH

ATA: 38 - 42

S

HHI 737-700

2 03-jun-04

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 49 49 - 00

490011 10000

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

AIRBORNE AUXILIARY POWER AUXILIARY POWER UNIT (APU) - GENERAL CHECK THE OIL LEVEL AND SERVICE THE APU WITH OIL AS REQUIRED 316

315A

empty

SERVICE EXPERIENCE

Date: 23-jul-08

THRESHOLD INTERVAL

ITEMS

I: 7 DAY

ATA: 49 - 00

S

HHI 737-700

3 23-jul-08

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 49 - 11

491111 40000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

APU - SYSTEM PERFORM A DETAILED VISUAL INSPECTION OF THE APU MOUNTS, STRUTS AND BRACKETS FOR CRACKS, FATIGUE OR CORROSION.

315 316

315A emp

ITEMS

MPD MRB

49-020-00 MSI 49-020-00 RTE:8

AMTOSS

49-13-11-20

I: 8 YRS I: 1 AC

ATA: 49 - 11

E3 HHI 737-700

5 03-jun-04

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 49 - 13

491311 20000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

APU MOUNTS PERFORM A GENERAL VISUAL INSPECTION OF THE APU MOUNTS FOR 315 GENERAL CONDITION AND SECURITY OF INSTALLATION 316

315A emp

ITEMS

MPD MRB

49-010-00 MSI 49-010-00 RTE:8

AMTOSS

49-13-11-20

I: 2 YRS

ATA: 49 - 13

E1 HHI 737-700

1 03-jun-04

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 49 - 15

491511 20000

491522 00000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

APU AIR INTAKE SYSTEM PERFORM A DETAILED INSPECTION OF THE SIGMA SEAL. (AFTER APU REMOVAL). NOTE( I ) APU CHANGE

316

LUBRICATE THE VORTEX GENERATOR HINGE PIN

312

315A

emp

ITEMS

MPD MRB

49-030-00 MSI 49-030-00 RTE:8

AMTOSS

49-15-11-20

MPD MRB

49-240-00 MSI 49-240-00 RTE:9

AMTOSS

49-15-22-60

I: 1 s.N

E3 HHI 737-700

3 03-jun-04

I: 16000 FLH

S

2 03-jun-04

ATA: 49 - 15

HHI 737-700

Page 1 of 1


HHI R E V

ITEM 49 - 16

R

491611 10000

R

R

737-6

MAINTENANCE SCHEDULE

491611 11000

R

491611 19900

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

APU DRAINS CLEAN THE COMBUSTOR DRAIN AND EXAMINE THE THREAD FOR CRACKS. PERFORM AN OPERATIONAL CHECK. NOTE( I ) INTERVAL 4000 APU HRS

315 316

315A emp

CLEAN AND EXAMINE THE DRAIN FITTING ON EXHAUST DUCT MUFFLER 315 EDUCTOR HOUSING. 316 NOTE( I ) INTERVAL 5000 APU-HRS

315A emp

PERFORM A GENERAL VISUAL INSPECTION OF THE APU DRAIN MAST FOR FLUID LEAKAGE. NOTE( I ) INTERVAL 1600 APU HRS

315A emp

315 316

ITEMS

MPD MRB

49-120-00 MSI 49-120-00 RTE:8

AMM AMM AMTOSS AMM AMM

49-16-12 49-16-11 49-16-11-10 49-16-11-100-801 49-16-12-100-801

MPD MRB

49-180-00 MSI 49-180-00 RTE:9

AMTOSS AMTOSS AMM

49-81-12-10 49-81-12-801 49-81-12-100-801

MPD MRB

49-090-00 MSI 49-090-00 RTE:8

AMTOSS

49-16-11-20

I: 1 s.N

S HHI F1 737-700 E3

5 23-jul-08

I: 1 s.N

E3 HHI S 737-700

8 23-jul-08

I: 1 s.N

E1 HHI 737-700

2 18-mar-05

ATA: 49 - 16

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 49 - 17

491711 20000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

APU INSULATION PANELS PERFORM A DETAILED INSPECTION OF THE APU INSULATION PANELS. 315 (AFTER APU REMOVAL). 316 NOTE( I ) APU CHANGE

315A emp

ITEMS

MPD MRB

49-040-00 MSI 49-040-00 RTE:8

AMTOSS

49-17-11-20

I: 1 s.N

ATA: 49 - 17

E3 HHI 737-700

2 03-jun-04

Page 1 of 1


HHI R E V

ITEM 49 - 30

R

737-6

MAINTENANCE SCHEDULE

493011 40000

R 493021 00000

DESCRIPTION

ZONE ACCESS

STRUCTURE

TSK

EFF

R L ITEM BY E E REVISION P V DATE

APU FUEL SYSTEM PERFORM A GENERAL VISUAL INSPECTION OF THE FCU, SEALS, FUEL 315 LINES, AND INTERFACING CONNECTIONS FOR LEAKAGE, GENERAL 316 CONDITION, AND SECURITY OF INSTALLATION NOTE( I ) INTERVAL 1600 APU HRS

315A emp

DISCARD THE FUEL INLET FILTER ELEMENT ON THE FUEL CONTROL UNIT 315 (FCU). 316 NOTE( I ) INTERVAL 4000 APU HRS

315A emp

MPD MRB

49-110-00 MSI 49-110-00 RTE:9

AMTOSS

49-31-11-200-801

MPD MRB

49-102-00 MSI 49-102-00 RTE:7 MSI 49-102-00 RTE:9

MRB AMTOSS AMTOSS

Date: 23-jul-08

THRESHOLD INTERVAL

REFERENCES

ITEMS

49-31-21-40 49-31-21-00

I: 1 s.N

E1 HHI 737-700

4 23-jul-08

I: 1 s.N

S

2 03-jun-04

ATA: 49 - 30

HHI 737-700

Page 1 of 1


HHI R E V

ITEM 49 - 41

R

737-6

MAINTENANCE SCHEDULE

494151 20000

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

IGNITION / STARTING PERFORM A DETAILED INSPECTION OF THE IGNITOR PLUG NOTE( I ) INTERVAL 2000 APU HRS

315 316

315A emp

R

Date: 23-jul-08

REFERENCES

ITEMS

MPD MRB

49-132-00 MSI 49-132-00 RTE:7

AMTOSS

49-41-51-20

I: 1 s.N

ATA: 49 - 41

E3 HHI 737-700

2 23-jul-08

Page 1 of 1


HHI R E V

ITEM 49 - 61 496100 70000

R

737-6

MAINTENANCE SCHEDULE

496100 90000

R

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

APU CONTROLS PERFORM AN OPERATIONAL CHECK OF THE FOLLOWING BY INTERROGATING THE CDU´S APU MAINTENANCE PAGES. -APU DATA MEMORY MODULE ( DMM ) - ELECTRONICS CONTROL UNIT ( ECU ) - SPEED SENSOR - EGT RAKE NOTE( I ) INTERVAL 1600 APU HRS

211

RECORD APU HOURS AND CYCLES VIA THE CDU NOTE( M ) RECORDING IS ALSO REQUIRED AT ECU OR APU CHANGE

210

emp

emp

MPD MRB

49-140-00 MSI 49-140-00 RTE:9

AMTOSS

49-61-00-710-801

I: 1 s.N

F1 HHI 737-700

4 30-nov-05

49-70-00 SERVICE EXPERIENCE

I: 500 FLH

M2 HHI 737-700

2 23-jul-08

empty

AMM

ITEMS

ATA: 49 - 61

Page 1 of 1


HHI R E V

ITEM 49 - 81 498111 20000

R

737-6

MAINTENANCE SCHEDULE

498111 20100

DESCRIPTION

ZONE ACCESS

STRUCTURE

Date: 23-jul-08

TSK

EFF

R L ITEM BY E E REVISION P V DATE

EXHAUST PERFORM A GENERAL VISUAL INSPECTION INSIDE THE EXHAUST DUCT 315 MUFFLER ( GAS FLOW PATH ) FOR OBVIOUS DAMAGE AND OBSTRUCTION. 316 NOTE( I ) APU CHANGE

315A emp

PERFORM A GENERAL VISUAL INSPECTION OF THE INSULATION BLANKET 317 ON THE EXHAUST DUCT MUFFLER FOR GENERAL CONDITION AND 318 SECURITY OF INSTALLATION

315A 318BR

R 498111 20200

THRESHOLD INTERVAL

REFERENCES

PERFORM A DETAILED INSPECTION OF THE EXHAUST DUCT MUFFLER 317 318 NOTE( I ) INTERVAL 10000 APU HRS

315A 318BR

ITEMS

MPD MRB

49-152-00 MSI 49-152-00 RTE:7

AMTOSS

49-81-11-20

MPD MRB

49-162-00 MSI 49-162-00 RTE:7

AMTOSS AMM

49-81-11-20 49-81-13-200-801

MPD MRB

49-172-00 MSI 49-172-00 RTE:7

AMTOSS

49-81-11-20

I: 1 s.N

E1 HHI 737-700

1 03-jun-04

I: 10000 FLH

E1 HHI 737-700

3 23-jul-08

I: 1 s.N

E3 HHI 737-700

2 03-jun-04

ATA: 49 - 81

Page 1 of 1


HHI R E V

ITEM 49 - 91

R

737-6

MAINTENANCE SCHEDULE

499111 00000

R

499113 20000

499141 20000

499171 20000

499171 21000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

APU EDUCTOR SYSTEM PERFORM A GENERAL VISUAL INSPECTION OF THE LUBE MODULE AND 315 LINES FOR LEAKAGE, GENERAL CONDITION, AND SECURITY OF 316 INSTALLATION. NOTE( I ) INTERVAL 1000 APU HRS

315A emp

PERFORM A DETAILED INSPECTION OF THE OIL FILTER DELTA-P INDICATOR. NOTE( I ) INTERVAL 1000 APU HRS

emp 315A

315 316

PERFORM A GENERAL VISUAL INSPECTION OF THE EDUCTOR ( ON THE 315 APU ) FOR GENERAL CONDITION 316 NOTE( I ) INTERVAL 5000 APU HRS

PERFORM A GENERAL VISUAL INSPECTION OF THE EDUCTOR INLET DUCT (AIR FLOW PATH) FOR OBVIOUS DAMAGE AND OBSTRUCTION (AFTER APU REMOVAL) NOTE( I ) APU CHANGE

315 emp

PERFORM A GENERAL VISUAL INSPECTION OF THE EDUCTOR INLET 317 DUCT (INSIDE THE AIRPLANE TAIL CONE COMPARTMENT) FOR FLUID 318 ACCUMULATION, GENERAL CONDITION, AND SECURITY OF INSTALLATION

315A emp

MPD MRB

49-190-00 MSI 49-190-00 RTE: 9

AMTOSS AMTOSS AMM

49-91-11-40 49-91-11-00 49-91-11-200-801

MPD MRB

49-200-00 MSI 49-200-00 RTE:9

AMTOSS

49-91-13-20

MPD MRB

49-212-00 MSI 49-212-00 RTE:7 MSI 49-212-00 RTE:8

MRB

315A 318BR

315A 318BR

ITEMS

AMTOSS

49-81-41-20

MPD MRB

49-230-00 MSI 49-230-00 RTE:8

AMTOSS

49-91-71-20

MPD MRB

49-220-00 MSI 49-220-00 RTE:8

AMTOSS

49-91-71-20

I: 1 s.N

E1 HHI 737-700

3 23-jul-08

I: 1 s.N

E3 HHI 737-700

2 03-jun-04

I: 1 s.N

E1 HHI 737-700

1 03-jun-04

I: 1 s.N

E1 HHI 737-700

3 03-jun-04

I: 12000 FLH

E1 HHI 737-700

4 22-mar-07

ATA: 49 - 91

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 52 52 - 11

521100 00000

521100 01000

521100 02000

521100 03000

521100 04000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

DOORS PASSENGER ENTRY DOOR GENERAL VISUAL INSPECTION OF THE FORWARD ENTRY DOOR PRESSURE SEAL AND FLAPPER SEALS FOR DEGRADATION.

831

831

MPD MRB

52-050-00 MSI 52-050-00 RTE:6

AMTOSS

52-11-00-20

MPD MRB

52-020-00 MSI 52-020-00 RTE: 9

AMTOSS

12-25-11-64

MPD MRB

52-030-00 MSI 52-030-00 RTE: 9

AMTOSS

52-11-00-20

831 831AW 831AZ 831BZ 831CZ 831DZ 831EZ

MPD MRB

52-010-00 MSI 52-010-00 RTE:9

AMTOSS

12-25-11-64

831

MPD MRB

52-610-00 MSI 52-610-00

LUBRICATE THE FORWARD ENTRY DOOR GUIDE PLATE TRACKS AND 831 ARM ASSEMBLIES (ROD END BEARINGS AND THREADS), THE UPPER AND LOWER HINGE ARM BUSHINGS, GATE HINGES AND THE FUSELAGE HINGE TORQUE TUBE BEARING.

831

DETAILED VISUAL INSPECTION OF THE FORWARD ENTRY DOOR CENTERING GUIDE STUD AND NYLON TRACK PADS CONDITION

831

LUBRICATE THE FORWARD ENTRY DOOR HANDLE, LATCH MECHANISMS, (LATCH TORQUE TUBE BEARINGS AND LATCH CONTROL RODS), THE BEARINGS ON THE DOOR HINGE TORQUE TUBE AND THE FWD ENTRY DOOR CONTROL RODS AND STOP RODS.

831

831 emp emp emp emp emp emp

DETAILED VISUAL INSPECTION OF THE FORWARD ENTRY DOOR STOP 831 FITTING AND PINS. E X T E R N A L ACCESS INSPECT WITH DOORS OPENED AND LINING NOT REMOVED.

ITEMS

I: 4000 FLH

E2 HHI 737-700

3 03-jun-04

I: 1 YRS

S

HHI 737-700

3 30-nov-05

I: 1 YRS

E3 HHI 737-700

3 03-jun-04

I: 2 YRS

S

HHI 737-700

2 03-jun-04

I: 24 MTH I: 4000 CYC

E3 HHI 737-700

1 03-jun-04

ATA: 52 - 11

Page 1 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

521100 05000

521100 06000

521100 09000

521100 09100

521100 09200

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

DETAILED VISUAL INPECTION OF THE FORWARD ENTRY DOOR STOP FITTING AND PINS. I N T E R N A L ACCESS REMOVE INSULATION, INTERIOR LINERS AND ACCESS PANELS AS REQUIRED.

831 emp

GENERAL VISUAL INSPECTION OF THE FORWARD ENTRY DOOR SKIN AND STRUCTURE. I N T E R N A L ACCESS REMOVE INSULATION, INTERIOR LINERS AND ACCESS PANELS AS REQUIRED.

831 emp emp emp emp emp emp

831 8311S 831AZ 831BZ 831CZ 831DZ 831EZ

MPD MRB

DETAILED VISUAL INSPECTION OF THE FORWARD AIRSTAIRS DOOR STOP 117 FITTINGS AND PINS. emp E X T E R N A L ACCESS INSPECT WITH DOOR OPENED

1172S 117BL

MPD MRB

GENERAL VISUAL INSPECTION OF THE FORWARD AIRSTAIRS ACCESS DOOR SKIN AND STRUCTURE. E X T E R N A L ACCESS INSPECT WITH DOOR BOTH OPENED AND CLOSED.

117BL

117

GENERAL VISUAL INSPECTION OF THE FORWARD AIRSTAIRS DOOR SKIN 117 AND STRUCTURE. emp I N T E R N A L ACCESS REMOVE INSULATION BLANKET

831 831AW

REFERENCES

1172S 117BL

ITEMS

MPD MRB

MPD MRB

MPD MRB

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

52-620-00 MSI 52-620-00 I: 8 YRS I: 18000 CYC

E3 HHI 737-700

1 03-jun-04

I: 8 YRS I: 18000 CYC

E2 HHI 737-700

2 03-jun-04

I: 24 MTH I: 4000 CYC

E3 HHI 737-700

2 03-jun-04

I: 4000 CYC I: 24 MTH

E2 HHI 737-700

1 03-jun-04

I: 18000 CYC I: 8 YRS

E2 HHI 737-700

2 03-jun-04

52-650-00 MSI 52-650-00

52-580-00 MSI 52-580-00

52-590-00 MSI 52-590-00

52-600-00 MSI 52-600-00

ATA: 52 - 11

Page 2 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 52 - 12

521200 00000

521200 00500

521200 01000

521200 01500

521200 02000

521200 02500

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

FORWARD AND AFT SERVICE DOORS GENERAL VISUAL INSPECTION OF THE FORWARD SERVICE DOOR PRESSURE SEAL FOR DEGRADATION.

841

GENERAL VISUAL INSPECTION OF THE AFT SERVICE DOOR PRESSURE 844 SEAL FOR DEGRADATION.

841

844

LUBRICATE THE FORWARD SERVICE DOOR GUIDE PLATE TRACKS AND 841 ARM ASSEMBLIES (ROD END BEARINGS AND THREADS), TORQUE TUBE BUSHINGS, THE UPPER AND LOWER HINGE ARM BUSHINGS AND GATE HINGES

841

LUBRICATE THE AFT SERVICE DOOR GUIDE PLATE AND ARM ASSEMBLIES 844 (ROD END BEARINGS AND THREADS), TORQUE TUBE BUSHINGS, THE UPPER AND LOWER HINGE ARM BUSHINGS AND GATE HINGES

844

DETAILED VISUAL INSPECTION OF THE FORWARD SERVICE DOOR CENTERING GUIDE BEARINGS FOR CONDITION

841

DETAILED VISUAL INSPECTION AFT SERVICE DOOR CENTERING GUIDE 844 BEARINGS FOR CONDITION

841

844

ITEMS

MPD MRB

52-050-00 MSI 52-050-00 RTE:6

AMTOSS

52-41-00-20

MPD MRB

52-050-00 MSI 52-050-00 RTE:6

AMTOSS

52-41-00-20

MPD MRB

52-020-00 MSI 52-020-00 RTE: 9

AMTOSS

12-25-13-64

MPD MRB

52-020-00 MSI 52-020-00 RTE: 9

AMTOSS

12-25-13-64

MPD MRB

52-040-00 MSI 52-040-00 RTE: 9

AMTOSS

52-41-00-20

MPD MRB

52-040-00 MSI 52-040-00 RTE: 9

AMTOSS

52-41-00-20

I: 4000 FLH

E2 HHI 737-700

3 03-jun-04

I: 4000 FLH

E2 HHI 737-700

3 03-jun-04

I: 1 YRS

S

HHI 737-700

3 30-nov-05

I: 1 YRS

S

HHI 737-700

3 30-nov-05

I: 1 YRS

E3 HHI 737-700

3 03-jun-04

I: 1 YRS

E3 HHI 737-700

3 03-jun-04

ATA: 52 - 12

Page 1 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

521200 03000

521200 03500

521200 04000

521200 05000

521200 06000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

LUBRICATE THE FORWARD SERVICE DOOR HANDLE, LATCH MECHANISMS 841 (LATCH TORQUE TUBE BEARINGS AND LATCH CONTROL RODS) AND THE emp BEARINGS ON THE DOOR HINGE TORQUE TUBE. emp emp emp

841 841AW 841AZ 841BZ 841CZ

MPD MRB

52-010-00 MSI 52-010-00 RTE:9

AMTOSS

12-25-13-64

LUBRICATE THE AFT SERVICE DOOR HANDLE, LATCH MECHANISMS 844 (LATCH TORQUE TUBE BEARINGS AND LATCH CONTROL RODS) AND THE emp BEARINGS ON THE DOOR HINGE TORQUE TUBE. emp emp emp

844 844AW 844AZ 844BZ 844CZ

MPD MRB

52-010-00 MSI 52-010-00 RTE:9

AMTOSS

12-25-13-64

DETAILED VISUAL INSPECTIONN OF THE FORWARD AND AFT SERVICE 841 DOOR STOP FITTING AND PINS. 844 E X T E R N A L ACCESS INSPECT WITH DOORS OPENED AND LINING NOT REMOVED.

841 844

MPD MRB

52-610-00 MSI 52-610-00

DETAILED VISUAL INSPECTION OF THE AFT AND FORWARD SERVICE DOORS STOP FITTING AND PINS. I N T E R N A L ACCESS REMOVE INSULATION, INTERIOR LINES AND ACCESS PANELS, AS REQUIRED.

841 emp 844 emp

841 841AW 844 844AW

MPD MRB

GENERAL VISUAL INSPECTION OF THE SERVICE DOORSSKIN AND STRUCTURE. I N T E R N A L ACCESS REMOVE INSULATION, INTERIOR LINERS AND ACCESS PANELS, AS REQUIRED.

841 emp emp emp emp emp emp 844 emp emp emp emp emp

841 8411S 841AZ 841BZ 841CZ 841DZ 841EZ 8441S 844AZ 844BZ 844CZ 844DZ 844EZ

MPD MRB

ITEMS

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

I: 2 YRS

S

HHI 737-700

2 03-jun-04

I: 2 YRS

S

HHI 737-700

0 03-jun-04

I: 24 MTH I: 4000 CYC

E3 HHI 737-700

1 03-jun-04

I: 8 YRS I: 18000 CYC

E3 HHI 737-700

1 03-jun-04

I: 18000 CYC I: 8 YRS

E2 HHI 737-700

1 03-jun-04

52-620-00 MSI 52-620-00

52-650-00 MSI 52-650-00

ATA: 52 - 12

Page 2 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 52 - 13

521300 00000

521300 01000

521300 02000

521300 03000

521300 04000

521300 05000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

AFT ENTRY DOOR GENERAL VISUAL INSPECTION OF THE AFT ENTRY DOOR PRESSURE SEAL FOR DEGRADATION.

834

834

LUBRICATE THE AFT ENTRY DOOR GUIDE PLATE TRACKS AND ARM 834 ASSEMBLIES (ROD END BEARINGS AND THREADS), THE UPPER AND LOWER HINGE ARM BUSHINGS, GATE HINGES AND THE FUSELAGE HINGE TORQUE TUBE BEARING.

834

DETAILED VISUAL INSPECTION OF THE AFT ENTRY DOOR CENTERING GUIDE BEARINGS FOR CONDITION

834

834

MPD MRB

52-050-00 MSI 52-050-00 RTE:6

AMTOSS

52-13-00-20

MPD MRB

52-020-00 MSI 52-020-00 RTE: 9

AMTOSS

12-25-12-64

MPD MRB

52-040-00 MSI 52-040-00 RTE: 9

AMTOSS

52-13-00-20

LUBRICATE THE AFT ENTRY DOOR HANDLE, LATCH MECHANISMS (LATCH 834 TORQUE TUBE BEARINGS AND LATCH CONTROL RODS) AND THE emp BEARINGS ON THE DOOR HINGE TORQUE TUBE.. emp emp emp

834 834AW 834AZ 834BZ 834CZ

MPD MRB

52-010-00 MSI 52-010-00 RTE:9

AMTOSS

12-25-12-64

DETAILED VISUAL INSPECTION OF THE AFT ENTRY DOOR STOP FITTING 834 AND PINS. E X T E R N A L ACCESS INSPECT WITH DOORS OPENED AND LINING NOT REMOVED.

834

MPD MRB

52-610-00 MSI 52-610-00

DETAILED VISUAL INSPECTION OF THE AFT ENTRY DOOR STOP FITTING 834 AND PINS. emp I N T E R N A L ACCESS REMOVE INSULATION, INTERIOR LINERS AND ACCESS PANELS AS REQUIRED.

834 834AW

ITEMS

MPD MRB

I: 4000 FLH

E2 HHI 737-700

3 03-jun-04

I: 1 YRS

S

HHI 737-700

3 30-nov-05

I: 1 YRS

E3 HHI 737-700

3 03-jun-04

I: 2 YRS

S

HHI 737-700

3 03-jun-04

I: 24 MTH I: 4000 CYC

E3 HHI 737-700

1 03-jun-04

I: 18000 CYC I: 8 YRS

E3 HHI 737-700

1 03-jun-04

52-620-00 MSI 52-620-00

ATA: 52 - 13

Page 1 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

521300 06000

Date: 23-jul-08

DESCRIPTION GENERAL VISUAL INSPECTION OF THE AFT ENTRY DOOR SKIN AND STRUCTURES. I N T E R N A L ACCESS REMOVE INSULATION, INTERIOR LINERS AND ACCESS PANELS, AS REQUIRED.

ZONE ACCESS 834 emp emp emp emp emp emp

STRUCTURE

834 8341S 834AZ 834BZ 834CZ 834DZ 834EZ

ITEMS

REFERENCES MPD MRB

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

52-650-00 MSI 52-650-00 I: 8 YRS I: 18000 CYC

ATA: 52 - 13

E2 HHI 737-700

1 03-jun-04

Page 2 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 52 - 22

522200 00000

522200 01000

522200 02000

522200 03000

522200 04000

522200 05000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

EMERGENCY EXIT DOOR OPERATIONALLY CHECK THE FLIGHT LOCK MECHANICAL SWITCHES FOR 833 THE AUTOMATIC OVERWING EXIT DOORS 843

OPERATIONALLY CHECK THE AUTOMATIC OVERWING EXIT DOORS.

DETAILED VISUAL INSPECTION OF THE AUTOMATIC OVERWING EXIT DOOR LATCH ROLLERS, LINKS AND PIVOT FITTINGS/JOINTS.

833 843

833 843

833 843

MPD MRB

52-210-00 MSI 52-210-00 RTE:7

AMTOSS

52-22-00-71

MPD MRB

52-220-00 MSI 52-220-00 RTE:8

AMTOSS

52-22-00-71

833 emp 843 emp

833 833AZ 843 843AZ

MPD MRB

52-230-00 MSI 52-230-00 RTE:8

AMTOSS

52-22-00-21

DETAILED VISUAL INSPECTION OF THE AUTOMATIC OVERWING EXIT DOOR STOP FITTINGS AND PINS. E X T E R N A L ACCESS INSPECT WITH DOORS OPENED AND LINING NOT REMOVED.

833 843

833 843

MPD MRB

52-730-00 MSI 52-730-00

OPERATIONALLY CHECK THE FLIGHT LOCK ENGAGEMENT AND DISENGAGEMENT.

833 843

DETAILED VISUAL INSPECTION OF THE AUTOMATIC EMERGENCY DOOR 833 FLIGHT LOCKS FOR CORROSION AND CONDITION. emp 843 emp

833 843

833 833AZ 843 843AZ

ITEMS

MPD MRB

52-240-00 MSI 52-240-00 RTE:8

AMTOSS

52-22-00-71

MPD MRB

52-250-00 MSI 52-250-00 RTE:8

AMTOSS

52-22-00-21

I: 4000 FLH

F1 HHI 737-700

3 03-jun-04

I: 2 YRS

F1 HHI 737-700

2 03-jun-04

I: 2 YRS

E3 HHI 737-700

2 03-jun-04

I: 24 MTH I: 4000 CYC

E3 HHI 737-700

3 18-mar-05

I: 2 YRS

F1 HHI 737-700

2 03-jun-04

I: 2 YRS

E3 HHI 737-700

2 03-jun-04

ATA: 52 - 22

Page 1 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

522200 06000

GENERAL VISUAL INSPECTION OF THE AUTOMATIC EMERGENCY EXIT DOOR PRESSURE SEALS FOR DEGRADATION.

522200 07000

522200 07500

Date: 23-jul-08

ZONE ACCESS 833 843

STRUCTURE

833 843

REFERENCES MPD MRB

52-260-00 MSI 52-260-00 RTE:6

AMTOSS

52-22-00-20 52-740-00 MSI 52-740-00

DETAILED VISUAL INSPECTION OF THE AUTOMATIC OVERWING EXIT DOOR STOP FITTINGS AND PINS. I N T E R N A L ACCESS INSPECT WITH HATCHES REMOVED, THE DOOR OPENED OR REMOVED. REMOVE LININGS AND INSULATIONS.

833 emp 843 emp

833 8331S 843 8431S

MPD MRB

GENERAL VISUAL INSPECTION OF THE AUTOMATIC OVERWING EXIT DOOR SKIN AND STRUCTURE. I N T E R N A L ACCESS INSPECT WITH HATCHES REMOVED, THE DOOR REMOVED OR OPENED. REMOVE LININGS AND INSULATIONS.

833 emp 843 emp

833 8331S 843 8431S

MPD MRB

ITEMS

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

I: 2 YRS

E2 HHI 737-700

2 03-jun-04

I: 8 YRS I: 18000 CYC

E3 HHI 737-700

2 18-mar-05

I: 8 YRS I: 18000 CYC

E2 HHI 737-700

3 18-mar-05

52-760-00 MSI 52-760-00

ATA: 52 - 22

Page 2 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 52 - 31

523100 00000

523100 00500

523100 01000

523100 01500

523100 02000

523100 03000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

CARGO DOOR GENERAL VISUAL INSPECTION OF THE FORWARD CARGO COMPARTMENT 821 DOOR PRESSURE SEAL FOR DEGRADATION.

GENERAL VISUAL INSPECTION OF THE AFT CARGO COMPARTMENT DOOR 822 PRESSURE SEAL FOR DEGRADATION.

LUBRICATE THE FORWARD CARGO COMPARTMENT DOOR LATCH 821 TORQUE TUBE BEARINGS AND THE COUNTER BALANCE IDLER CRANK.

LUBRICATE THE AFT CARGO COMPARTMENT DOOR LATCH TORQUE TUBE BEARINGS AND THE COUNTER BALANCE IDLER CRANK.

822

821

822

821

822

DETAILED VISUAL INSPECTION OF THE FORWARD AND AFT CARGO DOOR 821 STOP FITTINGS AND PINS. 822 E X T E R N A L ACCESS INSPECT WITH DOORS OPENED. LINING NOT REMOVED.

821 822

OPERATIONALLY CHECK THE FORWARD AND AFT CARGO COMPARTMENT 821 DOOR SNUBBER. 822

821 822

ITEMS

MPD MRB

52-100-00 MSI 52-100-00 RTE:6

AMTOSS

52-31-00-20

MPD MRB

52-100-00 MSI 52-100-00 RTE:6

AMTOSS

52-31-00-20

MPD MRB

52-090-00 MSI 52-090-00 RTE: 9

AMTOSS

12-25-31-64

MPD MRB

52-090-00 MSI 52-090-00 RTE: 9

AMTOSS

12-25-31-64

MPD MRB

52-670-00 MSI 52-670-00

MPD MRB

52-110-00 MSI 52-110-00 RTE:9

AMTOSS

52-31-13-710-802

I: 4000 FLH

E2 HHI 737-700

3 03-jun-04

I: 4000 FLH

E2 HHI 737-700

3 03-jun-04

I: 1 YRS

S

HHI 737-700

2 03-jun-04

I: 1 YRS

S

HHI 737-700

2 03-jun-04

I: 4000 CYC I: 24 MTH

E3 HHI 737-700

2 03-jun-04

I: 8000 FLH

F1 HHI 737-700

4 03-jun-04

ATA: 52 - 31

Page 1 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

523100 05000

DETAILED VISUAL INSPECTION OF THE FORWARD AND AFT CARGO DOOR STOP FITTINGS AND PINS. I N T E R N A L ACCESS REMOVE INSULATION BLANKET

821 emp 822 emp

821 8211S 822 8221S

MPD MRB

DETAILED VISUAL INSPECTION OF THE FORWARD AND AFT CARGO DOOR SKIN AND STRUCTURE. I N T E R N A L ACCESS REMOVE INSULATION BLANKET

821 emp 822 emp

821 8211S 822 8221S

MPD MRB

523100 06000

Date: 23-jul-08

ZONE ACCESS

STRUCTURE

ITEMS

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

52-680-00 MSI 52-680-00 I: 8 YRS I: 18000 CYC

E3 HHI 737-700

1 03-jun-04

I: 18000 CYC I: 8 YRS

E3 HHI 737-700

1 03-jun-04

52-710-00 MSI 52-710-00

ATA: 52 - 31

Page 2 of 2


HHI R E V

ITEM 52 - 48 524800 00000

R

737-6

MAINTENANCE SCHEDULE

524800 02000

R

524800 03000

524800 04000

524800 07000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

EQUIPMENT COMPARTMENT EXTERIOR DOORS GENERAL VISUAL INSPECTION OF THE E / E ACCESS DOOR PRESSURE 117 SEAL FOR DEGRADATION. 118

117A emp

DETAILED VISUAL INSPECTION OF THE E/E EQUIPMENT COMPARTMENT 117 ACCESS DOOR STOP FITTINGS AND PINS. emp E X T E R N A L ACCESS INSPECT WITH DOOR REMOVED

117 117A

DETAILED VISUAL INSPECTION OF THE E/E EQUIPMENT COMPARTMENT 117 ACCESS DOOR STOP FITTINGS AND PINS. I N T E R N A L ACCESS INSPECT WITH DOOR AND ACCESS PANEL REMOVED. REMOVE DAGGER PINS AS REQUIRED.

117A

GENERAL VISUAL INSPECTION OF THE E/E EQUIPMENT COMPARTMENT 117 DOOR SKIN AND STRUCTURE. I N T E R N A L ACCESS INSPECT WITH DOOR AND ACCESS PANEL REMOVED. REMOVE DAGGER PINS AS REQUIRED.

117A

LUBRICATE THE E/E ACCESS DOOR HANDLE LATCHING MECHANISM (RACK AND PINION GEAR AND THE LOCK PINS).

117A emp

117 118

ITEMS

MPD MRB

52-130-00 MSI 52-130-00 RTE:6

AMTOSS

52-48-41-20

MPD MRB

52-540-00 MSI 52-540-00

MPD MRB

MPD MRB

I: 4000 FLH

E2 HHI 737-700

2 03-jun-04

I: 24 MTH I: 4000 CYC

E3 HHI 737-700

3 23-jul-08

I: 8 YRS I: 18000 CYC

E3 HHI 737-700

2 05-sep-06

I: 8 YRS I: 18000 CYC

E2 HHI 737-700

2 05-sep-06

I: 2 YRS

S

2 03-jun-04

52-550-00 MSI 52-550-00

52-570-00 MSI 52-570-00

MPD MRB

52-120-00 MSI 52-120-00 RTE:9

AMTOSS

12-25-41-64

ATA: 52 - 48

HHI 737-700

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 52 - 49

524900 00000

524900 01000

524900 02000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

ACCESS AND BLOWOUT DOOR DETAILED VISUAL INSPECTION OF THE FORWARD ACCESS DOOR STOP 112 FITTINGS AND PINS. emp E X T E R N A L ACCESS INSPECT WITH DOOR OPENED. LINING NOT REMOVED.

1121S 112A

GENERAL VISUAL INSPECTION OF THE FORWARD ACCESS DOOR PRESSURE SEAL FOR DEGRADATION.

112A

112

GENERAL VISUAL INSPECTION OF THE FORWARD ACCESS DOOR SKIN 112 AND STRUCTURE. emp I N T E R N A L ACCESS INSPECT WITH DOOR REMOVED.

1121S 112A

ITEMS

MPD MRB

52-510-00 MSI 52-510-00

MPD MRB

52-140-00 MSI 52-140-00 RTE:6

AMTOSS

52-48-31-20

MPD MRB

52-530-00 MSI 52-530-00

I: 24 MTH I: 4000 CYC

E3 HHI 737-700

2 03-jun-04

I: 8000 FLH

E2 HHI 737-700

1 03-jun-04

I: 18000 CYC I: 8 YRS

E2 HHI 737-700

1 03-jun-04

ATA: 52 - 49

Page 1 of 1


HHI R E V

ITEM 52 52 - 60

N

526000 00000

N

N

526000 01000

N

N

737-6

MAINTENANCE SCHEDULE

526050 21000

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

DOORS AIR STAIRS LUBRICATE THE AIRSTAIR DOOR SYSTEM, (INCLUDES TWO ROLLERS, 117 THE CARRIAGE DRIVE BALL BEARING, DRIVE NUT IN JACKSCREW, LOCK emp PIN GREASE FITTING AND FOUR BEARINGS IN THE CARRIAGE ROLLERS). (APPLICABLE IF AIRSTAIR SYSTEM OR PARTIAL AIRSTAIR SYSTEM WITH ROLLER AND CARRIAGE DRIVE IS INSTALLED.)

117A 117BL

LUBRICATE THE AIRSTAIR SYSTEM PER THE MANUFACTURER'S 117 RECOMMENDATIONS (IF INSTALLED). NOTE( I ) STANDARD MAINTENANCE IS TO APPLY LUBRICANT PER MIL-G-23827 EVERY 300 COMPLETE CYCLES OR 1000 FLIGHT HOURS OR 6 MONTHS TIME, WHICHEVER OCCURS FIRST, AT ALL LUBRICATION POINTS (REF: MONOGRAM SYSTEMS (FORMERLY WEBER AIRCRAFT)-COMPONENT MAINTENANCE MANUAL 52-60-10; AIRSTAIR LUBRICATION DIAGRAM-FIGURE701).

117BL

INSPECT (GENERAL VISUAL) THE AIRSTAIR DOOR PRESSURE SEAL FOR 117 DEGRADATION (IF INSTALLED). emp

117A 117BL

N

Date: 30-jul-08

REFERENCES

ITEMS

MPD MRB

52-150-00 MSI 52-150-00 RTE:7

AMM

12-25-14-600

MPD MRB

52-160-00 MSI 52-160-00 RTE:7

AMM

12-25-71-600

MPD MRB

52-180-00 MSI 52-180-00 RTE:6

AMM

52-61-50-210

I: 1 YRS

LU HHI 737-700 only: D-AHIB

0 23-jul-08

I: 1 s.N

LU HHI 737-700 only: D-AHIB

0 23-jul-08

I: 4000 FLH

GV HHI 737-700 only: D-AHIB

0 23-jul-08

ATA: 52 - 60

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 52 - 70

527000 00000

527000 01000

527000 02000

527000 03000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

COCKPIT DOOR PERFORM A FUNCTIONAL CHECK OF THE LOCKING AND UNLOCKING 221 LATCH BOLT MECHANISM ON THE FLIGHT DECK DOOR DECOMPRESSION 222 PANEL. NOTE( E, I ) NOTE (E): APPLICABLE TO AIRPLANE L/N 1221 AND ON AND TO THOSE AIRPLANES WITH THE NEW FLIGHT DECK SECURITY DOOR INSTALLED BY THE CUSTOMER SPECIFIC BOEING SERVICE BULLETINS. NOTE (I): THE EQUIVALENT CMR TASK (52-CMR-01) IS PERFORMED AT 3000 HOURS, WHICH HAS PRECEDENCE OVER THE MRB INTERVAL OF 30000 HOURS. REFER TO MS 527000 07000.

emp emp

OPERATIONALLY CHECK THE FLIGHT DECK DOOR DECOMPRESSION 221 PANEL HINGES. 222 NOTE( E ) APPLICABLE TO AIRPLANE L/N 1221 AND ON AND TO THOSE AIRPLANES WITH THE NEW FLIGHT DECK SECURITY DOOR INSTALLED BY THE CUSTOMER SPECIFIC BOEING SERVICE BULLETINS.

emp emp

GENERAL VISUAL INSPECTION OF THE FLIGHT DECK DOOR 221 DECOMPRESSION PANEL HINGES FOR CONDITION AND SECURITY. 222 NOTE( E ) APPLICABLE TO AIRPLANE L/N 1221 AND ON AND TO THOSE AIRPLANES WITH THE NEW FLIGHT DECK SECURITY DOOR INSTALLED BY THE CUSTOMER SPECIFIC BOEING SERVICE BULLETINS.

emp emp

GENERAL VISUAL INSPECTION OF THE FLIGHT DECK DOOR SEALS FOR 221 CONDITION AND SECURITY. 222 NOTE( E ) APPLICABLE TO AIRPLANE L/N 1221 AND ON AND TO THOSE AIRPLANES WITH THE NEW FLIGHT DECK SECURITY DOOR INSTALLED BY THE CUSTOMER SPECIFIC BOEING SERVICE BULLETINS.

emp emp

ITEMS

MPD MRB

52-360-00 MSI 52-360-00 RTE:8

SB AMTOSS

CDRB 22-1-18 52-51-00-71

MPD MRB

52-370-00 MSI 52-370-00 RTE:8

SB AMTOSS

CDRB 22-1-18 52-51-00-71

MPD MRB

52-380-00 MSI 52-380-00 RTE:8

SB AMTOSS

CDRB 22-1-18 52-51-00-71

MPD MRB

52-390-00 MSI 52-390-00 RTE:8

SB AMTOSS

CDRB 22-1-18 52-51-00-71

I: 30000 FLH

F2 HHI 737-700

4 30-nov-05

I: 30000 FLH

F1 HHI 737-700

2 03-jun-04

I: 30000 FLH

E2 HHI 737-700

2 03-jun-04

I: 6000 FLH

E2 HHI 737-700

2 03-jun-04

ATA: 52 - 70

Page 1 of 4


HHI R E V

ITEM 527000 04000

R

527000 05000

R

R

737-6

MAINTENANCE SCHEDULE

527000 07000

R

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

GENERAL VISUAL INSPECTION OF THE FLIGHT DECK DOOR 221 DECOMPRESSION PANEL SEALS FOR CONDITION AND SECURITY. 222 NOTE( E ) APPLICABLE TO AIRPLANE L/N 1221 AND ON AND TO THOSE AIRPLANES WITH THE NEW FLIGHT DECK SECURITY DOOR INSTALLED BY THE CUSTOMER SPECIFIC BOEING SERVICE BULLETINS.

emp emp

FUNCTIONALLY CHECK THE DENY TIME DELAY FUNCTION OF THE FLIGHT 221 DECK SECURITY DOOR ACCESS SYSTEM TO VERIFY OPERATION OF THE 222 THREE POSITION ROTARY SWITCH IN THE P8 PANEL, THE DENY FUNCTION, AND REVERSION TO THE DEFAULT MODE. NOTE( E ) APPLICABLE TO AIRPLANE L/N 1221 AND ON AND TO THOSE AIRPLANES WITH THE NEW FLIGHT DECK SECURITY DOOR INSTALLED BY THE CUSTOMER SPECIFIC BOEING SERVICE BULLETINS.

emp emp

PERFORM A FUNCTIONAL CHECK OF THE LOCKING AND UNLOCKING 221 LATCH BOLT MECHANISM ON THE FLIGHT DECK DOOR DECOMPRESSION 222 PANEL. NOTE( E, R ) NOTE (E): APPLICABLE TO AIRPLANES L/N 1221 AND ON, AND L/N 1-1220 THAT HAVE INCORPORATED ENHANCED FLIGHT DECK SECURITY PHASE II COCKPIT DOOR NOTE (R): CMR B22-69-1 IS INCLUDED IN C&D AEROSPACE REPORT CDRB 22-69 REV. E, DATED NOVEMBER 8, 2002.

emp emp

STRUCTURE

REFERENCES MPD MRB

52-400-00 MSI 52-400-00 RTE:8

SB AMTOSS

CDRB 22-1-18 52-51-00-71

MPD MRB

52-410-00 MSI 52-410-00 RTE:6

SB AMTOSS

CDRB 22-1-18 52-51-00-70

AAR AAR SB AMM

ITEMS

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

I: 30000 FLH

E2 HHI 737-700

2 03-jun-04

I: 6000 FLH

F2 HHI 737-700

4 23-jul-08

I: 3000 FLH

F2 HHI 737-700

3 23-jul-08

52-CMR-01 ONE STAR CMR B22-69-1 ONE STAR CDRB 22-1-18 52-51-08

ATA: 52 - 70

Page 2 of 4


HHI

737-6

MAINTENANCE SCHEDULE

R E V

ITEM

R

527001 00000

R

527001 01000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

INTERNAL - DETAILED: FLIGHT DECK SECURITY DOOR PANEL ASSEMBLY. 221 INSPECT FLIGHT DECK SECURITY DOOR ASSEMBLY, INCLUDING MAIN 222 DOOR PANEL ASSY., MAIN DOOR PANEL BOND ASSY., AND ARMOR LAMINATE ASSY. I N T E R N A L NOTE( E ) APPLICABLE TO AIRPLANE L/N 1221 AND ON AND TO THOSE AIRPLANES WITH THE NEW FLIGHT DECK SECURITY DOOR INSTALLED BY THE CUSTOMER SPECIFIC BOEING SERVICE BULLETINS. ACCESS DISASSEMBLE DOOR ONLY IF EVIDENCE OF DAMAGE, FATIGUE, DELAMINATION, AND OR BULGING IS FOUND

emp emp

EXTERNAL - GENERAL VISUAL: FLIGHT DECK SECURITY DOOR SURROUND 221 ASSEMBLY. 222 INSPECT FLIGHT DECK SECURITY DOOR SURROUND ASSEMBLY, INCLUDING HEADER ASSEMBLY, POST ASSEMBLY (RIGHT HAND POST), LATCH AND DEADBOLT RECEIVER ASSEMBLY, SUPPORT STRUCTURE, POST COVER ARMOR ASSEMBLY AND HINGE ASSEMBLY. E X T E R N A L NOTE( E ) APPLICABLE TO AIRPLANE L/N 1221 AND ON AND TO THOSE AIRPLANES WITH THE NEW FLIGHT DECK SECURITY DOOR INSTALLED BY THE CUSTOMER SPECIFIC BOEING SERVICE BULLETINS. ACCESS AS VISIBLE WITH CARPET, TAPESTRIES (IF EQUIPPED) AND KICK STRIPS DISPLACED.

emp emp

STRUCTURE

ITEMS

REFERENCES MPD MRB

52-450-00 MSI 52-450-00

SB

CDRB 22-1-18

MPD MRB

52-460-00 MSI 52-460-00

SB

CDRB 22-1-18

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

I: 16000 CYC I: 3000 DAY

E3 HHI 737-700

4 23-jul-08

I: 8000 CYC I: 1500 DAY

E2 HHI 737-700

2 03-jun-04

ATA: 52 - 70

Page 3 of 4


HHI R E V

ITEM

R

527001 02000

R

R

737-6

MAINTENANCE SCHEDULE

527001 04000

R

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

INTERNAL - DETAILED: FLIGHT DECK SECURITY DOOR SURROUND 221 ASSEMBLY. 222 INSPECT FLIGHT DECK SECURITY DOOR SURROUND ASSEMBLY, INCLUDING HEADER ASSEMBLY, POST ASSEMBLY (RIGHT HAND POST), LATCH AND DEADBOLT RECEIVER ASSEMBLY, SUPPORT STRUCTURE, POST COVER ARMOR ASSEMBLY AND HINGE ASSEMBLY. I N T E R N A L NOTE( E ) APPLICABLE TO AIRPLANE L/N 1221 AND ON AND TO THOSE AIRPLANES WITH THE NEW FLIGHT DECK SECURITY DOOR INSTALLED BY THE CUSTOMER SPECIFIC BOEING SERVICE BULLETINS. ACCESS DISPLACE INTERIOR FURNISHINGS INCLUDING CLOSETS, LAVS, GALLEYS (IF EQUIPPED) ADJACENT TO DOOR FRAME, AND CEILING PANELS ABOVE DOOR. REMOVE ARMOR FROM DOOR FRAME.

emp emp

INTERNAL - DETAILED: FLIGHT DECK DOOR LATCH AND HINGE SUPPORT 221 ASSEMBLIES. 222 I N T E R N A L NOTE( E ) APPLICABLE TO AIRPLANE L/N 1221 AND ON AND TO THOSE AIRPLANES WITH THE NEW FLIGHT DECK SECURITY DOOR INSTALLED BY THE CUSTOMER SPECIFIC BOEING SERVICE BULLETINS. ACCESS DISASSEMBLE DOOR ONLY IF EVIDENCE OF DAMAGE, FATIGUE, DELAMINTION, AND OR BULGING IS FOUND

emp emp

STRUCTURE

ITEMS

REFERENCES MPD MRB

52-470-00 MSI 52-470-00

SB AMM AMM

CDRB 22-1-18 51-05-01-210 52-05-03-211

MPD MRB

52-490-00 MSI 52-490-00

SB AMM AMM

CDRB 22-1-18 51-05-01-210 52-05-03-211

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

I: 16000 CYC I: 3000 DAY

E3 HHI 737-700

3 23-jul-08

I: 16000 CYC I: 3000 DAY

E3 HHI 737-700

4 23-jul-08

ATA: 52 - 70

Page 4 of 4


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 52 - 71

527100 00000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

DOOR WARNING SYSTEM OPERATIONALLY CHECK THE DOOR SENSORS (PROXIMITY OR MECHANICAL SWITCHES AS APPLICABLE) FOR THE PASSENGER CABIN ENTRY / SERVICE, E / E ACCESS, AUTOMATIC OVERWING EXIT, FORWARD ACCESS, CARGO DOORS AND AIRSTAIR DOOR PROXIMITY SENSOR (AS APPLICABLE, IF AIRSTAIRS SYSTEM INCLUDING STAIRS INSTALLED).

112 117 emp 211 212 800 emp emp emp emp emp emp emp

112A 117A 117BL emp emp 821 822 831 833 834 841 843 844

ITEMS

MPD MRB

52-200-00 MSI 52-200-00 RTE:9

AMTOSS AMTOSS AMTOSS AMTOSS AMTOSS AMTOSS

52-71-11-71 52-71-42-71 52-71-41-71 52-71-31-71 52-71-21-71 52-71-61-71

I: 4000 FLH

ATA: 52 - 71

F1 HHI 737-700

2 03-jun-04

Page 1 of 1


HHI R E V

ITEM 53 53 - 09 530900 00000

R

737-6

MAINTENANCE SCHEDULE

530900 01000

R

530900 02000

530900 03000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

FUSELAGE BODY UPPER DETAILED VISUAL INSPECTION OF THE DOOR FRAMES, STOPS, LATCHES AND HINGES ON FORWARD AND AFT ENTRY AND GALLLEY DOOR CUTOUT SURROUND STRUCTURES. E X T E R N A L ACCESS OPEN FWD AND AFT ENTRY AND GALLEY DOORS

221 222 emp emp emp 241 242

emp 831 834 841 844 emp emp

MPD MRB

DETAILED VISUAL INSPECTION OF THE FORWARD AND AFT ENTRY AND GALLEY DOOR CUTOUT SURROUND STRUCTURE (THE DOOR CUTOUT TO, AND INCLUDING THE DOOR SIDE FIRST FRAME OF THE DOOR). I N T E R N A L ACCESS REMOVE GALLEYS/LAVS. REMOVE CABIN INTERIOR AS REQUIRED. REMOVE/DISPLACE INSULATION BLANKETS AS REQUIRED.

221 222 emp 241 242

emp 2001S 222AR emp emp

MPD MRB

GENERAL VISUAL INSPECTION OF THE AUTOMATIC OVERWING EXIT CUTOUT STRUCTURE, FITTINGS AND STOPS. E X T E R N A L ACCESS OPEN AUTOMATIC OVERWING EXITS.

231 232 emp

emp 833 843

MPD MRB

GENERAL VISUAL INSPECTION OF THE PASSENGER COMPARTMENT FLOOR STRUCTURE IN WET AREAS ( WITHIN APPROXIMATELY 20 INCHES FROM DOORS, GALLEYS AND LAVS) FROM LOWER LOBE. I N T E R N A L ACCESS REMOVE CEILING, SIDEWALL PANELS, INSULATION BLANKETS OF FWD AND AFT CARGO COMPARTMENT AS REQUIRED. REMOVE FORWARD AIRSTAIRS AND AIRSTAIRS COMPARTMENT (IF INSTALLED).

113 114 117 118 121 122 125 126 141 142 145 146

S1002 emp 117BL emp emp emp emp emp emp emp emp emp

MPD MRB

ITEMS

53-310-00 MSI 53-310-00 I: 4000 CYC I: 24 MTH

E3 HHI 737-700

2 18-mar-05

T: 24000 CYC T: 8 YRS I: 18000 CYC I: 6 YRS

E3 HHI 737-700

2 23-jul-08

I: 24000 CYC I: 8 YRS

E2 HHI 737-700

2 03-jun-04

T: 8 YRS I: 6 YRS

E2 HHI 737-700

1 03-jun-04

53-360-00 MSI 53-360-00

53-290-00 MSI 53-290-00

53-110-00 MSI 53-110-00

ATA: 53 - 09

Page 1 of 6


HHI R E V

R

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

530900 04000

GENERAL VISUAL INSPECTION OF THE PASSENGER COMPARTMENT FLOOR STRUCTURE IN WET AREA (WITHIN APPROXIMATELY 20 INCHES FROM DOORS, GALLEYS AND LAVS, AND THE FLOOR STRUCTURE BELOW THE DOOR TO AND INCLUDING THE DOORSIDE OF THE FIRST FRAME OF THE DOOR). I N T E R N A L ACCESS REMOVE GALLEYS, LAVS, FLOOR PANELS, SIDEWALLS AND INSULATION BLANKETS AS REQUIRED.

221 222 231 232 241 242

2003S emp emp emp emp emp

MPD MRB

GENERAL VISUAL INSPECTION OF THE PASSENGER COMPARTMENT FLOOR STRUCTURE IN WET AREA INSPECT GALLEY AND LAV ATTACH FITTINGS AND ANY OTHER EASILY VISIBLE PORTIONS OF THE FLOOR STRUCTURE IN WET AREA (WITHIN APPROXIMATELY 20 INCHES FROM GALLEYS AND LAVS, AND THE FLOOR STRUCTURE BELOW THE DOOR TO AND INCLUDING THE DOORSIDE OF THE FIRST FRAME FROM THE DOOR). I N T E R N A L ACCESS GALLEYS AND LAVS REMOVAL IS NOT REQUIRED. REMOVE GALLEY KICK-PLATES AND ANY OTHER EASILY REMOVABLE PANELS FOR INSPECTION.

221 222 231 232 241 242

2004S emp emp emp emp emp

MPD MRB

GENERAL VISUAL INSPECTION OF FORWARD AND AFT CARGO COMPARTMENT FLOOR STRUCTURE. I N T E R N A L ACCESS REMOVE CARGO FLOOR PANELS.

121 122 141 142

1003S emp emp emp

MPD MRB

112A

MPD MRB

530900 05000

R

530900 06000

530900 07000

Date: 23-jul-08

ZONE ACCESS

GENERAL VISUAL INSPECTION OF THE FLIGHT COMPARTMENT FLOOR 112 STRUCTURE FROM LOWER LOBE. I N T E R N A L

STRUCTURE

ITEMS

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

53-380-00 MSI 53-380-00 T: 8 YRS I: 6 YRS

E2 HHI 737-700

1 03-jun-04

T: 8 YRS I: 3 YRS

E2 HHI 737-700

2 23-jul-08

T: 24000 CYC T: 8 YRS I: 18000 CYC I: 6 YRS

E2 HHI 737-700

1 03-jun-04

I: 10 YRS

E2 HHI 737-700

1 03-jun-04

53-390-00 MSI 53-390-00

53-140-00 MSI 53-140-00

53-080-00 MSI 53-080-00

ATA: 53 - 09

Page 2 of 6


HHI R E V

ITEM

R

530900 08000

R

530900 09000

R

530900 10000

R

R

737-6

MAINTENANCE SCHEDULE

530900 11000

R

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

GENERAL VISUAL INSPECTION OF THE FLIGHT COMPARTMENT FLOOR 211 STRUCTURE. 212 I N T E R N A L ACCESS REMOVE SIDEWALLS AND FLOOR PANELS AS REQUIRED. REMOVE/DISPLACE INSULATION BLANKETS AS REQUIRED.

2102S emp

GENERAL VISUAL INSPECTION OF THE PASSENGER COMPARTMENT FLOOR STRUCTURE IN DRY AREAS ( AWAY FROM DOORS, GALLEYS AND LAVS) FROM LOWER LOBE. I N T E R N A L ACCESS REMOVE CEILING, SIDEWALL PANELS, INSULATION BLANKETS. REMOVE FORWARD AIRSTAIRS AND AIRSTAIRS COMPARTMENT (IF INSTALLED).

113 114 117 emp 118 121 122 125 126 141 142 145 146

emp emp 1001S 117BL emp emp emp emp emp emp emp emp emp

MPD MRB

GENERAL VISUAL INSPECTION OF THE FLIGHT COMPARTMENT, 211 INCLUDING SKIN PANELS (SKINS, FRAMES, STRINGERS), 212 CIRCUMFERENTIAL SKIN AND STRINGER SPLICE, CREW CABIN WINDOW CUTOUT STRUCTURE, AND FORWARD PRESSURE BULKHEAD. I N T E R N A L ACCESS REMOVE GLARE SHIELD, LINERS, OVERHEAD UNITS AND PANELS. REMOVE/DISPLACE INSULATION BLANKETS AS REQUIRED.

2101S emp

MPD MRB

GENERAL VISUAL INSPECTION OF THE PASSENGER COMPARTMENT 221 FROM STA 259.5 TO 360 (EXCEPT AREAS AROUND DOOR CUTOUTS), 222 INCLUDING SKIN PANELS (SKINS, FRAMES, STRINGERS), LONGITUDINAL LAP SPLICES, CIRCUMFERENTIAL SKIN AND STRINGER SPLICES. I N T E R N A L ACCESS REMOVE GALLEYS/LAVS. REMOVE CABIN INTERIOR AS REQUIRED. REMOVE/DISPLACE INSULATION BLANKETS AS REQUIRED.

2201S emp

ITEMS

MPD MRB

MPD MRB

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

53-340-00 MSI 53-340-00 I: 10 YRS

E2 HHI 737-700

2 23-jul-08

I: 12 YRS

E2 HHI 737-700

1 03-jun-04

T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS

E2 HHI 737-700

2 23-jul-08

T: 12 YRS T: 36000 CYC I: 8 YRS I: 24000 CYC

E2 HHI 737-700

2 23-jul-08

53-100-00 MSI 53-100-00

53-330-00 MSI 53-330-00

53-350-00 MSI 53-350-00

ATA: 53 - 09

Page 3 of 6


HHI R E V

ITEM 530900 12000

R

737-6

MAINTENANCE SCHEDULE

530900 13000

R

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

GENERAL VISUAL INSPECTION OF PASSENGER COMPARTMENT FROM 231 STA 360 TO 663.75, INCLUDING: 232 1.SKIN PANELS (SKINS, FRAMES AND STRINGERS), emp LONGITUDINAL LAP SPLICES, CIRCUMFERENTIAL SKIN AND STRINGER SPLICES; 2.WINDOW BELT STRUCTURE; 3.OVERWING EMERGENCY EXIT CUTOUT STRUCTURE; 4.FORWARD CARGO DOOR CUTOUT SURROUND STRUCTURE (PORTION IN UPPER LOBE); 5.STA 540 AND 663 BULKHEADS AND SPLICES; 6.OVERWING FRAMES AND STUB BEAMS. ATTENTION TO SKIN DAMAGE AROUND CRITICAL AERODYNAMIC AREAS OF THE FUSELAGE AT A/C OPERATING WITH RVSM (PITOT AND FLUSH STATIC PROBES AREA). I N T E R N A L ACCESS REMOVE CABIN INTERIOR AND INSULATION BLANKETS. OPEN AUTOMATIC OVERWING EXIT DOORS.

S2301 833 843

MPD MRB

GENERAL VISUAL INSPECTION OF THE PASSENGER COMPARTMENT FLOOR STRUCTURE IN DRY AREA (AWAY FROM DOORS, GALLEYS AND LAVS). EXCLUDE FLOOR STRUCTURE FROM STA 540 TO 727. I N T E R N A L ACCESS REMOVE FLOOR PANELS AND SIDEWALLS AS REQUIRED. REMOVE/DISPLACE INSULATION BLANKETS AS REQUIRED.

2002S emp emp emp emp emp

MPD MRB

221 222 231 232 241 242

ITEMS

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

53-400-00 MSI 53-400-00 T: 12 YRS T: 36000 CYC I: 8 YRS I: 24000 CYC

E2 HHI 737-700

4 03-jun-04

I: 12 YRS

E2 HHI 737-700

2 23-jul-08

53-370-00 MSI 53-370-00

ATA: 53 - 09

Page 4 of 6


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

530900 14000

530900 15000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

GENERAL VISUAL INSPECTION OF THE PASSENGER COMPARTMENT 241 FROM STA 663.75 TO 1016 (EXCEPT AREAS AROUND DOOR CUTOUTS), 242 INCLUDING: 1.SKIN PANELS (SKINS, FRAMES AND STRINGERS), LONGITUDINAL LAP SPLICES, CIRCUMFERENTIAL SKIN AND STRINGER SPLICES; 2.WINDOW BELT STRUCTURE; 3.STA 663 BULKHEAD AND SPLICES; 4.STA 727 BULKHEAD; 5.SIDE STRUT SUPPORT FRAME AT STA 706; 6.MAIN LANDING GEAR SUPPORT FRAMES AT STA 695 AND 716; 7.WHEEL WELL FRAME AT STA 685; 8.AFT CARGO DOOR CUTOUT SURROUND STRUCTURE (PORTION IN UPPER LOBE); 9.FORWARD SIDE OF STA 1016 BULKHEAD (CHORDS, PRESSURE WEB, STIFFENERS, CHORD/WEB ATTACHMENTS), INCLUDING VERTICAL FIN FRONT SPAR FITTINGS; 10.STRINGER SPLICE FITTINGS AND TENSION BOLTS AT STA 1016. I N T E R N A L ACCESS REMOVE GALLEYS/LAVS, CABIN INTERIOR AND INSULATION BLANKETS.

2401S emp

GENERAL VISUAL INSPECTION OF THE FUSELAGE LOWER LOBE ABOVE 135 WING BOX CENTER SECTION UPPER PANEL, INCLUDING SIDE SKIN 136 PANELS (SKINS, FRAMES AND STRINGERS), STA 540 BULKHEAD, AND OVERWING FRAMES AND STUB BEAMS. I N T E R N A L ACCESS REMOVE FLOOR PANELS AND INSULATION BLANKETS.

S1301 emp

STRUCTURE

ITEMS

REFERENCES MPD MRB

MPD MRB

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

53-410-00 MSI 53-410-00 T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS

E2 HHI 737-700

1 03-jun-04

T: 36000 CYC T: 12 YRS I: 36000 CYC I: 10 YRS

E2 HHI 737-700

1 03-jun-04

53-190-00 MSI 53-190-00

ATA: 53 - 09

Page 5 of 6


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

530900 16000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

GENERAL VISUAL INSPECTION OF THE FUSELAGE LOWER LOBE ABOVE 137 MAIN LANDING GEAR WHEEL WELL, INCLUDING: 138 1.PRESSURE DECK WEB TO STIFFENERS, STIFFENER ATTACHMENT TO FLOOR BEAM AT STA 727; 2.SIDE SKIN PANELS, CIRCUMFERENTIAL SKIN AND STRINGER SPLICE; 3.BULKHEADS AT STA 663 AND 727; 4.SIDE STRUT SUPPORT FRAME AT STA 706; 5.MAIN LANDING GEAR SUPPORT FRAME AT STA 695 AND 716; 6.WHEEL WELL FRAME AT STA 685. I N T E R N A L ACCESS REMOVE FLOOR PANELS AND INSULATION BLANKETS.

STRUCTURE

S1302 emp

REFERENCES MPD MRB

THRESHOLD INTERVAL

EFF

R L ITEM BY E E REVISION P V DATE

53-200-00 MSI 53-200-00 T: 36000 CYC T: 12 YRS I: 36000 CYC I: 10 YRS

ITEMS

TSK

ATA: 53 - 09

E2 HHI 737-700

1 03-jun-04

Page 6 of 6


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 53 - 13

531300 00000

531300 01000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

TAIL SECTION GENERAL VISUAL INSPECTION OF THE AREA AFT OF STA 1016 PRESSURE 311 BULKHEAD TO STA 1088, INCLUDING: 312 1.SKIN PANELS (SKINS, FRAMES AND STRINGERS), LONGITUDINAL LAP SPLICES, CIRCUMFERENTIAL SKIN AND STRINGER SPLICES; 2.AFT SIDE OF STA 1016 BULKHEAD (CHORDS, PRESSURE WEB, STIFFENERS, CHORD/WEB ATTACHMENTS) 3.STRINGER SPLICE FITTINGS AND TENSION BOLTS AT STA 1016. 4.STA 1088 BULKHEAD, INCLUDING VERTICAL FIN REAR SPAR FITTINGS AND HORIZONTAL STABILIZER CENTER SECTION JACKSREW FITTING LUGS AND BOLTS. I N T E R N A L

311BL emp

GENERAL VISUAL INSPECTION OF THE STABILIZER TORSION BOX COMPARTMENT AND APU COMPARTMENT, INCLUDING: 1.SKIN PANELS (SKINS, FRAMES AND STRINGERS), LONGITUDINAL LAP SPLICES 2.STA 1088 BULKHEAD, INCLUDING VERTICAL FIN REAR SPAR FITTINGS; 3.FORWARD SIDE OF STA 1156 BULKHEAD, INCLUDING HORIZONTAL STABILIZER HINGE FITTINGS AND BOLTS; 4.UPPER HORIZONTAL DECK (AT STRINGER 6) AND LOWER HORIZONTAL DECK (AT STRINGER 12). I N T E R N A L ACCESS FOR AREA BELOW STRINGER 12, REMOVE APU FIREWALLS AND APU PLENUM. FOR AREA ABOVE STRINGER 12, ADJUST STABILIZER TRIM AS REQUIRED. FOR ACCESS TO STA 1156 HORIZONTAL STABILIZER HINGE FITTING LUGS AND BOLTS, REMOVE HORIZONTAL STABILIZER REAR SPAR SLIDING SEAL AS REQUIRED. ACCESS PANELS 333BT AND 343 BT NOT ON ALL A/C'S.

311BL emp 315A 3101S 331A 332AB 332AT 333AB 333AT 333BT 341A 342AB 342AT 343AB 343AT

313 314 315 316 emp emp emp emp emp emp emp emp emp emp emp

ITEMS

MPD MRB

MPD MRB

53-420-00 MSI 53-420-00 T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS

E2 HHI 737-700

1 03-jun-04

T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS

E2 HHI 737-700

2 22-mar-07

53-430-00 MSI 53-430-00

ATA: 53 - 13

Page 1 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

531300 02000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

GENERAL VISUAL INSPECTION OF THE AFT SIDE OF STA 1156 BULKHEAD. 317 I N T E R N A L 318 ACCESS

STRUCTURE

318BR emp

REFERENCES MPD MRB

THRESHOLD INTERVAL

EFF

R L ITEM BY E E REVISION P V DATE

53-440-00 MSI 53-440-00 T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS

ITEMS

TSK

ATA: 53 - 13

E2 HHI 737-700

1 03-jun-04

Page 2 of 2


HHI R E V

ITEM 53 - 15 531500 00000

R

531500 01000

R

R

737-6

MAINTENANCE SCHEDULE

531500 02000

R

531500 03000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

NOSE AND MAIN LANDING GEAR WHEEL WELL GENERAL VISUAL INSPECTION OF THE KEEL BEAM IN WHEEL WELL 139 (STA663.75 TO 727), INCLUDING KEEL BEAM CHORDS, WEBS, STIFFENERS, 193 SPLICE, KEEL BEAM/REAR SPAR ATTACHMENT ANGLES. emp I N T E R N A L

emp 193B 193D

MPD MRB

GENERAL VISUAL INSPECTION OF THE NOSE LANDING GEAR WHEEL WELL, INCLUDING CANTED BULKHEAD (STA 224.8 TO 227.8), STA 294.5 BULKHEAD, SIDE AND TOP PANELS, TRUNNION SUPPORT FITTING, ACTUATOR SUPPORT FITTING, AND DRAG BRACE FITTING. E X T E R N A L

115 116

emp emp

MPD MRB

53-020-00 MSI 53-020-00

AMM AMM

51-05-01-210 53-05-03-210

GENERAL VISUAL INSPECTION OF THE MAIN LANDING GEAR WHEEL WELL, INCLUDING: 1. PRESSURE DECK WEB AND STIFFENERS, INCLUDING ATTACHMENT TO WING CENTER SECTION REAR SPAR AT STA 663; 2. BULKHEAD AT STA 663; 3. BULKHEAD AND PRESSURE WEB AT STA 727; 4. KEEL BEAM CHORDS, WEBS, STIFFENERS AND SPLICE, KEEL BEAM/ REAR SPAR ATTACHMENT ANGLES; 5. STRINGER 18A WEB, CHORD AND LINKS; 6. SIDE STRUT SUPPORT FRAME AT STA 706; 7. MAIN LANDING GEAR SUPPORT FRAME AT STA 695 AND716; 8. WHEEL WELL FRAME AT STA 685; 9. FLAP TRACK SUPPORT FITTINGS. E X T E R N A L

133 134 139 193

emp emp emp emp

MPD MRB

53-050-00 MSI 53-050-00

AMM AMM

51-05-01-210 53-05-03-210

1122S 112A

MPD MRB

53-070-00 MSI 53-070-00

GENERAL VISUAL INSPECTION OF THE FUSELAGE LOWER LOBE FROM 112 STA 178 BULKHEAD TO CANTED BULKHEAD (STA 224.8 TO 227.8), emp INCLUDING BULKHEADS, SKIN PANELS (SKINS, FRAMES, STRINGERS), LONGITUDINAL LAP SPLICES, FORWARD ACCESS DOOR CUTOUT, AND NOSE WHEEL WELL CUTOUT. I N T E R N A L ACCESS REMOVE/ DISPLACE INSULATION BLANKETS AS REQUIRED. REMOVE WEATHER RADAR RT SHELF.

ITEMS

53-220-00 MSI 53-220-00 I: 18000 CYC I: 6 YRS

E2 HHI 737-700

2 03-jun-04

T: 9 YRS I: 3 YRS

E2 HHI 737-700

2 23-jul-08

T: 9 YRS I: 3 YRS

E2 HHI 737-700

3 23-jul-08

T: 36000 CYC T: 12 YRS I: 8 YRS I: 24000 CYC

E2 HHI 737-700

2 03-jun-04

ATA: 53 - 15

Page 1 of 2


HHI

737-6

MAINTENANCE SCHEDULE

R E V

ITEM

R

531500 04000

R

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

SPECIAL DETAILED INSPECTION OF THE WHEEL WELL AFT BULKHEAD 141 INSPECT (ULTRASONIC) THE AFT SIDE OF 727 BULKHEAD AT THE FRAME 142 AROUND THE SIX FASTENERS THROUGH THE INNER CHORD AND WEB AT WL 201. (PSE 53-40-16-2) I N T E R N A L NOTE( E, I ) FOR 737-600 L/N #1-766 THRESHOLD IS 34,000 FC, REPEAT IS 7,000 FC. FOR 737-600 L/N #767-1192 THRESHOLD IS 56,000 FC, REPEAT IS 7,000 FC. FOR737-700 L/N #1-766 THRESHOLD IS 27,000 FC, REPEAT IS 7,000 FC. FOR 737-700 L/N #767-1192 THRESHOLD IS 56,000 FC, REPEAT IS 7,000 FC. FOR 737-600 AND 737-700 AIRPLANES SEE INTERVAL NOTE FOR AIRPLANE SPECIFIC THRESHOLD, REPEAT AND SAMPLING INTERVALS. ACCESS REMOVE AND/OR DISPLACE THE FORWARD BULKHEAD, SIDEWALL CEILING PANELS AND INSULATION BLANKETS AS REQUIRED.

STRUCTURE

emp emp

ITEMS

THRESHOLD INTERVAL

REFERENCES MPD MRB

53-668-00 MSI 57-05-02-200

AMM AMM

53-668-00 53-05-02-010-801

T: 27000 CYC I: 7000 CYC

ATA: 53 - 15

TSK

EFF

E4 HHI 737-700

R L ITEM BY E E REVISION P V DATE

2 23-jul-08

Page 2 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 53 - 30

533000 00000

533000 01000

533000 02000

533000 03000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

FUSELAGE EXTERIOR GENERAL VISUAL INSPECTION OF THE DOOR CUTOUTS AT FORWARD ACCESS DOOR, FORWARD AIRSTAIRS DOOR AND FORWARD E/E BAY DOOR. E X T E R N A L ACCESS OPEN FORWARD ACCESS DOOR, AIRSTAIRS DOOR AND E/E COMPARTMENT DOOR.

112 117 emp

112A 117A 117BL

MPD MRB

GENERAL VISUAL INSPECTION OF THE FUSELAGE SKIN UNDER DORSAL 321 FIN AND AFT TO STA 1016, INCLUDING CIRCUMFERENTIAL SPLICE. I N T E R N A L

321A

MPD MRB

GENERAL VISUAL INSPECTION OF THE AREA UNDER LOWER WING-TO-BODY FAIRING (AFT OF WHEEL WELL), INCLUDING SKIN PANELS, LONGITUDINAL LAP SPLICES, CIRCUMFERENTIAL SKIN SPLICE, STRINGER 18 STRAP AT SIDE OF BODY, STRINGER 18A (WEB, CHORDS AND LINKS), AND KEEL BEAM EXTENSION. I N T E R N A L

149 194 emp emp emp emp emp emp emp emp emp emp emp emp emp emp

emp 194AL 194AR 194BL 194BR 194CL 194CR 194DL 194DR 194E 194FL 194FR 194GL 194GR 194HL 194HR

MPD MRB

GENERAL VISUAL INSPECTION OF THE AREA UNDER WING-TO-BODY FAIRING (ABOVE WING), INCLUDING SKIN PANELS, CIRCUMFERENTIAL SKIN SPLICES, AND STRINGER 18 STRAP AT SIDE OF BODY. I N T E R N A L

195 emp emp 196 emp emp

195AL 195BL 195CL 196AR 196BR 196CR

MPD MRB

ITEMS

53-010-00 MSI 53-010-00 I: 24 MTH I: 4000 CYC

E2 HHI 737-700

3 03-jun-04

I: 24000 CYC I: 8 YRS

E2 HHI 737-700

1 03-jun-04

T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS

E2 HHI 737-700

1 03-jun-04

T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS

E2 HHI 737-700

2 05-sep-06

53-450-00 MSI 53-450-00

53-270-00 MSI 53-270-00

53-280-00 MSI 53-280-00

ATA: 53 - 30

Page 1 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

533000 04000

533000 05000

533000 06000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

GENERAL VISUAL INSPECTION OF THE VERTICAL FIN FRONT SPAR FITTING LUGS AND BOLTS (STA 1016) I N T E R N A L ACCESS PIN REMOVAL IS NOT REQUIRED.

322 emp emp emp

323AL 323AR 323BL 323BR

MPD MRB

GENERAL VISUAL INSPECTION OF THE VERTICAL FIN REAR SPAR FITTING LUGS AND BOLTS STA 1088. INSPECT FUSELAGE SKIN UNDER VERTICAL FIN FROM STA 1016 TO 1088. I N T E R N A L

323 emp emp emp emp emp

323AL 323AR 323BL 323BR 323CL 323CR

MPD MRB

53-480-00 MSI 53-480-00

AMM AMM

51-05-01-210 53-05-03-210

GENERAL VISUAL INSPECTION OF THE VERTICAL FIN FRONT SPAR FITTING LUGS AND BOLTS (STA 1016) I N T E R N A L ACCESS PIN REMOVAL IS REQUIRED. REMOVE ONLY ONE PIN AT A TIME.

322 emp emp emp

323AL 323AR 323BL 323BR

MPD MRB

53-470-00 MSI 53-470-00

ITEMS

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

53-460-00 MSI 53-460-00 T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS

E2 HHI 737-700

2 18-mar-05

T: 12 YRS T: 36000 CYC I: 8 YRS I: 24000 CYC

E2 HHI 737-700

2 05-sep-06

T: 20 YRS I: 8 YRS

E2 HHI 737-700

1 03-jun-04

ATA: 53 - 30

Page 2 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 53 - 51

535100 00000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

WING-TO-BODY FAIRING GENERAL VISUAL INSPECTION OF THE AREA UNDER LOWER WING-TO-BODY FAIRING (FORWARD OF WING BOX), INCLUDING SKIN PANELS, LONGITUDINAL LAP SPLICES, KEEL BEAM EXTENSION, WING-TO-BODY DRAG ANGLES, AND STA 540 BULKHEAD. I N T E R N A L

129 191 emp emp emp emp emp emp emp emp emp emp emp emp

emp 191AL 191AR 191BL 191BR 191CL 191CR 191D 191FL 191FR 191GL 191GR 191HL 191HR

ITEMS

MPD MRB

53-180-00 MSI 53-180-00 T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS

ATA: 53 - 51

E2 HHI 737-700

1 03-jun-04

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 53 - 81

538100 00000

538100 01000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

UNDERFLOOR NOSE COMPARTMENT AND ELECTRONIC EQUIPMENT COMPARTMENT GENERAL VISUAL INSPECTION OF THE E/E COMPARTMENT (STA294.5 TO 117 396), INCLUDING: emp 1.SKIN PANELS (SKINS, FRAMES, STRINGERS), LONGITUDINAL LAP 118 SPLICES, CIRCUMFERENTIAL SKIN AND STRINGER SPLICES, BULKHEAD AT STA 294.5; 2.E/E COMPARTMENT DOOR AND AIRSTAIRS DOOR CUTOUT SURROUND STRUCTURE 3. FORWARD ENTRY AND GALLEY DOOR CUTOUT SURROUND STRUCTURE (PORTION IN LOWER LOBE). I N T E R N A L ACCESS REMOVE LRU'S AND RACKS, DO NOT REMOVE PERMANENTLY INSTALLED STRUCTURE. REMOVE/ DISPLACE INSULATION BLANKETS AS REQUIRED.

1102S 117A emp

MPD MRB

GENERAL VISUAL INSPECTION OF THE FORWARD SIDE OF STA 178 BULKHEAD. I N T E R N A L ACCESS OPEN RADOME

111

MPD MRB

111

ITEMS

53-120-00 MSI 53-120-00 T: 12 YRS T: 36000 CYC I: 24000 CYC I: 8 YRS

E2 HHI 737-700

2 18-mar-05

T: 12 YRS T: 36000 CYC I: 8 YRS I: 24000 CYC

E2 HHI 737-700

1 03-jun-04

53-060-00 MSI 53-060-00

ATA: 53 - 81

Page 1 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

538100 02000

GENERAL VISUAL INSPECTION OF THE FUSELAGE LOWER LOBE FROM CANTED BULKHEAD (STA 224.8 TO 227.8) TO STA 294, INCLUDING: 1.SKIN PANELS (SKINS, FRAMES, STRINGERS), LONGITUDINAL LAP SPLICES, CIRCUMFERENTIAL SKIN AND STRINGER SPLICES, BULKHEAD AT STA 259.5; 2.NOSE WHEEL WELL CUTOUT SURROUND STRUCTURE, NOSE WHEEL WELL SIDE AND TOP PANELS; 3.TRUNNION SUPPORT FITTING, ACTUATOR SUPPORT FITTING AND DRAG BRACE FITTING. I N T E R N A L ACCESS ACCESS THROUGH NOSE WHEEL WELL SIDE AND TOP ACCESS PANELS, AND THROUGH ACCESS PANEL IN CREW FLOOR. REMOVE/ DISPLACE INSULATION BLANKETS AS REQUIRED.

Date: 23-jul-08

ZONE ACCESS 113 emp emp 114 emp emp emp

STRUCTURE

113AC 113AW 113BW 1101S 114AC 114AW 114BW

ITEMS

REFERENCES MPD MRB

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

53-090-00 MSI 53-090-00 T: 12 YRS T: 36000 CYC I: 8 YRS I: 24000 CYC

ATA: 53 - 81

E2 HHI 737-700

1 03-jun-04

Page 2 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 53 - 82

538200 00000

538200 01000

538200 02000

538200 03000

538200 04000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

FORWARD CARGO COMPARTMENT DETAILED VISUAL INSPECTION OF THE FORWARD CARGO DOOR SURROUND STRUCTURE, FITTINGS AND STOPS. E X T E R N A L

122

821

DETAILED VISUAL INSPECTION OF THE FORWARD CARGO DOOR CUTOUT 122 SURROUND STRUCTURE. I N T E R N A L ACCESS REMOVE DOOR REVEALS, SIDEWALLS AS REQUIRED AND INSULATION BLANKETS AS REQUIRED.

1221S

GENERAL VISUAL INSPECTION OF THE FORWARD BILGE SKIN PANELS 123 INCLUDING SKINS, FRAMES, STRINGERS, LONGITUDINAL LAP SPLICES, 124 AND CARGO DOOR CUTOUT SURROUND STRUCTURE IN BILGE. I N T E R N A L ACCESS REMOVE CARGO FLOOR PANELS AND SCUFF PLATES. REMOVE/DISPLACE INSULATION BLANKETS AS REQUIRED.

1202S emp

GENERAL VISUAL INSPECTION OF THE FORWARD CARGO COMPARTMENT 121 SKIN PANELS (SKINS, FRAMES AND STRINGERS). 122 I N T E R N A L ACCESS REMOVE SIDEWALL, CEILING PANELS, INSULATION BLANKETS AS REQUIRED.

1201S emp

GENERAL VISUAL INSPECTION OF THE AREA AFT OF FORWARD CARGO 125 COMPARTMENT, INCLUDING SKIN PANELS (SKINS, FRAMES, STRINGERS), 126 LONGITUDINAL LAP SPLICES, CIRCUMFERENTIAL SKIN AND STRINGER SPLICES, AND FORWARD SIDE OF STA 540 BULKHEAD AND BULKHEAD SPLICES. I N T E R N A L ACCESS REMOVE/DISPLACE FORWARD CARGO COMPARTMENT AFT BULKHEAD PANELS, INSULATION BLANKETS AND DUCTING AS REQUIRED.

1203S emp

ITEMS

MPD MRB

MPD MRB

MPD MRB

MPD MRB

MPD MRB

53-030-00 MSI 53-030-00 I: 24 MTH I: 4000 CYC

E3 HHI 737-700

2 18-mar-05

T: 24000 CYC T: 8 YRS I: 18000 CYC I: 6 YRS

E3 HHI 737-700

1 03-jun-04

T: 24000 CYC T: 8 YRS I: 18000 CYC I: 6 YRS

E2 HHI 737-700

3 05-sep-06

T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS

E2 HHI 737-700

1 03-jun-04

T: 36000 CYC T: 12 YRS I: 36000 CYC I: 10 YRS

E2 HHI 737-700

2 03-jun-04

53-150-00 MSI 53-150-00

53-160-00 MSI 53-160-00

53-130-00 MSI 53-130-00

53-170-00 MSI 53-170-00

ATA: 53 - 82

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 53 - 84

538400 00000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

AIR CONDITIONING COMPARTMENT LH AND RH GENERAL VISUAL INSPECTION OF THE KEEL BEAM UNDER WING-TO-BODY FAIRING (UNDER WING BOX, STA 540 TO 663.75), INCLUDING KEEL BEAM CHORDS, WEBS, STIFFENERS, SPLICE, KEEL BEAM/ REAR SPAR ATTACHMENT ANGLES. I N T E R N A L ACCESS OPTION 1: REMOVE CENTER WING-TO-BODY FAIRING (192CL, 192CR, 192E, 192F) AND OPEN AC BAY ACCESS DOOR. OPTION 2: OPEN AC BAY DOOR AND REMOVE AC PACK TO GAIN ACCESS TO ACCESS HOLES.

139 192 emp emp emp

1004S 192CL 192CR 192E 192F

ITEMS

MPD MRB

53-210-00 MSI 53-210-00 T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS

ATA: 53 - 84

E2 HHI 737-700

3 03-jun-04

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 53 - 85

538500 00000

538500 01000

538500 02000

538500 03000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

AFT CARGO COMPARTMENT DETAILED VISUAL INSPECTION OF THE AFT CARGO DOOR SURROUND 142 STRUCTURE, FITTINGS AND STOPS. E X T E R N A L

822

DETAILED VISUAL INSPECTION OF THE AFT CARGO DOOR CUTOUT SURROUND STRUCTURE. I N T E R N A L ACCESS REMOVE DOOR REVEALS, SIDEWALLS AND INSULATION BLANKETS.

1421S

142

GENERAL VISUAL INSPECTION OF THE AFT BILGE SKIN PANELS (SKINS, 143 FRAMES, STRINGERS), LONGITUDINAL LAP SPLICES, CIRCUMFERENTIAL 144 SKIN AND STRINGER SPLICES, STA 727 BULKHEAD AND PRESSURE WEB, AND CARGO DOOR CUTOUT SURROUND STRUCTURE IN BILGE. I N T E R N A L ACCESS REMOVE CARGO FLOOR PANELS AND SCUFF PLATES. REMOVE/DISPLACE INSULATION BLANKETS AS REQUIRED.

1402S emp

GENERAL VISUAL INSPECTION OF THE AFT CARGO COMPARTMENT, 141 INCLUDING: 142 1.SIDE SKIN PANELS ( SKIN, FRAMES, STRINGERS), CIRCUMFERENTIAL SKIN AND STRINGER SPLICE; 2.STRINGER 18 STRAP AT SIDE OF BODY; 3.STRINGER 18A WEB, CHORD AND LINKS; 4.AFT SIDE OF STA 727 BULKHEAD AND PRESSURE WEB. I N T E R N A L ACCESS REMOVE AFT CARGO COMPARTMENT AFT BULKHEAD PANEL AND POTABLE WATER TANK. REMOVE/DISPLACE INSULATION BLANKETS AS REQUIRED.

S1401 emp

ITEMS

MPD MRB

MPD MRB

53-030-00 MSI 53-030-00 I: 4000 CYC I: 24 MTH

E3 HHI 737-700

2 18-mar-05

T: 24000 CYC T: 8 YRS I: 18000 CYC I: 6 YRS

E3 HHI 737-700

1 03-jun-04

T: 24000 CYC T: 8 YRS I: 18000 CYC I: 6 YRS

E2 HHI 737-700

2 05-sep-06

T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS

E2 HHI 737-700

1 03-jun-04

53-240-00 MSI 53-240-00

MPD MRB

53-250-00 MSI 53-250-00

AMM AMM

51-05-01-210 53-05-03-210

MPD MRB

53-230-00 MSI 53-230-00

ATA: 53 - 85

Page 1 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

538500 04000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

GENERAL VISUAL INSPECTION OF THE AREA AFT CARGO COMPARTMENT, 145 INCLUDING: 146 1.SKIN PANELS (SKINS, FRAMES, STRINGERS), LONGITUDINAL LAP SPLICES, CIRCUMFERENTIAL SKIN AND STRINGER SPLICES; 2.AFT ENTRY AND GALLEY DOOR CUTOUT SURROUND STRUCTURE IN LOWER LOBE; 3.STA 1016 BULKHEAD, INCLUDING CHORDS, PRESSURE WEB, STIFFENERS, CHORD/WEB ATTACHMENTS; 4.STRINGER SPLICE FITTINGS AND TENSION BOLTS AT STA 1016. I N T E R N A L ACCESS REMOVE AFT CARGO COMPARTMENT AFT BULKHEAD PANEL AND POTABLE WATER TANK. REMOVE/DISPLACE INSULATION BLANKETS AS REQUIRED.

STRUCTURE

1403S emp

REFERENCES MPD MRB

THRESHOLD INTERVAL

EFF

R L ITEM BY E E REVISION P V DATE

53-260-00 MSI 53-260-00 T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS

ITEMS

TSK

ATA: 53 - 85

E2 HHI 737-700

1 03-jun-04

Page 2 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 54 54 - 30

543000 00000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

NACELLES/ PYLONS PYLON-SKIN GENERAL VISUAL INSPECTION OF THE EXTERNAL AREAS OF L/H AND R/H STRUT BOX, INCLUDING UPPER AND LOWER SPARS, FORWARD ENGINE MOUNT BULKHEAD, AFT BULKHEAD, AND SIDE SKINS. I N T E R N A L ACCESS REMOVE INSULATION BLANKETS/HEAT SHIELDS AND FAN COWLS. TR'S MUST BE OPEN TO REMOVE ACCESS PANELS 431EL, 431ER, 441EL AND 441ER.

433 emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp 443 emp emp emp emp emp emp emp

413 414 415 416 423 424 425 426 431AT 431BL 431BR 431CL 431CR 431EL 431ER S4331 441AT 441BL 441BR 441CL 441CR 441EL 441ER S4431

ITEMS

MPD MPD MRB MRB

54-070-01 54-070-02 MSI 54-070-01 MSI 54-070-02 I: 18000 CYC I: 6 YRS

ATA: 54 - 30

E2 HHI 737-700

3 25-apr-06

Page 1 of 3


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

543000 01000

GENERAL VISUAL INSPECTION OF THE INTERNAL AREAS OF STRUT BOX L/H AND R/H, INCLUDING UPPER AND LOWER SPARS, FORWARD AND AFT ENGINE MOUNT BULKHEAD, AFT AND MID BULKHEADS, AND SIDE SKINS. I N T E R N A L ACCESS DISASSEMBLE PNEUMATIC DUCTS AS REQUIRED. TR'S MUST BE OPEN TO REMOVE ACCESS PANELS 431EL, 431ER, 441EL AND 441ER.

433 emp emp emp emp emp emp emp emp emp emp emp emp emp emp 443 emp emp emp emp emp emp emp emp emp emp emp emp emp emp

431BL 431BR 431CL 431CR 431DL 431DR 431EL 431ER 4332S 433AL 433AR 433AT 433BT 433CT 433DT 441BL 441BR 441CL 441CR 441DL 441DR 441EL 441ER 4432S 443AL 443AR 443AT 443BT 443CT 443DT

MPD MPD MRB MRB

FUNCTIONALLY CHECK THE LEFT ENGINE FORWARD STRUT AND AFT STRUT FAIRING DRAINS.

410 430 emp

emp 434AR 434BL

MPD MRB

543001 00000

Date: 23-jul-08

ZONE ACCESS

STRUCTURE

ITEMS

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

54-080-01 54-080-02 MSI 54-080-01 MSI 54-080-02 I: 18000 CYC I: 6 YRS

E2 HHI 737-700

3 25-apr-06

T: 9000 CYC T: 30 MTH I: 9000 CYC I: 30 MTH

F2 HHI 737-700

1 30-nov-05

54-090-01 MSI 54-090-01 RTE:9

ATA: 54 - 30

Page 2 of 3


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

543002 00000

DESCRIPTION

ZONE ACCESS

FUNCTIONALLY CHECK THE RIGHT ENGINE FORWARD STRUT AND AFT 420 STRUT FAIRING DRAINS. 440 emp

STRUCTURE

emp 444AL 444BR

REFERENCES MPD MRB

THRESHOLD INTERVAL

ITEMS

EFF

R L ITEM BY E E REVISION P V DATE

54-090-02 MSI 54-090-02 RTE:9 T: 9000 CYC T: 30 MTH I: 30 MTH I: 9000 CYC

Date: 23-jul-08

TSK

ATA: 54 - 30

F2 HHI 737-700

1 30-nov-05

Page 3 of 3


HHI R E V

ITEM 54 - 40

R

737-6

MAINTENANCE SCHEDULE

544000 00000

R

544000 01000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

ATTACHMENT FITTINGS GENERAL VISUAL INSPECTION OF THE L/H AND R/H STRUTS TO WING UPPER LINK, DIAGONAL BRACE, SIDE LINKS, AND STRUT ATTACHMENT FITTINGS. I N T E R N A L ACCESS REMOVE UPPER AND LOWER WING JUNCTION FAIRINGS. REMOVE THRUST REVERSER STRUT FAIRING AND AFT STRUT FAIRING. TR'S MUST BE OPEN TO REMOVE ACCESS PANELS 431EL, 431ER, 441EL AND 441ER.

431 emp emp emp emp emp 434 emp emp 441 emp emp emp emp emp 444 emp emp

431CL 431CR 431DL 431DR 431EL 431ER 434AL 434AR 434BL 441CL 441CR 441DL 441DR 441EL 441ER 444AL 444AR 444BR

MPD MPD MRB MRB

DETAILED VISUAL INSPECTION OF L/H AND R/H PINS AND FUSE PINS ON UPPER LINK, MIDSPAR, DIAGONAL BRACE, AND SIDE LINKS. PIN REMOVAL IS NOT REQUIRED. I N T E R N A L ACCESS REMOVE UPPER AND LOWER WING JUNCTION FAIRINGS. REMOVE THRUST REVERSER STRUT FAIRING AND AFT STRUT FAIRING PANELS, AS REQUIRED. TR'S MUST BE OPEN TO REMOVE ACCESS PANELS 431EL, 431ER, 441EL AND 441ER.

431 emp emp emp emp emp 434 emp emp 441 emp emp emp emp emp 444 emp emp

431CL 431CR 431DL 431DR 431EL 431ER 434AL 434AR 434BL 441CL 441CR 441DL 441DR 441EL 441ER 444AL 444AR 444BR

MPD MPD MRB MRB

ITEMS

54-040-01 54-040-02 MSI 54-040-01 MSI 54-040-02 I: 9000 CYC I: 30 MTH I: 36 MTH

E2 HHI 737-700

4 23-jul-08

I: 9000 CYC I: 30 MTH

E3 HHI 737-700

3 03-jun-04

54-050-01 54-050-02 MSI 54-050-01 MSI 54-050-02

ATA: 54 - 40

Page 1 of 4


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

544000 02000

GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT FORWARD ENGINE MOUNT ASSEMBLY, INCLUDING FAN CASE FITTING, SIDE LINKS, HANGER AND LINK PINS. E X T E R N A L ACCESS OPEN FAN COWL.

413 414 423 424

GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT STRUT ATTACH BOLTS AT FORWARD ENGINE MOUNT. I N T E R N A L ACCESS REMOVE FAN COWL.

413 414 emp emp 423 424

413 414 431AT 441AT 423 424

MPD MPD MRB MRB

54-015-01 54-015-02 MSI 54-015-01 MSI 54-015-02

AMM AMM

54-05-03-210 51-05-01-210

GENERAL VISUAL INSPECTION OF THE L/H AND R/H AFT ENGINE MOUNT ASSEMBLY, INCLUDING THRUST LINKS AND THRUST LINK PINS; MOUNT TO ENGINE LEFT, CENTER AND RIGHT LINKS, INCLUDING LINK PINS; HANGER AND EVENER BAR; ATTACH BOLTS. E X T E R N A L

415 416 425 426

415 416 425 426

MPD MPD MRB MRB

54-030-01 54-030-02 MSI 54-030-01 MSI 54-030-02

DETAILED VISUAL INSPECTION OF THE L/H AND R/H BORES OF PINS AND FUSE PINS ON UPPER LINK, MIDSPAR, DIAGONAL BRACE, AND SIDE LINKS. PIN REMOVAL IS NOT REQUIRED. I N T E R N A L ACCESS TR'S MUST BE OPEN TO REMOVE ACCESS PANELS 431EL, 431ER, 441EL AND 441ER.

431 emp emp emp emp emp 434 emp emp 441 emp emp emp emp emp 444 emp emp

544000 03000

544000 04000

544000 05000

Date: 23-jul-08

ZONE ACCESS

STRUCTURE

413 414 423 424

431CL 431CR 431DL 431DR 431EL 431ER 434AL 434AR 434BL 441CL 441CR 441DL 441DR 441EL 441ER 444AL 444AR 444BR

ITEMS

REFERENCES MPD MPD MRB MRB

MPD MPD MRB MRB

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

54-010-01 54-010-02 MSI 54-010-01 MSI 54-010-02 I: 6 YRS I: 18000 CYC

E2 HHI 737-700

3 25-apr-06

I: 18000 CYC I: 6 YRS

E2 HHI 737-700

4 05-sep-06

I: 18000 CYC I: 6 YRS

E2 HHI 737-700

2 25-apr-06

I: 36000 CYC I: 10 YRS

E3 HHI 737-700

3 03-jun-04

54-060-01 54-060-02 MSI 54-060-01 MSI 54-060-02

ATA: 54 - 40

Page 2 of 4


HHI

737-6

MAINTENANCE SCHEDULE

R E V

ITEM

R

544000 06000

R

Date: 23-jul-08

DESCRIPTION GENERAL VISUAL INSPECTION OF THE FORWARD AND AFT ENGINE MOUNT TO STRUT SHEAR PINS. I N T E R N A L NOTE( I ) AT ENGINE REMOVAL. ACCESS ENGINE REMOVAL REQUIRED.

ZONE ACCESS 413 emp 414 emp emp emp 423 emp 424 emp emp emp 433 emp emp emp emp emp emp emp emp 443 emp emp emp emp emp emp emp emp

STRUCTURE

4001S 413 414 415 416 416CR 423 S4002 424 425 425CL 426 431AL 431AT 431BL 431BR 431CL 431DL 431DR 431EL 431ER 441AL 441AT 441BL 441BR 441CL 441DL 441DR 441EL 441ER

ITEMS

REFERENCES MPD MRB MPD MPD MRB MRB

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

54-020-01 MSI 54-020-01 54-020-01 54-020-02 MSI 54-020-01 MSI 54-020-02 I: 1 EC

ATA: 54 - 40

E2 HHI 737-700

4 23-jul-08

Page 3 of 4


HHI

737-6

MAINTENANCE SCHEDULE

R E V

ITEM

N

544000 06100

N

Date: 23-jul-08

DESCRIPTION GENERAL VISUAL INSPECTION OF THE FORWARD AND AFT ENGINE MOUNT TO STRUT SHEAR PINS. I N T E R N A L NOTE( I ) AT ENGINE REMOVAL. ACCESS ENGINE REMOVAL REQUIRED.

ZONE ACCESS 423 emp 424 emp emp emp 443 emp emp emp emp emp emp emp emp

STRUCTURE

423 S4002 424 425 425CL 426 441AL 441AT 441BL 441BR 441CL 441DL 441DR 441EL 441ER

ITEMS

REFERENCES MPD MRB

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

54-020-02 MSI 54-020-02 I: 1 EC

ATA: 54 - 40

E2 HHI 737-700

0 23-jul-08

Page 4 of 4


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 55 55 - 10

551000 00000

551000 01000

551000 02000

551000 03000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

STABILIZERS STABILIZER- HORIZONTAL GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT HORIZONTAL STABILIZER FRONT SPAR TERMINAL FITTINGS AND CENTER SECTION FRONT SPAR LUGS. I N T E R N A L ACCESS BOLT REMOVAL IS NOT REQUIRED.

331 341

GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT HORIZONTAL STABILIZER REAR SPAR TERMINAL FITTINGS AND CENTER SECTION REAR SPAR LUGS. I N T E R N A L ACCESS BOLT REMOVAL IS NOT REQUIRED .

333 emp 343 emp

331A 341A

333AB 333AT 343AB 343AT

GENERAL VISUAL INSPECTION OF THE HORIZONTAL STABILIZER CENTER 311 SECTION JACKSCREW FITTING. 312 I N T E R N A L

311BL emp

GENERAL VISUAL INSPECTION OF THE HORIZONTAL STABILIZER CENTER 313 SECTION FRONT SPAR, REAR SPAR, PIVOT FITTINGS, AND PRIMARY AND emp SECONDARY THRUST BEAMS. 314 I N T E R N A L ACCESS ADJUST STABILIZER TRIM AS REQUIRED. REMOVE GAP SEAL AND REAR SPAR SLIDING SEAL TO INSPECT PIVOT FITTINGS.

3102S 311BL emp

ITEMS

MPD MPD MRB MRB

MPD MPD MRB MRB

MPD MRB

MPD MRB

55-080-01 55-080-02 MSI 55-080-01 MSI 55-080-02 T: 8 YRS I: 4 YRS

E2 HHI 737-700

1 03-jun-04

T: 8 YRS I: 4 YRS

E2 HHI 737-700

1 03-jun-04

T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS

E2 HHI 737-700

1 03-jun-04

T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS

E2 HHI 737-700

1 03-jun-04

55-120-01 55-120-02 MSI 55-120-01 MSI 55-120-02

55-010-00 MSI 55-010-00

55-020-00 MSI 55-020-00

ATA: 55 - 10

Page 1 of 3


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

551000 05000

GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT HORIZONTAL STABILIZER FROM FRONT SPAR TO REAR SPAR INCLUDING SPAR CHORDS, WEBS, TERMINAL FITTINGS, UPPER AND LOWER INSPAR SKINS. I N T E R N A L

Date: 23-jul-08

ZONE ACCESS 332 emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp 342 emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp

STRUCTURE

331B 331BZ 331CZ 331DZ 332AB 332AT 332BB 332CB 332DB 332EB 332FB 332GB 332HB 332JB 332KB 332LB 332MB 332NB 335A 341B 341BZ 341CZ 341DZ 342AB 342AT 342BB 342CB 342DB 342EB 342FB 342GB 342HB 342JB 342KB 342LB 342MB 342NB 345A

ITEMS

REFERENCES MPD MPD MRB MRB

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

55-100-01 55-100-02 MSI 55-100-01 MSI 55-100-02 T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS

ATA: 55 - 10

E2 HHI 737-700

1 03-jun-04

Page 2 of 3


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

551000 06000

GENERAL VISUAL INSPECTION OF THE L/H AND R/H FORWARD SIDE OF FRONT SPAR, INCLUDING FRONT SPAR CHORDS AND WEBS, TERMINAL FITTINGS, AND CENTER SECTION FRONT SPAR LUGS. I N T E R N A L ACCESS BOLT REMOVAL IS REQUIRED TO INSPECT TERMINAL FITTINGS AND CENTER SECTION FRONT SPAR LUGS.

331 emp emp emp 341 emp emp emp

3311S 331A 331AZ 331B 3411S 341A 341AZ 341B

MPD MPD MRB MRB

GENERAL VISUAL INSPECTION OF THE AFT SIDE OF LEFT AND RIGHT HORIZONTAL STABILIZER REAR SPAR INCLUDING SPAR CHORDS, WEBS, TERMINAL FITTINGS, ELEVATOR TAB ACTUATOR SUPPORT FITTING, CENTER SECTION REAR SPAR LUGS, ELEVATOR HINGE RIBS AND ELEVATOR TAB LEADING EDGE. I N T E R N A L ACCESS DISCONNECT BALANCE PANELS IN BALANCE BAYS. BOLT REMOVAL IS REQUIRED TO INSPECT TERMINAL FITTINGS AND CENTER SECTION REAR SPAR LUGS, EXCEPT AT REAR SPAR UPPER LUGS AND CLEVIS. REMOVE TAB HINGE COVERS TO INSPECT ELEVATOR TAB LEADING EDGE.

333 emp emp emp emp emp emp emp emp emp emp emp emp emp emp 343 emp emp emp emp emp emp emp emp emp emp emp emp emp emp

3331S 333AB 333AT 333BB 333CB 333DB 333EB 333FB 334AB 334BB 334CB 334DB 334EB 334FB 335A 3431S 343AB 343AT 343BB 343CB 343DB 343EB 343FB 344AB 344BB 344CB 344DB 344EB 344FB 345A

MPD MPD MRB MRB

551000 07000

Date: 23-jul-08

ZONE ACCESS

STRUCTURE

ITEMS

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

55-070-01 55-070-02 MSI 55-070-01 MSI 55-070-02 T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS

E2 HHI 737-700

1 03-jun-04

T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS

E2 HHI 737-700

4 03-jun-04

55-110-01 55-110-02 MSI 55-110-01 MSI 55-110-02

ATA: 55 - 10

Page 3 of 3


HHI R E V

ITEM 55 - 20 552000 00000

552000 01000

R

737-6

MAINTENANCE SCHEDULE

552000 03000

R

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

ELEVATOR, HINGE SUPPORT AND BALANCE MECHANISM GENERAL VISUAL INSPECTION OF THE ELEVATOR AND ELEVATOR TAB SKIN PANELS, ELEVATOR SPARS, INSPAR RIBS, LEADING EDGE SKINS AND LEADING EDGE RIBS AND LEADING EDGE SPARS. I N T E R N A L

334 emp emp emp emp emp 344 emp emp emp emp emp emp

333AB 333BB 333EB 333FB 334AB 334PT 3001S 343BB 343CB 343DB 343EB 343FB 344PT

MPD MRB

DETAILED VISUAL INSPECTION OF THE LEFT AND RIGHT ELEVATOR TAB 334 MECHANISM SUPPORT FITTINGS ON ELEVATOR FRONT SPAR AND 344 ELEVATOR TAB SPAR AT LEADING EDGE CUTOUTS. I N T E R N A L ACCESS REMOVE UPPER OR LOWER HORIZONTAL STABILIZER TRAILING EDGE SEAL AND ELEVATOR INBOARD HINGE COVER PANEL TO INSPECT SUPPORT FITTINGS. REMOVE TAB HINGE COVERS TO LOCALLY INSPECT FORWARD FACE OF SPAR.

emp emp

MPD MPD MRB MRB

INSPECT DETAILED THE ELEVATOR HINGE FITTINGS, ELEVATOR 334 ACTUATOR FITTINGS, ELEVATOR BALANCE WEIGHT SUPPORT 344 STRUCTURE, ELEVATOR TAB MAST ARM FITTING AND ELEVATOR TAB HINGE FITTINGS. I N T E R N A L NOTE( ) ACCESS REMOVE LOWER TRAILING EDGE PANELS AND DISCONNECT BALANCE BAYS. REMOVE ELEVATOR HINGE COVER PLATES. ALTERNATIVE REMOVE ELEVATOR FROM HORIZONTAL STABILIZER. FOR ELEVATOR TAB MAST ARM FITTINGS, REMOVE FAIRING ON UPPER SURFACE OF ELEVATOR TO GAIN ACCESS.

emp emp

ITEMS

MPD MPD MRB MRB

55-130-00 MSI 55-130-00 T: 36000 CYC T: 12 YRS I: 10 YRS I: 30000 CYC

E2 HHI 737-700

4 03-jun-04

T: 12 YRS T: 36000 CYC I: 8 YRS I: 24000 CYC

E3 HHI 737-700

2 03-jun-04

T: 18000 CYC T: 8 YRS I: 18000 CYC I: 8 YRS

E3 HHI 737-700

5 23-jul-08

55-115-01 55-115-02 MSI 55-115-01 MSI 55-115-02

55-135-01 55-135-02 MSI 55-135-01 MSI 55-135-02

ATA: 55 - 20

Page 1 of 1


HHI R E V

ITEM 55 - 30

R

737-6

MAINTENANCE SCHEDULE

553000 00000

R

553000 01000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

VERTICAL STABILIZER GENERAL VISUAL INSPECTION OF THE VERTICAL FIN FROM FRONT SPAR TO REAR SPAR, INCLUDING SPAR CHORDS AND WEBS, INSPAR SKINS, LOWER CLOSURE RIB, AND REAR SPAR TERMINAL FITTINGS. I N T E R N A L ACCESS REMOVE UPPER REMOVABLE WEB. PIN REMOVAL IS NOT REQUIRED FOR TERMINAL FITTING INSPECTION.

323 emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp

322A 322AL 322AR 322B 322C 323AL 323AR 323BL 323BR 323CL 323CR 323DL 323EL 323FL 323GL 324AL 324AR 324BL 324BR 324DL 324DR 324JL 324KL 324LL 324ML 324NL S3232

MPD MRB MPD MRB

GENERAL VISUAL INSPECTION OF THE FORWARD SIDE OF THE VERTICAL FIN FRONT SPAR, INCLUDING FRONT SPAR CHORDS, WEBS, AND TERMINAL FITTINGS. I N T E R N A L

322 emp emp emp emp emp

322B 322C 323AL 323AR 323BL 323BR

MPD MRB

ITEMS

55-050-00 MSI 55-050-00 55-050-00 MSI 55-050-00 T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS

E2 HHI 737-700

3 23-jul-08

T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS

E2 HHI 737-700

1 03-jun-04

55-030-00 MSI 55-030-00

ATA: 55 - 30

Page 1 of 2


HHI

737-6

MAINTENANCE SCHEDULE

R E V

ITEM

DESCRIPTION

R

553000 02000

GENERAL VISUAL INSPECTION OF THE AFT SIDE OF VERTICAL FIN REAR SPAR,INCLUDING REAR SPAR CHORDS AND WEBS, AND RUDDER HINGE RIBS. I N T E R N A L

R

Date: 23-jul-08

ZONE ACCESS 324 emp emp emp emp emp emp emp

STRUCTURE

323CL 324BL 324DL 324GL 324KL 324LL 324ML 324NL

ITEMS

REFERENCES MPD MRB MPD MRB

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

55-060-00 MSI 55-060-00 55-060-00 MSI 55-060-00 T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS

ATA: 55 - 30

E2 HHI 737-700

3 23-jul-08

Page 2 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 55 - 40

554000 00000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

RUDDER GENERAL VISUAL INSPECTION OF THE RUDDER SKIN PANELS, SPARS, 325 INSPAR RIBS, LEADING EDGE SKINS AND LEADING EDGE RIBS AND LEADING EDGE SPARS. I N T E R N A L

3001S

MPD MRB

55-130-00 MSI 55-130-00 T: 36000 CYC T: 12 YRS I: 10 YRS I: 30000 CYC

ITEMS

ATA: 55 - 40

E2 HHI 737-700

4 03-jun-04

Page 1 of 1


HHI R E V

ITEM 56 56 - 11 561100 00000

561100 01000

R

561100 02000

R

N

737-6

MAINTENANCE SCHEDULE

561100 03000

N

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

WINDOWS FLIGHT COMPARTMENT WINDOWS LUBRICATE THE INSIDE RELEASE MECHANISMS FOR THE PILOTS AND CO-PILOTS #2 SLIDING WINDOWS. LUBRICATE THE OUTSIDE RELEASE MECHANISM FOR THE CO-PILOTS #2 SLIDING WINDOW.

211 212

emp emp

OPERATIONALLY CHECK THE INSIDE RELEASE MECHANISMS FOR THE 211 PILOTS AND CO-PILOTS #2 SLIDING WINDOWS. 212 OPERATIONALLY CHECK THE CO-PILOTS #2 SLIDING WINDOW FROM THE OUTSIDE.

emp emp

PERFORM A GENERAL VISUAL INSPECTION OF THE PILOTS AND 211 CO-PILOTS #2 SLIDING WINDOW SILL DRAIN FOR OBVIOUS DAMAGE, 212 CLOGGING, CONDITION AND SECURITY. I N T E R N A L NOTE( E ) APPLICABLE TO AIRPLANES LINE NUMBER 145 AND ON. APPLICABLE TO AIRPLANES LINE NUMBER 1 TO 144 INCORPORATING SB 737-56-1011.

emp emp

DO AN INTERNAL AND EXTERNAL DETAILED INSPECTION OF THE LEFT 211 SIDE AND RIGHT SIDE FLIGHT DECK WINDOWS NUMBER 2, 4 AND 5 FOR 212 CRACKING AND DAMAGE IN THE VINYL INTERLAYER AND GLASS PANES. NOTE( T ) THE INITIAL INSPECTION ON D-AHIB MUST BE DONE PRIOR TO JANUARY 3, 2009. THE INITIAL INSPECTION ON D-AHIC MUST BE DONE PRIOR TO JULY 3, 2009.

emp emp

ITEMS

MPD MRB

56-010-00 MSI 56-010-00 RTE:9

AMTOSS

12-25-81-60

MPD MRB

56-030-00 MSI 56-030-00 RTE:9

AMTOSS

56-12-11-71

MPD MRB

56-050-00 MSI 56-050-00 RTE:9

AMTOSS

56-12-11-20

AAR AAR EO SB

AD 2008-11-08 LTA D-2008-235 160169 737-56A1022

I: 2 YRS

S

HHI 737-700

2 03-jun-04

I: 2 YRS

F1 HHI 737-700

2 03-jun-04

I: 2 YRS

E2 HHI 737-700

4 23-jul-08

T: 1 s.N I: 6000 FLH I: 24 MTH

E3 HHI 737-700

0 23-jul-08

ATA: 56 - 11

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 57 57 - 10

571000 00000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

WINGS INTERSPAR WING GENERAL VISUAL INSPECTION OF THE OUTBOARD WING FRONT SPAR. INSPECT LEFT AND RIGHT FRONT SPAR CHORDS, WEBS AND STIFFENERS, INCLUDING AT SIDE OF BODY JOINT AND AT NACELLE FITTING ATTACHMENT. I N T E R N A L ACCESS EXTEND KRUEGER FLAPS. ACCESS PANEL: 521AAB, 521ABB, 621AAB

511 emp 521 emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp 611 emp 621 emp emp emp emp emp emp emp

511AT 511BT 521AB 521BB 521CB 521DB 521EB 521FB 521GB 521HB 521JB 521KB 521LB 521MB 521NB 521PB 521QB 521RB 521SB 521TB 521UB 521VB 521WB 521XB 521YB 521ZB 611AT 611BT 621AB 621AT 621BB 621CB 621DB 621EB 621FB 621GB

ITEMS

MPD MPD MRB MRB

57-120-01 57-120-02 MSI 57-120-01 MSI 57-120-02 I: 18000 CYC I: 6 YRS

ATA: 57 - 10

E2 HHI 737-700

2 25-apr-06

Page 1 of 5


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

571000 01000

571000 02000

Date: 23-jul-08

DESCRIPTION

GENERAL VISUAL INSPECTION OF THE L/H AND R/H AFT SIDE OF REAR SPAR (CHORDS, WEBS AND STIFFENERS), INCLUDING FLAP 1&2 AND 7&8 SUPPORT FITTINGS. I N T E R N A L

GENERAL VISUAL INSPECTION OF THE L/H AND R/H WING AFT SIDE OF REAR SPAR (CHORDS, WEBS AND STIFFENERS), INCLUDING AT MAIN LANDING GEAR OUTBOARD SUPPORT ATTACHMENT, AND AT TRUNNION ATTACHMENT. I N T E R N A L

ZONE ACCESS

STRUCTURE

REFERENCES

emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp

621HB 621JB 621KB 621LB 621MB 621NB 621PB 621QB 621RB 621SB 621TB 621UB 621VB 621WB 621XB 621YB 621ZB

561 571 emp emp emp emp 661 emp emp emp emp 671

emp 561AB 561BB 561CB 571CB 571DB 661AB 661BB 661CB 671CB 671DB emp

MPD MPD MRB MRB

551 emp emp 651 emp emp

551BT 551CT 551EB 651BT 651CT 651EB

MPD MPD MRB MRB

ITEMS

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

57-310-01 57-310-02 MSI 57-310-01 MSI 57-310-02 I: 18000 CYC I: 6 YRS

E2 HHI 737-700

2 25-apr-06

I: 18000 CYC I: 6 YRS

E2 HHI 737-700

2 25-apr-06

57-260-01 57-260-02 MSI 57-260-01 MSI 57-260-02

ATA: 57 - 10

Page 2 of 5


HHI

737-6

MAINTENANCE SCHEDULE

R E V

ITEM

DESCRIPTION

R

571000 03000

GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT OUTBOARD WING FROM SIDE OF BODY RIB TO RIB 5: 1.SIDE OF BODY RIB (INCLUDING WEBS AND STIFFENERS, UPPER RIB CHORD, LOWER TEE CHORD, SPLICE FITTINGS, TERMINAL FITTINGS AT FRONT AND REAR SPARS); 2.UPPER AND LOWER SURFACES (INCLUDING SKINS; TYPICAL SPLICE, VENT AND RAIL STRINGERS; AT DRAIN INSTALLATION; AT ATTACHMENTS TO FRONT AND REAR SPARS; AT ATTACHMENTS TO SHEAR TIED RIBS AND SUPPORT FITTINGS); 3.FRONT AND REAR SPAR CHORDS, WEBS, STIFFENERS AND RIB POSTS; 4.SHEAR TIED AND NON-SHEAR TIED RIBS. I N T E R N A L

R

Date: 23-jul-08

ZONE ACCESS 531 emp 631 emp

STRUCTURE

531AB 531BB 631AB 631BB

REFERENCES MPD MPD MRB MRB

THRESHOLD INTERVAL

EFF

R L ITEM BY E E REVISION P V DATE

57-170-01 57-170-02 MSI 57-170-01 MSI 57-170-02 I: 36000 CYC I: 10 YRS

ITEMS

TSK

ATA: 57 - 10

E2 HHI 737-700

2 23-jul-08

Page 3 of 5


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

571000 04000

Date: 23-jul-08

DESCRIPTION GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT OUTBOARD WING FROM RIB5 TO RIB 22: 1.UPPER AND LOWER SURFACES (INCLUDING SKINS; TYPICAL SPLICE, VENT AND RAIL STRINGERS; AT ATTACHMENTS TO FRONT AND REAR SPARS; AT ATTACHMENTS TO SHEAR TIED RIBS AND SUPPORT FITTINGS; AT ATTACHMENT TO NACELLE FITTINGS; AT DRAIN INSTALLATIONS); 2.FRONT SPAR CHORDS, WEBS, STIFFENERS AND RIB POSTS, INCLUDING AT NACELLE FITTING ATTACHMENTS; 3.REAR SPAR CHORDS, WEBS, STIFFENERS AND RIB POSTS, FLAP TRACK SUPPORT FITTINGS, INCLUDING REAR SPAR AT MAJOR FITTING ATTACHMENTS; 4.SHEAR TIED AND NON-SHEAR TIED RIBS (INCLUDING RIB 6 STRUCTURAL DOORS, RIBS 6 AND 7 AT NACELLE SUPPORT FITTINGS, RIBS 10 AND 14 AT FLAP TRACK SUPPORT FITTINGS); 5.NACELLE SUPPORT FITTINGS (R2 BACKUP LINK, R4 BACK UP LINK, R7/8 BACKUP FITTING). I N T E R N A L ACCESS DO NOT REMOVE THE 532AZ AND THE 532BZ ACCESS DOORS AT THE SAME TIME.

ZONE ACCESS 532 emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp 632 emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp

STRUCTURE

5321S 532AB 532AZ 532BB 532BZ 532CB 532DB 532EB 532FB 532GB 532HB 532JB 532KB 532LB 532MB 532NB 532PB 532QB 532RB 6321S 632AB 632AZ 632BB 632BZ 632CB 632DB 632EB 632FB 632GB 632HB 632JB 632KB 632LB 632MB 632NB 632PB 632QB 632RB

ITEMS

REFERENCES MPD MPD MRB MRB

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

57-180-01 57-180-02 MSI 57-180-01 MSI 57-180-02 I: 36000 CYC I: 10 YRS

ATA: 57 - 10

E2 HHI 737-700

1 03-jun-04

Page 4 of 5


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

571000 05000

GENERAL VISUAL INPECTION OF THE LEFT AND RIGHT OUTBOARD WING SURGE TANK AND DRY BAY (FROM RIB 22 TO RIB 27), INCLUDING UPPER AND LOWER SKINS, STRINGERS, FRONT AND REAR SPARS, RIB POSTS "WBL 656.17 CLOSURE RIB (LN 778 AND ON)", SHEAR TIED AND NON-SHEAR TIED RIBS, AND ACCESS HOLES. I N T E R N A L

Date: 23-jul-08

ZONE ACCESS 533 emp emp 534 emp 633 emp emp 634 emp

STRUCTURE

533AB 533BB 533CB 534AB 534BB 633AB 633BB 633CB 634AB 634BB

ITEMS

REFERENCES MPD MPD MRB MRB

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

57-190-01 57-190-02 MSI 57-190-01 MSI 57-190-02 I: 36000 CYC I: 10 YRS

ATA: 57 - 10

E2 HHI 737-700

2 03-jun-04

Page 5 of 5


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 57 - 12

571200 00000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

FRONT AND REAR SPAR GENERAL VISUAL INSPECTION OF THE WING CENTER SECTION AFT SIDE OF REAR SPAR, INCLUDING KEEL BEAM STIFFENERS AT BL 6.2., AND SIDE OF BODY REAR SPAR TERMINAL FITTING. E X T E R N A L

133 134 192 emp emp emp emp emp

emp 1007S 192BL 192BR 192CL 192CR 192E 192F

ITEMS

MPD MRB

57-030-00 MSI 57-030-00 T: 9 YRS I: 3 YRS

ATA: 57 - 12

E2 HHI 737-700

1 03-jun-04

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 57 - 14

571400 00000

571400 01000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

CENTER WING BOX GENERAL VISUAL INSPECTION OF THE LOWER SIDE OF LOWER SURFACE OF WING CENTER SECTION: 1.SKINS, TYPICAL STRINGERS, SPLICE STRINGERS, FRONT AND REAR SPAR LOWER CHORDS; 2.SIDE OF BODY LOWER TEE CHORD AND SPLICE PLATES; 3.LOWER BEAMS AT BL 41; 4.AT ATTACHMENTS TO KEEL BEAM, TO LOWER BEAMS AT BL 41, TO FUSELAGE DRAG ANGLES; AT DRAIN INSTALLATION AND ACCESS HOLES. I N T E R N A L ACCESS REMOVE ECS HEAT EXCHANGER ACCESS PANEL.

131 132 192 emp emp emp emp emp emp emp emp emp emp

emp emp 1008S 192AL 192AR 192BL 192BR 192CL 192CR 192E 192F 192HL 192HR

MPD MRB

GENERAL VISUAL INSPECTION OF THE WING CENTER SECTION FORWARD SIDE OF FRONT SPAR, INCLUDING SIDE OF BODY/TERMINAL FITTING ATTACHMENTS. I N T E R N A L

125 emp 126 192 emp emp emp emp emp emp emp

121EW 121HW 122GW 191FL 191FR 192AL 192AR 192BL 192BR 192HL 192HR

MPD MRB

57-050-00 MSI 57-050-00

AMM AMM

51-05-01-210 57-05-03-210

ITEMS

57-040-00 MSI 57-040-00 I: 6 YRS I: 18000 CYC

E2 HHI 737-700

2 25-apr-06

I: 18000 CYC I: 6 YRS

E2 HHI 737-700

3 05-sep-06

ATA: 57 - 14

Page 1 of 4


HHI

737-6

MAINTENANCE SCHEDULE

R E V

ITEM

DESCRIPTION

R

571400 02000

GENERAL VISUAL INSPECTION OF THE FORWARD SIDE OF WING CENTER SECTION FRONT SPAR, INCLUDING THE SIDE OF BODY/TERMINAL FITTING. I N T E R N A L ACCESS REMOVE AFT PANELS IN FORWARD CARGO COMPARTMENT.

125 126 191 emp emp emp emp emp emp 195 emp 196 emp

emp S1006 191AL 191AR 191CL 191CR 191D 191FL 191FR 195AL 195AR 196AL 196AR

MPD MRB

GENERAL VISUAL INSPECTION OF THE INSIDE WING CENTER SECTION: 1.UPPER SURFACE (INCLUDING SKINS, TYPICAL AND VENT STRINGERS, SPLICE STRINGER, AT ATTACHMENT TO FLOOR BEAMS); 2.LOWER SURFACE (INCLUDING SKINS, TYPICAL STRINGERS, SPLICE STRINGERS, AT ATTACHMENT TO KEEL BEAM, AT DRAIN INSTALLATION, AT ACCESS HOLE, AT ATTACHMENT TO FUSELAGE DRAG ANGLE, AT ATTACHMENT TO LOWER BEAM AT BL 41); 3.FRONT AND REAR SPARS (INCLUDING WEBS AND STIFFENERS, UPPER AND LOWER SPAR CHORDS, ATTACHMENTS TO SKIN); 4.SIDE OF BODY RIB (INCLUDING WEBS AND STIFFENERS, UPPER RIB CHORD, LOWER TEE CHORD, FRONT AND REAR SPAR TERMINAL FITTINGS, SPLICE FITTINGS); 5.SPANWISE BEAMS. I N T E R N A L

131 emp 132 emp emp emp 231 232

131AB S1303 192CL 192CR 192E 192F emp emp

MPD MRB

57-020-00 MSI 57-020-00

AMM AMM

51-05-01-210 57-05-03-210

R

571400 03000

Date: 23-jul-08

ZONE ACCESS

STRUCTURE

ITEMS

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

57-010-00 MSI 57-010-00 I: 10 YRS I: 36000 CYC

E2 HHI 737-700

2 23-jul-08

I: 36000 CYC I: 10 YRS

E2 HHI 737-700

3 05-sep-06

ATA: 57 - 14

Page 2 of 4


HHI

737-6

MAINTENANCE SCHEDULE

R E V

ITEM

DESCRIPTION

R

571400 04000

DETAILED INSPECTION OF LOWER WING PANEL, RAIL STRINGERS; INTERNAL SURFACE OF STRINGERS 6 & 8, ALL LOCATIONS AT EXTERNAL FAIRINGS/FITTINGS WHERE STRINGER IS VISIBLE IN VICINITY OF RIBS 6, 7, 10, & 14. (PSE 57-20-02) I N T E R N A L NOTE( I ) SEE MPD SECTION 9, FIGURE 1, FLIGHT LENGTH SENSITIVE (FLS) TO DETERMINE THRESHOLD INTERVAL. FOR REPEAT INTERVAL AND SAMPLING SEE DTR 57-20-02.

532 emp emp emp emp emp 632 emp emp emp emp emp

532AB 532BB 532DB 532EB 532HB 532JB 632AB 632BB 632DB 632EB 632HB 632JB

MPD MRB

57-616-00 MSI 57-616-00

AMM

57-05-02-200

DETAILED INSPECTION OF LOWER WING PANEL, SPLICE STRINGERS; STRINGERS 5 & 9, ALL LOCATIONS AT EXTERNAL FAIRINGS/FITTINGS WHERE STRINGER IS VISIBLE IN VICINITY OF RIBS 6, 7, 10, & 14. (PSE57-20-03) I N T E R N A L NOTE( I ) SEE MPD SECTION 9, FIGURE 1, FLIGHT LENGTH SENSITIVE (FLS) TO DETERMINE THRESHOLD INTERVAL. FOR REPEAT INTERVAL AND SAMPLING SEE DTR 57-20-03.

434 444 532 emp emp emp emp emp 543 544 632 emp emp emp emp emp 643 644

emp emp 532AB 532BB 532DB 532EB 532HB 532JB emp emp 632AB 632BB 632DB 632EB 632HB 632JB emp emp

MPD MRB

57-618-00 MSI 57-618-00

AMM

57-05-02-200

R

R

571400 05000

R

Date: 23-jul-08

ZONE ACCESS

STRUCTURE

ITEMS

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

T: 40000 CYC T: 88000 FLH I: 1 s.N I: 36000 CYC

E3 HHI 737-700

1 23-jul-08

T: 30000 CYC T: 64000 FLH I: 1 s.N I: 36000 CYC

E3 HHI 737-700

1 23-jul-08

ATA: 57 - 14

Page 3 of 4


HHI

737-6

MAINTENANCE SCHEDULE

R E V

ITEM

DESCRIPTION

R

571400 05500

SPECIAL DETAILED INSPECTION OF LOWER WING PANEL, SPLICE STRINGERS; INSPECT (HIGH FREQUENCY EDDY CURRENT) THE INTERNAL SURFACE OF STRINGERS 5 & 9, ALL LOCATIONS AT EXTERNAL FAIRINGS/FITTINGS WHERE STRINGER IS VISIBLE IN VICINITY OF RIBS 6, 7, 10, & 14. (PSE57-20-03) I N T E R N A L NOTE( I ) SEE MPD SECTION 9, FIGURE 1, FLIGHT LENGTH SENSITIVE (FLS) TO DETERMINE THRESHOLD INTERVAL. FOR REPEAT INTERVAL AND SAMPLING SEE DTR 57-20-03.

434 444 532 emp emp emp emp emp 543 544 632 emp emp emp emp emp 643 644

emp emp 532AB 532BB 532DB 532EB 532HB 532JB emp emp 632AB 632BB 632DB 632EB 632HB 632JB emp emp

MPD MRB

57-618-01 MSI 57-618-01

AMM

57-05-02-200

SPECIAL DETAILED INSPECTION OF LOWER WING PANEL, UNDER THE NACELLE FITTING; INSPECT (ULTRASONIC) THE SKIN PANEL UNDER R2, R3 AND R4 NACELLE FITTINGS BETWEEN THE FRONT SPAR CHORD AND SPLICE STRINGER 5. (PSE 57-20-09) I N T E R N A L NOTE( I ) SEE MPD SECTION 9, FIGURE 1, FLIGHT LENGTH SENSITIVE (FLS) TO DETERMINE THRESHOLD INTERVAL. FOR REPEAT INTERVAL AND SAMPLING SEE DTR 57-20-09.

434 emp emp 444 emp emp 532 632

434AL 434AR 434BL 444AL 444AR 444BL emp emp

MPD MRB

57-643-00 MSI 57-643-00

AMM

57-05-02-200

R

R

571400 07000

R

Date: 23-jul-08

ZONE ACCESS

STRUCTURE

ITEMS

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

T: 40000 CYC T: 88000 FLH I: 1 s.N I: 36000 CYC

E4 HHI 737-700

1 23-jul-08

T: 40000 CYC T: 88000 FLH I: 18000 CYC I: 1 s.N

E4 HHI 737-700

1 23-jul-08

ATA: 57 - 14

Page 4 of 4


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 57 - 15

571500 00000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

MAIN LANDING GEAR TRUNNION SUPPORT BEAM GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT MAIN LANDING GEAR SUPPORT STRUCTURE: 1.MAIN LANDING GEAR BEAM ASSEMBLY; 2.OUTBOARD SUPPORT (DOG HOUSE) ASSEMBLY; 3.INBOARD SUPPORT (HANGER LINK) ASSEMBLY; 4.TRUNNION SUPPORT ASSEMBLY; 5.STABILIZER LINKS, INCLUDING ATTACH FITTINGS AND FUSE PINS. I N T E R N A L

551 emp 651 emp

551DT 551ET 651DT 651ET

MPD MPD MRB MRB

57-250-01 57-250-02 MSI 57-250-01 MSI 57-250-02 I: 18000 CYC I: 6 YRS

ITEMS

ATA: 57 - 15

E2 HHI 737-700

2 25-apr-06

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 57 - 21

572100 00000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

LEADING EDGE GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT WING LEADING EDGE CAVITY, INCLUDING FLAPS AND SLATS. I N T E R N A L ACCESS EXTEND KRUEGER FLAPS AND SLATS. ACCESS PANEL: 521AAB , 521ABB, 621AAB

511 512 513 521 emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp 522 523 524 525 611 612 613 621 emp emp

emp emp emp 521AB 521BB 521CB 521DB 521EB 521FB 521GB 521HB 521JB 521KB 521LB 521MB 521NB 521PB 521QB 521RB 521SB 521TB 521UB 521VB 521WB 521XB 521YB 521ZB emp emp emp emp emp emp emp 621AB 621BB 621CB

ITEMS

MPD MPD MRB MRB

57-130-01 57-130-02 MSI 57-130-01 MSI 57-130-02 I: 10 YRS

ATA: 57 - 21

E2 HHI 737-700

1 03-jun-04

Page 1 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

ZONE ACCESS emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp 622 623 624 625

Date: 23-jul-08

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

621DB 621EB 621FB 621GB 621HB 621JB 621KB 621LB 621MB 621NB 621PB 621QB 621RB 621SB 621TB 621UB 621VB 621WB 621XB 621YB 621ZB emp emp emp emp

ITEMS

ATA: 57 - 21

Page 2 of 2


HHI R E V

ITEM 57 - 22

R

737-6

MAINTENANCE SCHEDULE

572200 00000

R

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

TRAILING EDGE GENERAL VISUAL INSPECTION OF THE INTERIOR OF LEFT AND RIGHT WING TRAILING EDGE CAVITY, INCLUDING SKINS, RIBS, AILERONS AND SPOILERS. I N T E R N A L ACCESS FLAP EXTENSION REQUIRED FOR INSPECTION.

551 emp emp emp emp emp emp 552 553 561 emp emp 562 563 564 565 566 567 571 emp emp emp emp emp 572 emp emp emp emp emp emp emp emp emp emp emp emp

551AB 551BB 551CB 551DB 551EB 551FB 551GB emp emp 561AB 561BB 561CB emp emp emp emp emp emp 571AB 571BB 571CB 571DB 571EB 571FB 572AB 572BB 572CB 572CT 572DB 572DT 572EB 572FB 572FT 572GB 572GT 572HB S5001

ITEMS

MPD MPD MRB MRB

57-270-01 57-270-02 MSI 57-270-01 MSI 57-270-02 T: 10 YRS I: 5 YRS

ATA: 57 - 22

E2 HHI 737-700

3 23-jul-08

Page 1 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

ZONE ACCESS 651 emp emp emp emp emp emp 652 653 661 emp emp 662 663 664 665 666 667 671 emp emp emp emp emp 672 emp emp emp emp emp emp emp emp emp emp emp emp

Date: 23-jul-08

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

651AB 651BB 651CB 651DB 651EB 651FB 651GB emp 653AT 661AB 661BB 661CB emp emp emp emp emp emp 671AB 671BB 671CB 671DB 671EB 671FB 672AB 672BB 672CB 672CT 672DB 672DT 672EB 672FB 672FT 672GB 672GT 672HB S6002

ITEMS

ATA: 57 - 22

Page 2 of 2


HHI R E V

ITEM 57 - 31

R

737-6

MAINTENANCE SCHEDULE

573100 00000

DESCRIPTION

Date: 23-jul-08

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

WING UPPER SURFACE GENERAL VISUAL INSPECTION OF THE UPPER SIDE OF LEFT AND RIGHT OUTBOARD WING UPPER SURFACE (UNDER SIDE-OF-BODY FAIRING), INCLUDING: 1.WING UPPER SURFACE AT SIDE-OF-BODY SPLICE, INCLUDING UPPER RIB CHORD; 2.WING UPPER SURFACE AT ATTACHMENT LOCATIONS. I N T E R N A L

R

573100 02000

ZONE ACCESS

GENERAL VISUAL INSPECTION OF THE UPPER SIDE OF UPPER WING SURFACE: 1.UPPER PANEL, INCLUDING AT ATTACHMENTS, FRONT AND REAR SPAR UPPER CHORDS, AND SIDE OF BODY UPPER RIB CHORD; 2.FLOOR BEAMS FROM STA 540 TO STA 727, INCLUDING AT FLOOR BEAM ATTACHMENTS; 3.INSPECT FOR CONDITION OF SECONDARY VAPOR BARRIER. I N T E R N A L ACCESS REMOVE FLOOR PANELS AND INSULATION AS REQUIRED IN PASSENGER COMPARTMENT AS REQUIRED FOR ACCESS.

195 emp emp emp emp emp emp 196 emp emp emp emp emp emp 511 531 551 611 631 651

191AR 195AL 195AR 195BL 195BR 195CL 195CR 191AL 196AL 196AR 196BL 196BR 196CL 196CR emp emp emp emp emp emp

MPD MPD MRB MRB MPD MPD MRB

135 136 231 232

emp emp emp emp

MPD MRB

ITEMS

57-070-01 57-070-02 MSI 57-070-01 MSI 57-070-02 57-070-01 57-070-02 MSI 57-070-01 I: 6 YRS I: 18000 CYC

E2 HHI 737-700

3 23-jul-08

I: 36000 CYC I: 10 YRS

E2 HHI 737-700

2 25-apr-06

57-090-00 MSI 57-090-00

ATA: 57 - 31

Page 1 of 1


HHI R E V

ITEM 57 - 32

R

737-6

MAINTENANCE SCHEDULE

573200 01000

DESCRIPTION

Date: 23-jul-08

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

WING LOWER SURFACE GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT WING LOWER SURFACE UNDER STRUT FAIRING, INCLUDING ALL ATTACHMENT LOCATIONS. I N T E R N A L

R

573200 02000

ZONE ACCESS

GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT OUTBOARD WING LOWER SURFACE (UNDER LOWER SIDE OF BODY FAIRING), INCLUDING ATTACHMENT LOCATIONS. I N T E R N A L

434 emp emp 444 emp emp 531 532 631 632

434AL 434AR 434BL 444AL 444AR 444BR emp emp emp emp

MPD MPD MRB MRB

192 emp emp emp emp emp emp emp emp emp emp emp emp emp 511 531 551 611 631 651

191AL 191AR 191FL 191FR 192AL 192AR 192BL 192BR 192HL 192HR 193AL 193AR 193CL 193CR emp emp emp emp emp emp

MPD MPD MRB MRB

ITEMS

57-110-01 57-110-02 MSI 57-110-01 MSI 57-110-02 I: 9000 CYC I: 30 MTH I: 36 MTH

E2 HHI 737-700

3 23-jul-08

I: 18000 CYC I: 6 YRS

E2 HHI 737-700

2 25-apr-06

57-060-01 57-060-02 MSI 57-060-01 MSI 57-060-02

ATA: 57 - 32

Page 1 of 3


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

573200 03000

GENERAL VISUAL INSPECTION OF THE FUEL ACCESS HOLES IN LEFT AND RIGHT OUTBOARD WING LOWER SURFACE. ( TANK ENTRY IS NOT REQUIRED.) I N T E R N A L

Date: 23-jul-08

ZONE ACCESS 531 emp 532 emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp 533 emp emp 534 emp 631 emp 632 emp emp emp emp emp emp emp emp emp emp emp emp emp

STRUCTURE

531AB 531BB 532AB 532BB 532CB 532DB 532EB 532FB 532GB 532HB 532JB 532KB 532LB 532MB 532NB 532PB 532QB 532RB 533AB 533BB 533CB 534AB 534BB 631AB 631BB 632AB 632BB 632CB 632DB 632EB 632FB 632GB 632HB 632JB 632KB 632LB 632MB 632NB 632PB

ITEMS

REFERENCES MPD MPD MRB MRB

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

57-160-01 57-160-02 MSI 57-160-01 MSI 57-160-02 I: 18000 CYC I: 6 YRS

ATA: 57 - 32

E2 HHI 737-700

2 25-apr-06

Page 2 of 3


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

573200 04000

573200 05000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS emp emp 633 emp emp 634 emp

632QB 632RB 633AB 633BB 633CB 634AB 634BB

GENERAL VISUAL INSPECTION OF THE L/H AND R/H LOWER SIDE OF 542 LOWER SURFACE (UNDER FLAP SUPPORT NO.3 AND NO. 6 642 FAIRING),INCLUDING ALL ATTACHMENT LOCATIONS AND ACCESS HOLES. I N T E R N A L ACCESS EXTEND FLAPS

542AB 642AB

GENERAL VISUAL INSPECTION OF THE L/H AND R/H LOWER SIDE OF LOWER SURFACE (UNDER FLAP SUPPORT NO.1&2 AND 7&8 FAIRINGS), INCLUDING ALL ATTACHMENT LOCATIONS AND ACCESS HOLES. I N T E R N A L ACCESS EXTEND FLAPS

543AB 544AB 643AB 644AB

543 544 643 644

STRUCTURE

ITEMS

REFERENCES

MPD MPD MRB MRB

MPD MPD MRB MRB

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

57-220-01 57-220-02 MSI 57-220-01 MSI 57-220-02 I: 18000 CYC I: 6 YRS

E2 HHI 737-700

2 25-apr-06

I: 18000 CYC I: 6 YRS

E2 HHI 737-700

2 25-apr-06

57-240-01 57-240-02 MSI 57-240-01 MSI 57-240-02

ATA: 57 - 32

Page 3 of 3


HHI R E V

ITEM 57 - 35

R

737-6

MAINTENANCE SCHEDULE

573500 00000

R

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

WING FITTINGS GENERAL VISUAL INSPECTION OF THE FOLLOWING FITTINGS L/H AND R/H: 1. FRONT SPAR PITCH LOAD FITTING (R1); 2. AFT DRAG LOAD FITTING (R2); 3.OUTBOARD SIDE LOAD FITTING (R3); 4.INBOARD SIDE LOAD FITTING (R4); 5.SIDE BRACE SUPPORT FITTINGS (R7 AND R8); 6.R3 FORWARD BACKUP FITTING. INSPECT UPPER WING SKIN AT ATTACHMENT TO NACELLE FITTING R1. I N T E R N A L ACCESS REMOVE UPPER WING JUNCTION FAIRING AND AFT STRUT FAIRING PANEL.

431 emp emp emp emp 434 441 emp 444 emp emp emp

431CL 431CR 434AL 434AR 434BL emp 441CL 441CR 444AL 444AR 444BL 444BR

ITEMS

MPD MPD MRB MRB

57-100-01 57-100-02 MSI 57-100-01 MSI 57-100-02 I: 9000 CYC I: 30 MTH I: 36 MTH

ATA: 57 - 35

E2 HHI 737-700

3 23-jul-08

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 57 - 52

575200 00000

575200 01000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

TRAILING EDGE FLAPS GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT OUTBOARD FLAP INBOARD AND OUTBOARD TRACK ASSEMBLY, CARRIAGE ASSEMBLY, FORWARD FITTING ASSEMBLY,AND AFT LINKS. NORMAL OVERHAUL PROCEDURES, APPLIED WITH THE FLAP TRACK ASSEMBLIES, CARRIAGE ASSEMBLIES AND FORWARD FITTING ASSEMBLIES REMOVED, AT INTERVALS NOT EXCEEDING 10 YEARS, ARE ADEQUATE TO MAINTAIN CORROSION AT SAFE LEVELS ON THESE COMPONENTS. THEREFORE APPLICATION OF THE BASIC TASKS AND REPORTING ARE NOT REQUIRED ON THESE COMPONENTS I N T E R N A L ACCESS REMOVE FLAP FORWARD FAIRINGS AND DEPLOY FLAPS.

543 544 643 644

GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT INBOARD FLAP 542 OUTBOARD TRACK ASSEMBLY, CARRIAGE ASSEMBLY, FORWARD FITTING 642 ASSEMBLY,AND AFT ATTACH FITTING. NORMAL OVERHAUL PROCEDURES, APPLIED WITH THE FLAP TRACK ASSEMBLIES, CARRIAGE ASSEMBLIES AND FORWARD FITTING ASSEMBLIES REMOVED, AT INTERVALS NOT EXCEEDING 10 YEARS, ARE ADEQUATE TO MAINTAIN CORROSION AT SAFE LEVELS ON THESE COMPONENTS. THEREFORE APPLICATION OF THE BASIC TASKS AND REPORTING ARE NOT REQUIRED ON THESE COMPONENTS I N T E R N A L ACCESS REMOVE FLAP SUPPORT FORWARD FAIRING AND DEPLOY FLAPS.

543AB 544AB 643AB 644AB

542AB 642AB

ITEMS

MPD MPD MRB MRB

MPD MPD MRB MRB

57-230-01 57-230-02 MSI 57-230-01 MSI 57-230-02 I: 18000 CYC I: 6 YRS

E2 HHI 737-700

2 25-apr-06

I: 18000 CYC I: 6 YRS

E2 HHI 737-700

2 25-apr-06

57-210-01 57-210-02 MSI 57-210-01 MSI 57-210-02

ATA: 57 - 52

Page 1 of 3


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

575200 02000

GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT INBOARD FLAP INBOARD TRACK ASSEMBLY, CARRIAGE ASSEMBLY, FORWARD FITTING ASSEMBLY, AFT LINK AND AFT LINK PINS. NORMAL OVERHAUL PROCEDURES, APPLIED WITH THE FLAP TRACK ASSEMBLIES, CARRIAGE ASSEMBLIES AND FORWARD FITTING ASSEMBLIES REMOVED, AT INTERVALS NOT EXCEEDING 10 YEARS, ARE ADEQUATE TO MAINTAIN CORROSION AT SAFE LEVELS ON THESE COMPONENTS. THEREFORE APPLICATION OF THE BASIC TASKS AND REPORTING ARE NOT REQUIRED ON THESE COMPONENTS I N T E R N A L ACCESS TO INBOARD SIDE OF TRACK ASSEMBLY THROUGH THE MLG WHEEL WELL.

541 emp emp emp emp 641

193CL 193CR 194BL 194CL 194CR 194BR

MPD MPD MRB MRB

GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT INBOARD FLAP INTERNALLY: 1.FRONT SPAR (AFT SIDE), REAR SPAR (FORWARD SIDE), INSPAR RIBS, TORQUE TUBE, TORQUE TUBE RIBS; 2.AFT FLAP TRACK SUPPORT ASSEMBLY ATTACHMENT ON MAIN FLAP REAR SPAR. I N T E R N A L

553 emp emp emp emp 653 emp emp emp emp

553AT 553BB 553CT 553DT 553ET 653AT 653BB 653CT 653DT 653ET

MPD MPD MRB MRB

575200 06000

Date: 23-jul-08

ZONE ACCESS

STRUCTURE

ITEMS

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

57-200-01 57-200-02 MSI 57-200-01 MSI 57-200-02 I: 18000 CYC I: 6 YRS

E2 HHI 737-700

3 25-apr-06

I: 36000 CYC I: 10 YRS

E2 HHI 737-700

1 03-jun-04

57-300-01 57-300-02 MSI 57-300-01 MSI 57-300-02

ATA: 57 - 52

Page 2 of 3


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

575200 07000

GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT OUTBOARD FLAP INTERNALLY: 1.FRONT SPAR (AFT SIDE), INCLUDING SUPPORT FITTINGS AT WBL 254 AND 358; 2.REAR SPAR (FORWARD SIDE); 3.INSPAR RIBS AND AFT FLAP TRACK SUPPORT RIBS. I N T E R N A L ACCESS DEPLOY AFT FLAP SO THAT AFT FLAP TRACKS DO NOT BLOCK VIEW OF REAR SPAR LOWER CHORD.

Date: 23-jul-08

ZONE ACCESS 567 emp emp emp emp emp emp emp 667 emp emp emp emp emp emp emp

STRUCTURE

567AT 567BT 567CT 567DT 567ET 567FT 567GT 567HT 667AT 667BT 667CT 667DT 667ET 667FT 667GT 667HT

ITEMS

REFERENCES MPD MPD MRB MRB

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

57-330-01 57-330-02 MSI 57-330-01 MSI 57-330-02 I: 36000 CYC I: 10 YRS

ATA: 57 - 52

E2 HHI 737-700

1 03-jun-04

Page 3 of 3


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 57 - 54

575400 00000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

SLATS DETAILED VISUAL INSPECTION OF THE LEFT AND RIGHT WING SLAT TRACKS. I N T E R N A L ACCESS EXTEND SLATS.

522 emp emp emp emp emp emp emp 523 524 525 622 emp emp emp emp emp emp emp 623 624 625

521CB 521FB 521JB 521MB 521QB 521TB 521WB 521ZB emp emp emp 621CB 621FB 621JB 621MB 621QB 621TB 621WB 621ZB emp emp emp

ITEMS

MPD MPD MRB MRB

57-140-01 57-140-02 MSI 57-140-01 MSI 57-140-02 I: 6 YRS

ATA: 57 - 54

E3 HHI 737-700

2 25-apr-06

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 57 - 55

575500 00000

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

SPOILER GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT INBOARD GROUND SPOILER ACTUATOR FITTINGS. I N T E R N A L ACCESS EXTEND FLAPS AND GROUND SPOILERS.

552 652

5521S 6521S

MPD MPD MRB MRB

57-280-01 57-280-02 MSI 57-280-01 MSI 57-280-02 I: 6 YRS I: 18000 CYC

ITEMS

ATA: 57 - 55

E2 HHI 737-700

2 25-apr-06

Page 1 of 1


HHI R E V

ITEM 71 71 - 11 711101 20000

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

711102 20000

VISUALLY CHECK THE LEFT AND RIGHT INLET COWL (INNER SIDE AND 412 OUTER SKIN). 422

emp emp

VISUALLY CHECK THE LEFT AND RIGHT ENGINE FAN COWL FOR CONDITION AND SECURITY OF INSTALLATION.

413 414 423 424

emp emp emp emp

R

MPD MPD MRB

Date: 23-jul-08

EFF

R L ITEM BY E E REVISION P V DATE

71-11-01-200-801-F00 I: 800 FLH

MPD MPD MRB

71-020-01 71-020-02 MSI 71-020-01 RTE:9 MSI 71-020-02 RTE:9

CHECK THRUST REVERSER, EXHAUST PLUG, EXHAUST CASE STRUTS 410 AND VISIBLE TURBINE BLADES ON LPT FOR OBVIOUS DAMAGE AND 420 EVIDENCE OF METAL / OIL ACCUMULATION

emp emp

empty

CHECK ENGINE COWLING, INLET COWL, NOSE DOME AND VISIBLE FAN 410 BLADES FOR OBVIOUS DAMAGE. 420 CHECK ACCESS PANELS AND BLOW OUT DOORS FOR CONDITION AND SECURITY ALSO CHECK FOR OPEN LATCHES AND SIGNS OF FLUID LEAKAGE.

emp emp

empty

AMM

AMM AMM AMM

ITEMS

71-010-01 71-010-02 MSI 71-010-01 RTE:9 MSI 71-010-02 RTE:9

AMTOSS

AMTOSS AMM

711104 20000

TSK

INLET COWL

MRB

711103 20000

THRESHOLD INTERVAL

POWER PLANT

MRB

R

737-6

MAINTENANCE SCHEDULE

E2 HHI 737-700

3 03-jun-04

71-11-02-20 I: 4000 FLH 71-11-02-200-801-F00

E2 HHI 737-700

3 23-jul-08

71-00-00 SERVICE EXPERIENCE

I: 1 T

E2 HHI 737-700

1 02-aug-99

SERVICE I: 1 T EXPERIENCE 71-11-00 71-11-01-200-801-F00 71-11-02-200-802-F00

E2 HHI 737-700

3 03-jun-04

ATA: 71 - 11

Page 1 of 1


HHI R E V

ITEM 71 - 71

R

737-6

MAINTENANCE SCHEDULE

717100 20000

R

717100 70000

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

ENGINE DRAINS GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT ENGINE DRAIN 411 LINES. emp 415 416 417 421 emp 425 426 427

413 414 415 416 emp 423 424 425 426 emp

MPD MPD MRB

AMTOSS AMM

71-71-00-20 I: 6000 FLH 71-71-00-200-802-F00

OPERATIONALLY CHECK ALL LEFT AND RIGHT ENGINE DRAIN LINES.

emp emp

MPD MPD MRB

71-040-01 71-040-02 MSI 71-040-01 RTE:9 MSI 71-040-02 RTE:9

411 421

MRB

MRB AMTOSS

Date: 23-jul-08

THRESHOLD INTERVAL

ITEMS

71-050-01 71-050-02 MSI 71-050-01 RTE:9 MSI 71-050-02 RTE:9

71-71-00-700-801-F00 I: 6 YRS

ATA: 71 - 71

E1 HHI 737-700

5 23-jul-08

F1 HHI 737-700

3 25-apr-06

Page 1 of 1


HHI R E V

R

ITEM

DESCRIPTION

72

ENGINE

72 - 00

ENGINE

720000 20000

R R

720000 20200

ZONE ACCESS

STRUCTURE

REFERENCES

413 414 415 416 423 424 425 426

MPD MPD MRB

AMTOSS AMM

72-00-00-20 I: 1600 CYC 72-00-00-200-805-F00

BORESCOPE INSPECTION OF THE LEFT AND RIGHT ENGINE HPT NOZZLE. 411 emp 421 emp

415 416 425 426

MPD MPD MRB

72-200-01 72-200-02 MSI 72-200-01 RTE:6 MSI 72-200-02 RTE:6

R 720000 20300

MRB

BORESCOPE INSPECTION OF THE LEFT AND RIGHT ENGINE HPT BLADES. 411 emp 421 emp

415 416 425 426

R

72-00-00-20 I: 1600 CYC 72-00-00-200-806-F00

MPD MPD MRB

72-210-01 72-210-02 MSI 72-210-01 RTE:6 MSI 72-210-02 RTE:6

AMTOSS AMM

ITEMS

TSK

EFF

R L ITEM BY E E REVISION P V DATE

72-180-01 72-180-02 MSI 72-180-01 RTE:9 MSI 72-180-02 RTE:9

AMTOSS AMM

MRB

Date: 23-jul-08

THRESHOLD INTERVAL

BORESCOPE INSPECTION OF THE LEFT AND RIGHT ENGINE COMBUSTION 411 CHAMBER. emp emp emp 421 emp emp emp

MRB

R

737-6

MAINTENANCE SCHEDULE

72-00-00-20 I: 1600 CYC 72-00-00-200-807-F00

ATA: 72 - 00

E4 HHI 737-700

2 23-jul-08

E4 HHI 737-700

2 23-jul-08

E4 HHI 737-700

2 23-jul-08

Page 1 of 2


HHI R E V

ITEM

R

720000 20400

R

R

720011 01200

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

413 414 415 416 423 424 425 426

MPD MPD MRB

AMTOSS AMM AMM AMM

72-00-00-200-814-F00 I: 6000 FLH 72-00-00-200-804-F00 I: 6000 CYC 72-00-00-200-802-F00 72-00-00-200-817-F00

VISUAL CHECK OF THE LEFT AND RIGHT ENGINE FAN INLET ATTACHMENT 411 BOLTS. emp 421 emp

413 414 423 424

MPD MPD MRB

72-080-01 72-080-02 MSI 72-080-01 RTE:9 MSI 72-080-02 RTE:9

R 720021 00200

MRB

VISUAL CHECK OF THE ATTACHMENT BOLTS FOR THE LEFT AND RIGHT 411 FORWARD ENGINE MOUNT. emp 421 emp

413 414 423 424

R

71-11-01-20 I: 6000 FLH 71-11-01-200-802-F00

MPD MPD MRB

72-090-01 72-090-02 MSI 72-090-01 RTE:9 MSI 72-090-02 RTE:9

AMM AMTOSS

ITEMS

TSK

EFF

R L ITEM BY E E REVISION P V DATE

72-120-01 72-120-02 MSI 72-120-01 RTE:6 MSI 72-120-02 RTE:6

AMTOSS AMM

MRB

Date: 23-jul-08

THRESHOLD INTERVAL

BORESCOPE INSPECTION OF THE LEFT AND RIGHT ENGINE STAGES 2, 411 4, 6 & 8 HPC BLADES emp emp emp 421 emp emp emp

MRB

R

737-6

MAINTENANCE SCHEDULE

71-21-00-200-801-F00 I: 6000 FLH 71-21-00-20

ATA: 72 - 00

E4 HHI 737-700

4 23-jul-08

E2 HHI 737-700

3 23-jul-08

E2 HHI 737-700

3 23-jul-08

Page 2 of 2


HHI R E V

ITEM 72 - 20

R

737-6

MAINTENANCE SCHEDULE

722000 21000

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

FAN SECTION VISUALLY CHECK OF THE LEFT AND RIGHT ENGINE TRANSFER AND /OR 411 ACCESSORY GEARBOX MOUNT FLANGES. emp 421 emp

413 414 423 424

MPD MPD MRB MRB

R

Date: 23-jul-08

THRESHOLD INTERVAL

AMM AMTOSS

ITEMS

72-070-01 72-070-02 MSI 72-070-01 RTE:9 MSI 72-070-02 RTE:9 72-20-00-210-801-F00 I: 6000 FLH 72-20-00-21 I: 6000 CYC

ATA: 72 - 20

E2 HHI 737-700

3 23-jul-08

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 72 - 21

722100 20000

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

VISUALLY CHECK THE LEFT AND RIGHT ENGINE INLET AND FAN BLADES. 411 421

emp emp

MPD MPD MRB

EFF

R L ITEM BY E E REVISION P V DATE

DETAILED INSPECTION OF THE LEFT AND RIGHT ENGINE INLET AND FAN 411 BLADES. 421

emp emp

72-21-00-200-801-F00 I: 50 FLH

MPD MPD MRB

72-020-01 72-020-02 MSI 72-020-01 RTE:6 MSI 72-020-02 RTE:6

AMTOSS

ITEMS

72-010-01 72-010-02 MSI 72-010-01 RTE:6 MSI 72-010-02 RTE:6

AMTOSS

MRB

Date: 23-jul-08

TSK

SPINNER CONE

MRB

722100 22000

THRESHOLD INTERVAL

72-21-00-220-801-F00 I: 1200 FLH

ATA: 72 - 21

E2 HHI 737-700

3 03-jun-04

E3 HHI 737-700

4 25-apr-06

Page 1 of 1


HHI R E V

ITEM 72 - 23

R

722304 20000

R R

737-6

MAINTENANCE SCHEDULE

722304 21000

R

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

THRUST MOUNT FITTINGS VISUAL CHECK OF THE LEFT AND RIGHT ENGINE ATTACHMENT BOLTS 411 FOR THE THRUST MOUNT FITTINGS. emp emp emp 421 emp emp emp

413 414 415 416 423 424 425 426

MPD MPD MRB

AMM AMTOSS

72-23-04-200-802-F00 I: 5000 CYC 72-23-04-20

VISUAL CHECK OF THE LEFT AND RIGHT ENGINE THRUST MOUNT FITTINGS.

413 414 415 416 423 424 425 426

MPD MPD MRB

72-110-01 72-110-02 MSI 72-110-01 RTE:8 MSI 72-110-02 RTE:8

411 emp emp emp 421 emp emp emp

ITEMS

MRB

MRB AMM AMTOSS

72-100-01 72-100-02 MSI 72-100-01 RTE:9 MSI 72-100-02 RTE:9

72-23-04-200-801-F00 I: 6000 FLH 72-23-04-20

ATA: 72 - 23

E2 HHI 737-700

2 23-jul-08

E2 HHI 737-700

3 23-jul-08

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 72 - 30

723000 31000

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

COMPRESSOR SECTION DETAILED INSPECTION AND LUBRICATION OF THE ENGINES FAN BLADE 411 PRESSURE FACES AND FAN DISK DOVETAIL SLOTS. 421

emp emp

empty

AMM

AMM

Date: 23-jul-08

THRESHOLD INTERVAL

ITEMS

ESM 005 72-21-02 REMOVAL/ INSTALLATION 72-21-01 REMOVAL/ INSTALLATION

I: 3000 CYC I: 5000 FLH

ATA: 72 - 30

E3 HHI S 737-700

3 18-mar-05

Page 1 of 1


HHI R E V

ITEM 72 - 50

R

737-6

MAINTENANCE SCHEDULE

725000 20000

R

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

TURBINE SECTION VISUAL CHECK OF THE LEFT AND RIGHT ENGINE AFT MOUNTS CLEVIS 411 FOR STRUCTURAL INTEGRITY FAILURE. emp emp emp 421 emp emp emp

413 414 415 416 423 424 425 426

ITEMS

MPD MPD MRB MRB AMTOSS AMM

72-300-01 72-300-02 MSI 72-300-01 RTE:9 MSI 72-300-02 RTE:9 72-56-00-20 I: 6000 FLH 72-56-00-200-802-F00

ATA: 72 - 50

E2 HHI 737-700

3 23-jul-08

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM 72 - 60

726000 20000

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

ACCESSORY DRIVE SECTION VISUAL CHECK OF THE LEFT AND RIGHT ENGINE AGB AND TGB ATTACHMENT FLANGES.

411 emp 421 emp

413 414 423 424

MPD MPD MRB MRB AMTOSS AMTOSS

Date: 23-jul-08

THRESHOLD INTERVAL

ITEMS

72-340-01 72-340-02 MSI 72-340-01 RTE:9 MSI 72-340-02 RTE:9 72-60-00-200-801-F00 I: 6000 FLH 72-63-00-200-801-F00

ATA: 72 - 60

E2 HHI 737-700

3 30-nov-05

Page 1 of 1


HHI R E V

ITEM 73 73 - 11

R

737-6

MAINTENANCE SCHEDULE

731102 00000

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

ENGINE FUEL AND CONTROL FUEL FILTER REPLACE THE LEFT AND RIGHT ENGINE FUEL FILTER.

411 emp 421 emp

413 414 423 424

MPD MPD MRB MRB

R

Date: 23-jul-08

THRESHOLD INTERVAL

AMTOSS AMM AMM

ITEMS

73-010-01 73-010-02 MSI 73-010-01 RTE:6 MSI 73-010-02 RTE:6 73-11-02-00 I: 6000 FLH 73-11-02-000-801-F00 73-11-02-400-801-F00

ATA: 73 - 11

S

HHI 737-700

3 23-jul-08

Page 1 of 1


HHI R E V

ITEM 73 - 21

R

737-6

MAINTENANCE SCHEDULE

732100 74000

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

FUEL CONTROL SYSTEM INTERROGATE THE FMC CDU FOR LEFT AND RIGHT ENGINE FAULTS.

211 212

emp emp

MPD MPD MRB MRB

R

Date: 23-jul-08

THRESHOLD INTERVAL

AMTOSS AMM

ITEMS

73-020-01 73-020-02 MSI 73-020-01 RTE:9 MSI 73-020-02 RTE:9 73-21-00-74 I: 150 FLH 73-21-00-740-803-F00

ATA: 73 - 21

F1 HHI 737-700

2 23-jul-08

Page 1 of 1


HHI R E V

ITEM 74 74 - 21

R

742101 20000

R R

737-6

MAINTENANCE SCHEDULE

742102 20000

R

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

IGNITION IGNITION LEADS DETAILED INSPECTION OF THE LEFT AND RIGHT ENGINE IGNITOR LEAD. 411 emp emp emp 421 emp emp emp

413 414 415 416 423 424 425 426

MPD MPD MRB

AMTOSS AMM

74-21-01-20 I: 4000 CYC 74-21-01-200-801-F00

DETAILED INSPECTION OF THE ENGINE IGNITOR PLUGS.

413 414 415 416 423 424 425 426

MPD MPD MRB

74-010-01 74-010-02 MSI 74-010-01 RTE:6 MSI 74-010-02 RTE:6

411 emp emp emp 421 emp emp emp

ITEMS

MRB

MRB AMTOSS AMM

74-020-01 74-020-02 MSI 74-020-01 RTE:6 MSI 74-020-02 RTE:6

74-21-02-20 I: 1600 CYC 74-21-02-200-801-F00

ATA: 74 - 21

E3 HHI 737-700

3 23-jul-08

E3 HHI 737-700

3 23-jul-08

Page 1 of 1


HHI R E V

ITEM 78 78 - 11

R

737-6

MAINTENANCE SCHEDULE

781100 21000

R

Date: 23-jul-08

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

EXHAUST TURBINE EXHAUST SYSTEM VISUAL CHECK OF LEFT AND RIGHT ENGINE LABYRINTH SEALS.

417 emp emp emp 427 emp emp emp

413 414 415 416 423 424 425 426

ITEMS

MPD MPD MRB MRB AMTOSS AMM

78-020-01 78-020-02 MSI 78-020-01 RTE:9 MSI 78-020-02 RTE:9 78-11-00-21 I: 6000 FLH 78-11-00-210-801-F00

ATA: 78 - 11

E2 HHI 737-700

3 23-jul-08

Page 1 of 1


HHI R E V

ITEM 78 - 31

R

783100 70000

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

PERFORM OPERATIONAL CHECK (BITE) ON THE LEFT AND RIGHT ENGINE 117 EAU. 118

117A emp

R 783100 71000

PERFORM AN OPERATIONAL CHECK OF THE LEFT AND RIGHT ENGINE 117 T/R SYNC LOCK 118 415 416 425 426

117A emp emp emp emp emp

R 783100 73000

MPD MPD MRB

783106 20000

R

Date: 23-jul-08

TSK

EFF

R L ITEM BY E E REVISION P V DATE

PERFORM AN OPERATIONAL CHECK OF THE LEFT AND RIGHT ENGINE 211 "REVERSER" LIGHT INDICATION SYSTEM. 212

emp emp

VISUALLY CHECK THE LEFT AND RIGHT ENGINE BLOCKER DOORS.

415 emp emp 416 425 emp emp 426

413 414 415 416 423 424 425 426

ITEMS

78-120-01 78-120-02 MSI 78-120-01 RTE:9 MSI 78-120-02 RTE:9

AMTOSS AMM

78-31-00-70 I: 1200 FLH 78-31-00-700-804-F00

AAR MPD MPD MRB

78-CMR-01 78-110-01 78-110-02 MSI 78-110-01 RTE:9 MSI 78-110-02 RTE:9

MRB

F1 HHI 737-700

3 23-jul-08

F1 HHI 737-700

2 23-jul-08

I: 6000 FLH

F1 HHI 737-700

3 18-mar-05

78-31-06-20 I: 6000 FLH 78-31-06-200-801-F00

E2 HHI 737-700

4 23-jul-08

AMTOSS AMM

78-31-00-70 I: 5000 FLH 78-31-00-700-803-F00

MPD MPD MRB

78-130-01 78-130-02 MSI 78-130-01 RTE:9 MSI 78-130-02 RTE:9

MRB

R

THRESHOLD INTERVAL

THRUST REVERSER SYSTEM ( HARDWARE)

MRB

R

737-6

MAINTENANCE SCHEDULE

AMTOSS AMTOSS

78-31-00-71 78-31-00-70

MPD MPD MRB

78-070-01 78-070-02 MSI 78-070-01 RTE:9 MSI 78-070-02 RTE:9

MRB AMTOSS AMM

ATA: 78 - 31

Page 1 of 3


HHI R E V

ITEM

R

783107 90000

DESCRIPTION DETAILED INSPECTION OF THE THRUST REVERSER DRAG LINK SPHERICAL BEARINGS

R R

783112 20000

VISUALLY CHECK THE RIGHT AND LEFT ENGINE T / R FIRE SEAL.

R R

737-6

MAINTENANCE SCHEDULE

783112 21000

DETAILED INSPECT THE LEFT AND RIGHT ENGINE T/R FIRE SEAL.

R 783114 20000

Date: 23-jul-08

VISUALLY CHECK THE LEFT AND RIGHT ENGINE T/R'S INNER WALL.

ZONE ACCESS

STRUCTURE

REFERENCES

THRESHOLD INTERVAL

415 emp emp 416 425 emp emp 426

413 414 415 416 423 424 425 426

MPD MPD MRB

AMTOSS AMM

78-31-07-90 I: 6000 FLH 78-31-07-900-801-F00

415 emp emp 416 425 emp emp 426

413 414 415 416 423 424 425 426

MPD MPD MRB

78-090-01 78-090-02 MSI 78-090-01 RTE:8 MSI 78-090-02 RTE:8

AMTOSS AMM

78-31-12-20 I: 3600 FLH 78-31-12-200-801-F00

415 emp emp 416 425 emp emp 426

413 414 415 416 423 424 425 426

MPD MPD MRB

78-100-01 78-100-02 MSI 78-100-01 RTE:8 MSI 78-100-02 RTE:8

AMTOSS AMM

78-31-12-20 I: 6000 FLH 78-31-12-200-802-F00

415 emp emp 416 425 emp emp 426

413 414 415 416 423 424 425 426

MPD MPD MRB

78-050-01 78-050-02 MSI 78-050-01 RTE:9 MSI 78-050-02 RTE:9

ITEMS

MRB

MRB

MRB

MRB AMTOSS

TSK

EFF

R L ITEM BY E E REVISION P V DATE

78-060-01 78-060-02 MSI 78-060-01 RTE:9 MSI 78-060-02 RTE:9

78-31-14-20

I: 6000 FLH

ATA: 78 - 31

E3 HHI 737-700

7 23-jul-08

E2 HHI 737-700

6 23-jul-08

E3 HHI 737-700

3 23-jul-08

E2 HHI 737-700

3 18-mar-05

Page 2 of 3


HHI

737-6

MAINTENANCE SCHEDULE

R E V

ITEM

DESCRIPTION

R

783123 20000

VISUALLY CHECK THE LEFT AND RIGHT ENGINE BULLNOSE SEAL AND RETAINER.

R

Date: 23-jul-08

ZONE ACCESS 415 emp emp 416 425 emp emp 426

STRUCTURE

413 414 415 416 423 424 425 426

ITEMS

REFERENCES MPD MPD MRB MRB AMTOSS AMM

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

78-080-01 78-080-02 MSI 78-080-01 RTE:9 MSI 78-080-02 RTE:9 78-31-23-20 I: 6000 FLH 78-31-23-200-801-F00

ATA: 78 - 31

E2 HHI 737-700

4 23-jul-08

Page 3 of 3


HHI R E V

ITEM 79 79 - 00

R

790000 20000

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

DETAILED INSPECTION OF THE LEFT AND RIGHT ENGINE OIL SUPPLY FILTER POP-OUT INDICATOR.

411 421

413BL 423BL

MPD MPD MRB

DETAILED INSPECTION OF THE LEFT AND RIGHT ENGINE AGB/ TGB AND AFT AND FWD SUMP MAGNETIC CHIP DETECTOR FOR PARTICLES (FOR ENGINES WITH MCD) OR INTERROGATE DMS FOR CHIP DETECTOR STATUS (FOR ENGINES WITH DEBRIS MONITORING SYSTEM).

211 212 411 421

emp emp 413BL 423BL

R

79-00-00-20 I: 1200 FLH 79-00-00-200-805-F00

MPD MPD MRB

72-320-01 72-320-02 MSI 72-320-01 RTE:6 MSI 72-320-02 RTE:6

AMTOSS AMM

Date: 23-jul-08

EFF

R L ITEM BY E E REVISION P V DATE

TOP OFF ENGINE OIL ON BOTH ENGINES AFTER 5 MINUTES FROM ENGINE 410 SHUT DOWN, BUT NOT GREATER THAN 30 MINUTES AND RECORD 420 CONSUMPTION. CHECK OIL TANK CAP FOR PROPER INSTALLATION.

emp emp

E3 HHI 737-700

3 23-jul-08

79-00-00-20 I: 500 FLH 79-00-00-200-804-F00

E3 HHI 737-700

3 23-jul-08

SERVICE EXPERIENCE 12-13-11

S HHI E1 737-700

2 18-mar-05

empty

AMM

ITEMS

79-020-01 79-020-02 MSI 79-020-01 RTE:9 MSI 79-020-02 RTE:9

AMTOSS AMM

MRB

790000 80000

TSK

ENGINE OIL GENERAL

R 790000 20500

THRESHOLD INTERVAL

OIL

MRB

R

737-6

MAINTENANCE SCHEDULE

I: 1 Z

ATA: 79 - 00

Page 1 of 1


HHI R E V

ITEM 79 - 21

R

792103 00000

DESCRIPTION

ZONE ACCESS

STRUCTURE

REFERENCES

REMOVE AND REPLACE THE LEFT AND RIGHT ENGINE OIL SUPPLY FILTER 411 ELEMENT. 421

413 423

R

792106 00000

MPD MPD MRB

TSK

EFF

R L ITEM BY E E REVISION P V DATE

REMOVE AND REPLACE THE LEFT AND RIGHT ENGINE OIL SCAVENGE FILTER ELEMENT.

411 421

413 423

R

79-21-03-40 I: 6000 FLH 79-21-03-00 79-21-03-000-802-F00 79-21-03-400-801-F00

MPD MPD MRB

79-040-01 79-040-02 MSI 79-040-01 RTE:9 MSI 79-040-02 RTE:9

AMTOSS AMTOSS AMM AMM

ITEMS

79-010-01 79-010-02 MSI 79-010-01 RTE:9 MSI 79-010-02 RTE:9

AMTOSS AMTOSS AMM AMM

MRB

Date: 23-jul-08

THRESHOLD INTERVAL

ENGINE OIL FILTER

MRB

R

737-6

MAINTENANCE SCHEDULE

79-21-06-40 I: 6000 FLH 79-21-06-00 79-21-06-000-801-F00 79-21-06-400-801-F00

ATA: 79 - 21

S

HHI 737-700

3 23-jul-08

S

HHI 737-700

3 23-jul-08

Page 1 of 1


HHI R E V

R

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

80

STARTING

80 - 11

STARTER

801101 20000

DETAILED INSPECTION OF THE LEFT AND RIGHT ENGINE STARTER MAGNETIC CHIP DETECTOR FOR METAL CHIPS.

ZONE ACCESS

411 421

STRUCTURE

413 423

REFERENCES

MPD MPD MRB MRB

R

Date: 23-jul-08

AMTOSS AMM

ITEMS

THRESHOLD INTERVAL

TSK

EFF

R L ITEM BY E E REVISION P V DATE

80-010-01 80-010-02 MSI 80-010-01 RTE:6 MSI 80-010-02 RTE:6 80-11-01-20 I: 1600 CYC 80-11-01-200-801-F00

ATA: 80 - 11

E3 HHI 737-700

2 23-jul-08

Page 1 of 1


HHI

1

MAINTENANCE SCHEDULE

737-6/-7/-8

GENERAL

This Component Maintenance Section is an integrated part of the 737 Maintenance Schedule. Component Maintenance Section reflects specific component maintenance tasks under consideration of Airworthiness Authority Requirements as like: - Life Limits from Service Letters - Life Limits from Engine Manual - Requirements from Type Certification Data Sheets - National Requirements - MRBR component requirements All common statements from Maintenance Schedule Introduction are also effective for Component Maintenance Section. Explanation of deviations from Maintenance Schedule Introduction to Component Maintenance Section are given in the following.

2

FORMAT LAYOUT DESCRIPTION AND DEFINITION OF TERMS

2.1

Revision Column

A letter code gives the status of the item at the date of publication shown in the page header: "N" : New "R" : Revised "D" : Deleted Blank : No change

Date: 23-Jul-2008

EXPLANATION COMPONENT MAINTENANCE SECTION

Page: 1 of 6


HHI

2.2

MAINTENANCE SCHEDULE

737-6/-7/-8

ITEM Column

The item number is split into four figure groups: • group 1 : 2 digits (CM) indicating that this item is part of the Component Maintenance Section • group 2 : 4 digits giving ATA / sub ATA specification as per IPC • group 3 : 2 digits giving ATA-unit specification as per IPC • group 4 : 3 digits giving item number identification In principle each item corresponds to one task (which may cover several "tasks codes") and one interval (and possibly one threshold). If several intervals do appear, they are always in different units (FLH, CYC,...) and in that case the meaning of such a situation is: to apply the interval "what ever comes first".

2.3

Description Column

It gives an accurate part description according to manufacturer nomenclature with a specified part number reference. The part number reference gives a clear statement of considered part numbers approved for installation by IPC or equivalent documents. - P/N all - P/N only - except P/N

i.e. all part numbers with this part description are effected i.e. only specified part numbers with this part description are effected i.e. all part numbers with this part description except for specified part numbers are effected

In addition in that column may appear some notes when necessary. These notes are of 2 categories:

Date: 23-Jul-2008

EXPLANATION COMPONENT MAINTENANCE SECTION

Page: 2 of 6


HHI

MAINTENANCE SCHEDULE

737-6/-7/-8

Note: General notes affecting some of the parameters produced in the layout (INTERVAL, TASK CODE, etc.). In any case a highlight "NOTE" appear, with, in front of it, a note mark identifying the affected parameters. These possible note marks are: • E : effectivity • T : threshold • I : interval • J : task code • R : reference • M : miscellaneous Condition Note: Specific note when the task to be performed depends on the embodiment of such modifications which are then indicated in that note. In that case a highlight "CONDITION" appears.

2.4

ZONE Column (not used)

NOTE: Due to EDP requirements this field has an initial setting „000“.

2.5

ACCESS Column (not used)

2.6

Structure Column (not used)

Date: 23-Jul-2008

EXPLANATION COMPONENT MAINTENANCE SECTION

Page: 3 of 6


HHI

2.7

MAINTENANCE SCHEDULE

737-6/-7/-8

REFERENCES Column

It shows each document or manual necessary to be consulted to produce a clear understanding of the requested task, as well as references covering the origin of the item. For items which are affected by Directive from Airworthiness Authorities, the letter's reference will be mentioned in this column, and the maximum allowable limit shown in a NOTE preceded by the note mark "I" (for interval). Such references are indicated by means of their alphabetical code and their number. Examples of references types: Indicates an Airworthiness Requirement • AAR......AD number: Aircraft Maintenance Manual • AMM...........number: Certification Maintenance Requirements • CMR........................: Requirement of US Department of Transportation • DOT........................: Maintenance Significant Item of the MRBR • MSI.............number: Structural Significant Item of the MRBR • SSI..............number: Cross Reference to MS task • MS .............number: Service Information. Indicates if source of task is experience of Lufthansa Technik (LHT) or a customer request. • SI ...........................:

2.8

THRESHOLD / INTERVAL Column

It shows the maximum allowed interval for each task to be performed. This interval is preceded by the letter "I:". Should the task become effective only after expiration of a certain limit, this limit appears (as a THRESHOLD) preceded by the letter "T:". The units in which intervals/ thresholds are expressed are as follows:

Date: 23-Jul-2008

EXPLANATION COMPONENT MAINTENANCE SECTION

Page: 4 of 6


HHI

• • • • • • • • • • •

MAINTENANCE SCHEDULE

FLH CYC OPM OSM STM C CR IL D EC AC

2.9

737-6/-7/-8

flight hours flight cycles Operational Month Operational & Storage Month Storage Month C-check Cabin Refurbishment Intermediate Layover D-Check Engine Change APU Change

TASK Column

The task code indicated in this column gives a definition of the required task. Task Codes in accordance with JAA Form One are used as follows: Inspection / Test • F Overhaul • O Discard • Y

2.10 EFFECTIVITY Column It describes the Airline, or Aircraft model, or Engine type, or specific individual a/c to which the concerned task applies. "ALL" appears when the task applies to all aircraft.

Date: 23-Jul-2008

EXPLANATION COMPONENT MAINTENANCE SECTION

Page: 5 of 6


HHI

MAINTENANCE SCHEDULE

737-6/-7/-8

2.11 BY Column (not used) 2.12 REP Column Information for LHT internal purposes only.

2.13 LEV Column It shows, for each time, the revision level of this item (00 for the first issue, 01 to 99 for revisions).

2.14 ITEM REVISION DATE Column It shows, for each item, the last revision date of this item. This date is always lower or equal to the date of revision of the whole Maintenance Schedule.

Date: 23-Jul-2008

EXPLANATION COMPONENT MAINTENANCE SECTION

Page: 6 of 6


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM CM CM - 21

DESCRIPTION

ZONE ACCESS

STRUCTURE

TSK

EFF

R L ITEM BY E E REVISION P V DATE

COMPONENT MAINTENANCE SECTION AIR CONDITIONING

R CM2132 00000 FUNCTIONAL CHECK OF THE POSITIVE PRESSURE RELIEF VALVES AND 000 REPLACEMENT OF THE POSITIVE PRESSURE RELIEF VALVE FILTERS

emp

MPD MPD MRB MRB

R

Date: 23-jul-08

THRESHOLD INTERVAL

REFERENCES

21-070-00 21-080-00 MSI 21-070-00 RTE:9 MSI 21-080-00 RTE:9 I: 10000 FLH

ITEMS

ATA: CM - 21

O

HHI 737-700

2 23-jul-08

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM CM - 23

DESCRIPTION

ZONE ACCESS

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

COMMUNICATIONS

R CM2324 00000 EMERGENCY LOCATOR TRANSMITTER (AUTOMATIC/FIXED). P/N 453-5004 NOTE( J ) R TASK TO INCLUDE BATTERY REPLACEMENT.

000

R CM2371 00010 UNDERWATER LOCATOR BEACON 000 P/N "ALL" NOTE( M, I ) R NOTE:(I) INTERVAL LIMIT TO BE CALCULATED FROM BATTERY FABRICATION DATE. NOTE: (M) TASK TO INCLUDE BATTERY REPLACEMENT.

Date: 23-jul-08

STRUCTURE

emp

emp

ITEMS

MRB

MSI 23-110-00 RTE:8

AMM

23-24-00-900-801-001 I: 60 OSM

MRB

MSI 23-070-00 RTE:9

MS

237121 00000

I: 72 OSM

ATA: CM - 23

Y F

HHI 737-700 only: D-AHIC

2 23-jul-08

O

HHI 737-700

3 23-jul-08

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM CM - 24

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

EFF

R L ITEM BY E E REVISION P V DATE

ELECTRICAL POWER

CM2430 00010 BATTERY, MAIN AND AUXILIARY P/N "ALL"

000

emp

MRB MRB

MSI 24-090-00 RTE:8 MSI 24-120-00 RTE:8 I: 2000 FLH

Date: 23-jul-08

TSK

ITEMS

ATA: CM - 24

O

HHI 737-700

1 03-jun-04

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM CM - 25

DESCRIPTION

ZONE ACCESS

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

EQUIPMENT/ FURNISHING

R CM2560 00020 LIFE VEST CREW P/N 63600-505 NOTE( E ) R VACUUM SEALED LIFE VESTS

000

R CM2560 00021 LIFE VEST CREW P/N 63600-505 NOTE( E ) R NON-VACUUM SEALED LIFE VESTS

000

R CM2560 00030 LIFE VEST ADULT/CHILD ADULT: P/N 63600-105 P/N 0723E105P CHILD: P/N 216200-0 R P/N 208511-1 NOTE( E ) VACUUM SEALED LIFE VESTS

000

R CM2560 00031 LIFE VEST ADULT/CHILD ADULT: P/N 63600-105 P/N 0723E105P R CHILD: P/N 21600-0 P/N 208511-1 NOTE( E ) NON-VACUUM SEALED LIFE VESTS

000

CM2564 00020 EMERGENCY LOCATOR TRANSMITTER (PORTABLE) P/N 1151324-1 NOTE( J ) TASK TO INCLUDE BATTERY REPLACEMENT

000

CM2564 00090 SMOKE HOODS P/N "ALL" NOTE( I ) VENDOR RECOMMENDATION

000

Date: 23-jul-08

STRUCTURE

emp

emp

emp

emp

emp

emp

ITEMS

MRB

MRB

MPD MRB

MRB

MSI 25-290-00 RTE:8 I: 120 OSM I: 1 s.N

O

HHI 737-700

3 23-jul-08

I: 1 s.N I: 60 OSM

O

HHI 737-700

1 23-jul-08

I: 120 OSM I: 1 s.N

O

HHI 737-700

3 23-jul-08

I: 60 OSM I: 1 s.N

O

HHI 737-700

1 23-jul-08

I: 60 OSM

F

HHI 737-700

5 18-mar-05

I: 120 OSM

Y

HHI 737-700

0 25-apr-06

MSI 25-290-00 RTE:8

25-290-00 MSI 25-290-00 RTE:8

MSI 25-290-00 RTE:8

MRB

MSI 25-350-00 RTE:8

CMM

25-60-10

MPD MRB

25-410-00 MSI 25-410-00 RTE:8

ATA: CM - 25

Page 1 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

ZONE ACCESS

R CM2566 00010 ESCAPE SLIDE 1L/R 000 P/N "ALL" NOTE( I ) INFLATABLES FIFTEEN YEARS AND OLDER SHOULD BE INSPECTED AT 12 MTH INTERVAL (BFG SNL 25-163 OF NOV 12/99).

STRUCTURE

emp

THRESHOLD INTERVAL

REFERENCES MPD MPD MPD MRB MPD MRB MRB MRB

emp

MPD MRB MRB MRB

CM2566 00030 RESERVOIR AND VALVE ASSY, ESCAPE SLIDE 1 L/R, 3L/R P/N "ALL"

CM2566 00040 RESERVOIR ASSY, ESCAPE SLIDE 1 L/R, 3L/R P/N "ALL" NOTE( I ) LIFE LIMIT 180 MTH REQUIRED BY DOT

Date: 23-jul-08

000

000

emp

emp

ITEMS

MPD MRB

AAR

EFF

R L ITEM BY E E REVISION P V DATE

25-260-00 25-270-00 25-280-00 MSI 25-280-00 RTE:8 25-240-00 MSI 25-240-00 RTE:8 MSI 25-260-00 RTE:8 MSI 25-270-00 RTE:8

R CM2566 00020 ESCAPE SLIDE 3L/R 000 P/N "ALL" NOTE( I ) INFLATABLES FIFTEEN YEARS AND OLDER SHOULD BE INSPECTED AT 12 MTH INTERVAL (BFG SNL 25-163 OF NOV 12/99)

TSK

I: 36 OSM

O

HHI 737-700

2 23-jul-08

I: 36 OSM

O

HHI 737-700

1 03-jun-04

I: 36 OSM

O

HHI 737-700

3 22-mar-07

I: 180 OSM

Y

HHI 737-700

1 26-jun-02

25-240-00 MSI 25-240-00 RTE:8 MSI 25-260-00 RTE:8 MSI 25-270-00 RTE:8

25-240-00 MSI 25-240-00 RTE:8

DOT

ATA: CM - 25

Page 2 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM CM - 26

DESCRIPTION

ZONE ACCESS

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

FIRE PROTECTION

CM2600 00010 LOWER CARGO COMPARTMENT FIRE EXTINGUISHING BOTTLE 000 P/N "ALL" NOTE( I, J ) NOTE (I): HYDROSTATIC TEST PRIOR TO ITS NEXT REFILL AFTER 60 MTH SINCE PREVIOUS HYDROSTATIC TEST NOTE (J): HYDROSTATIC TEST INCLUDES THE FUNCTIONAL CHECK OF THE FIRE BOTTLE PRESSURE SWITCH. ACCESS REMOVAL OF AIR CONDITIONING DUCTING MAY BE REQUIRED.

emp

CM2621 00010 ENGINE FIRE EXTINGUISHING BOTTLE 000 P/N "ALL" NOTE( I, J ) NOTE (I): HYDROSTATIC TEST PRIOR TO ITS NEXT REFILL AFTER 60 MONTHS SINCE PREVIOUS HYDROSTATIC TEST NOTE (J): HYDROSTATIC TEST INCLUDES THE FUNCTIONAL CHECK OF THE FIRE BOTTLE PRESSURE SWITCH, REMOVAL FOR FUNCTIONAL TEST OF THE FIRE BOTTLE PRESSURE GAUGE AND REPLACEMENT OF THE ENGINE FIRE BOTTLE OVERPRESSURE RELIEF DISC.

emp

CM2621 00020 CARTRIDGE, ENGINE FIRE EXTINGUISHER 000 P/N "ALL" NOTE( I ) FOR CARTRIDGES MANUFACTURED PRIOR TO 07/1991 THE TOTAL LIFE IS REDUCED TO 78 MONTH.

emp

Date: 23-jul-08

STRUCTURE

MRB MRB

MRB MRB MRB MRB

ITEMS

MRB

MSI 26-351-00 MSI 26-360-00 RTE:9 I: 120 OSM

O

HHI 737-700

6 22-mar-07

I: 120 OSM

O

HHI 737-700

4 30-nov-05

I: 132 OSM

Y

HHI 737-700

1 03-jun-04

MSI 26-061-00 MSI 26-100-00 RTE:8 MSI 26-120-00 RTE:8 MSI 26-130-00 RTE:8

MSI 26-070-00 RTE:8

ATA: CM - 26

Page 1 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

ZONE ACCESS

CM2622 00010 APU FIRE EXTINGUISHING BOTTLE 000 P/N "ALL" NOTE( I, J ) NOTE (I): HYDROSTATIC TEST PRIOR TO ITS NEXT REFILL AFTER 60 MONTHS SINCE PREVIOUS HYDROSTATIC TEST NOTE (J): HYDROSTATIC TEST INCLUDES THE FUNCTIONAL CHECK OF THE FIRE BOTTLE PRESSURE SWITCH.

emp

CM2622 00020 CARTRIDGE, APU FIRE EXTINGUISHER 000 P/N "ALL" NOTE( I ) FOR CARTRIDGES MANUFACTURED PRIOR TO 07/1991 THE TOTAL LIFE IS REDUCED TO 78 MONTH.

emp

CM2623 00010 CARTRIDGE, CARGO FIRE EXTINGUISHER P/N "ALL"

emp

000

CM2626 00010 WATER FIRE EXTINGUISHER, PORTABLE P/N "ALL" NOTE( J ) TASK TO INCLUDE HYDROSTATIC TEST

000

CM2626 00020 HALON FIRE EXTINGUISHER 1.1KG, PORTABLE P/N "ALL" NOTE( J ) TASK TO INCLUDE HYDROSTATIC TEST.

000

Date: 23-jul-08

STRUCTURE

emp

THRESHOLD INTERVAL

REFERENCES MRB MRB

MRB

MRB

MRB

MRB

R L ITEM BY E E REVISION P V DATE

I: 120 OSM

O

HHI 737-700

5 30-nov-05

I: 132 OSM

Y

HHI 737-700

1 03-jun-04

I: 120 OSM

Y

HHI 737-700

2 03-jun-04

O

HHI 737-700

4 30-nov-05

O

HHI 737-700

4 30-nov-05

MSI 26-210-00 RTE:8

MSI 26-330-00 RTE:8

MSI 26-481-00

MSI 26-461-00 VENDOR I: 144 OSM RECOMMENDATION

ITEMS

EFF

MSI 26-181-0 MSI 26-260-00 RTE:8

VENDOR I: 60 OSM RECOMMENDATION emp

TSK

ATA: CM - 26

Page 2 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM CM - 27

DESCRIPTION

ZONE ACCESS

STRUCTURE

TSK

EFF

R L ITEM BY E E REVISION P V DATE

FLIGHT CONTROLS

CM2721 00010 RUDDER POWER CONTROL UNIT P/N 381500-1001 P/N 381500-1003 P/N S251A301-1 P/N S251A301-2 R CM2740 00020 STABILIZER TRIM ACTUATOR P/N 251A4510-6 AND ON

000

000

emp

emp

AAR

AD 99-11-05

AAR

LTA 1999-278

MRB

MSI 27-108-00 RTE:8 MSI 27-108-00 RTE:9

MRB R

Date: 23-jul-08

THRESHOLD INTERVAL

REFERENCES

MS SB

ITEMS

274181 01000 737-27A1277 R1 SB CONTAINS THE REQUIREMENT FOR OVERHAUL

I: 24000 FLH

F

HHI 737-700

2 30-nov-05

I: 25000 FLH

O

HHI 737-700

2 23-jul-08

ATA: CM - 27

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM CM - 28

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

EFF

R L ITEM BY E E REVISION P V DATE

FUEL

CM2822 00010 BATTERY ASSY, FUEL SHUTOFF P/N "ALL"

000

emp

MRB

MSI 28-130-00 RTE:9 I: 84 OPM

Date: 23-jul-08

TSK

ITEMS

ATA: CM - 28

O

HHI 737-700

1 03-jun-04

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM CM - 29

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

EFF

R L ITEM BY E E REVISION P V DATE

HYDRAULIC POWER

CM2900 00010 FUSE ASSY, HYDRAULIC B-SYSTEM RUDDER P/N "ALL"

R CM2900 00020 FUSE ASSY , LEADING EDGE STAND BY P/N "ALL"

000

000

emp

emp

MRB

MPD MRB

MSI 29-170-00 RTE:8

CM2900 00030 FUSE ASSY, A SYSTEM BRAKE P/N "ALL"

CM2911 00010 FUSE ASSY, B SYSTEM BRAKE P/N "ALL"

CM2921 00010 FUSE ASSY, EM DP - THRUST REVERSER A-SYSTEM P/N "ALL"

CM2921 00020 FUSE ASSY, STAND BY THRUST REVERSER P/N "ALL"

CM2999 00010 FUSE ASSY, NLG UP LINE P/N "ALL"

000

000

000

000

000

emp

emp

emp

emp

emp

ITEMS

MRB

MRB

MRB

MRB

MRB

I: 25000 FLH

F

HHI 737-700

1 03-jun-04

I: 25000 FLH

F

HHI 737-700

2 23-jul-08

I: 25000 FLH

F

HHI 737-700

1 03-jun-04

I: 25000 FLH

F

HHI 737-700

1 03-jun-04

I: 25000 FLH

F

HHI 737-700

1 03-jun-04

I: 25000 FLH

F

HHI 737-700

1 03-jun-04

I: 25000 FLH

F

HHI 737-700

1 03-jun-04

29-290-00 MSI 29-290-00 RTE:8

R

Date: 23-jul-08

TSK

MSI 29-160-00 RTE:8

MSI 29-150-00 RTE:8

MSI 29-130-00 RTE:8

MSI 29-300-00 RTE:8

MSI 29-120-00 RTE:8

ATA: CM - 29

Page 1 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

CM2999 00020 FUSE ASSY, NLG DOWN LINE P/N "ALL"

R CM2999 00030 FUSE ASSY, LEADING EDGE B-SYSTEM P/N "ALL"

ZONE ACCESS 000

000

STRUCTURE

emp

emp

R

Date: 23-jul-08

ITEMS

THRESHOLD INTERVAL

REFERENCES MRB

MPD MRB

TSK

EFF

R L ITEM BY E E REVISION P V DATE

MSI 29-110-00 RTE:8 I: 25000 FLH

F

HHI 737-700

0 03-jun-04

I: 25000 FLH

F

HHI 737-700

1 23-jul-08

29-140-00 MSI 29-140-00 RTE:8

ATA: CM - 29

Page 2 of 2


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM CM - 31

DESCRIPTION

ZONE ACCESS

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

INSTRUMENTS

CM3131 00010 UNDERWATER LOCATOR BEACON 000 P/N "ALL" NOTE( I, J ) NOTE (I): INTERVAL LIMIT ARE TO BE COMPUTED FROM BATTERY FABRICATION DATE. NOTE (J): TASK TO INCLUDE BATTERY REPLACEMENT.

Date: 23-jul-08

STRUCTURE

emp

MPD MPD MRB MRB MS

ITEMS

31-140-00 31-150-00 MSI 31-140-00 RTE:9 MSI 31-150-00 RTE:9 313109 70000

I: 72 OSM

ATA: CM - 31

O

HHI 737-700

2 03-jun-04

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM CM - 32

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

EFF

R L ITEM BY E E REVISION P V DATE

LANDING GEAR

R CM3211 00010 MAIN LANDING GEAR MAIN LANDING GEAR ASSY LH/RH P/N "ALL"

000

emp

MPD MPD MPD MPD MRB MRB MRB MRB

32-040-01 32-040-02 32-720-01 32-720-02 MSI 32-040-01 RTE:8 MSI 32-040-02 RTE:8 MSI 32-720-01 MSI 32-720-02

R

R CM3211 00020 MAIN LANDING GEAR STRUT ASSY - SIDE LH / RH P/N "ALL"

000

emp

MPD MPD MPD MPD MRB MRB MRB MRB

R

Date: 23-jul-08

TSK

ITEMS

I: 18000 CYC I: 120 OPM I: 21000 CYC

O

HHI 737-700

2 23-jul-08

I: 18000 CYC I: 120 OPM I: 21000 CYC

O

HHI 737-700

2 23-jul-08

32-040-01 32-040-02 32-720-01 32-720-02 MSI 32-040-01 RTE:8 MSI 32-040-02 RTE:8 MSI 32-720-01 MSI 32-720-02

ATA: CM - 32

Page 1 of 15


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

R CM3211 00030 MAIN LANDING GEAR STRUT ASSY - UPPER AND LOWER P/N "ALL"

ZONE ACCESS 000

STRUCTURE

emp

THRESHOLD INTERVAL

REFERENCES MPD MPD MPD MPD MRB MRB MRB MRB

000

emp

MPD MPD MPD MPD MRB MRB MRB MRB

R

Date: 23-jul-08

ITEMS

EFF

R L ITEM BY E E REVISION P V DATE

32-040-01 32-040-02 32-720-01 32-720-02 MSI 32-040-01 RTE:8 MSI 32-040-02 RTE:8 MSI 32-720-01 MSI 32-720-02

R

R CM3211 00040 MAIN LANDING GEAR LINK ASSY - UPPER LH / RH P/N "ALL"

TSK

I: 18000 CYC I: 120 OPM I: 21000 CYC

O

HHI 737-700

3 23-jul-08

I: 18000 CYC I: 120 OPM I: 21000 CYC

O

HHI 737-700

2 23-jul-08

32-040-01 32-040-02 32-720-01 32-720-02 MSI 32-040-01 RTE:8 MSI 32-040-02 RTE:8 MSI 32-720-01 MSI 32-720-02

ATA: CM - 32

Page 2 of 15


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

R CM3211 00050 MAIN LANDING GEAR LINK ASSY - LOWER P/N "ALL"

DESCRIPTION

ZONE ACCESS 000

STRUCTURE

emp

THRESHOLD INTERVAL

REFERENCES MPD MPD MPD MPD MRB MRB MRB MRB

000

emp

MPD MPD MPD MPD MRB MRB MRB MRB

R

Date: 23-jul-08

ITEMS

EFF

R L ITEM BY E E REVISION P V DATE

32-040-01 32-040-02 32-720-01 32-720-02 MSI 32-040-01 RTE:8 MSI 32-040-02 RTE:8 MSI 32-720-01 MSI 32-720-02

R

R CM3211 00060 MAIN LANDING GEAR LINK ASSY - REACTION P/N "ALL"

TSK

I: 18000 CYC I: 120 OPM I: 21000 CYC

O

HHI 737-700

2 23-jul-08

I: 18000 CYC I: 120 OPM I: 21000 CYC

O

HHI 737-700

2 23-jul-08

32-040-01 32-040-02 32-720-01 32-720-02 MSI 32-040-01 RTE:8 MSI 32-040-02 RTE:8 MSI 32-720-01 MSI 32-720-02

ATA: CM - 32

Page 3 of 15


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

R CM3211 00070 MAIN LANDING GEAR LINK ASSY - HANGER P/N "ALL"

DESCRIPTION

ZONE ACCESS 000

STRUCTURE

emp

THRESHOLD INTERVAL

REFERENCES MPD MPD MPD MPD MRB MRB MRB MRB

000

emp

MPD MPD MPD MPD MRB MRB MRB MRB

R

Date: 23-jul-08

ITEMS

EFF

R L ITEM BY E E REVISION P V DATE

32-040-01 32-040-02 32-720-01 32-720-02 MSI 32-040-01 RTE:8 MSI 32-040-02 RTE:8 MSI 32-720-01 MSI 32-720-02

R

R CM3211 00080 MAIN LANDING GEAR LINK ASSY - RETRACTION P/N "ALL"

TSK

I: 18000 CYC I: 120 OPM I: 21000 CYC

O

HHI 737-700

2 23-jul-08

I: 18000 CYC I: 120 OPM I: 21000 CYC

O

HHI 737-700

2 23-jul-08

32-040-01 32-040-02 32-720-01 32-720-02 MSI 32-040-01 RTE:8 MSI 32-040-02 RTE:8 MSI 32-720-01 MSI 32-720-02

ATA: CM - 32

Page 4 of 15


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

R CM3211 00090 MAIN LANDING GEAR BEAM ASSY - WALK. P/N "ALL"

ZONE ACCESS 000

STRUCTURE

emp

THRESHOLD INTERVAL

REFERENCES MPD MPD MPD MPD MRB MRB MRB MRB

000

emp

MPD MPD MPD MPD MRB MRB MRB MRB

000

emp

CMR

000

emp

CMR

ITEMS

O

HHI 737-700

2 23-jul-08

I: 18000 CYC I: 120 OPM I: 21000 CYC

O

HHI 737-700

2 23-jul-08

I: 45000 CYC

Y

HHI 737-700

0 17-oct-02

I: 45000 CYC

Y

HHI 737-700

0 17-oct-02

STRUCTURAL SAFE LIFE PARTS DRW 161A0002

Date: 23-jul-08

I: 18000 CYC I: 120 OPM I: 21000 CYC

STRUCTURAL SAFE LIFE PARTS DRW 161A0002

CM3211 03000 MLG INNER CYLINDER ASSY-SHOCK STRUT P/N "ALL"

R L ITEM BY E E REVISION P V DATE

32-040-01 32-040-02 32-720-01 32-720-02 MSI 32-040-01 RTE:8 MSI 32-040-02 RTE:8 MSI 32-720-01 MSI 32-720-02

R

CM3211 02000 MLG OUTER CYLINDER ASSY-SHOCK STRUT P/N "ALL"

EFF

32-040-01 32-040-02 32-720-01 32-720-02 MSI 32-040-01 RTE:8 MSI 32-040-02 RTE:8 MSI 32-720-01 MSI 32-720-02

R

R CM3211 00100 MAIN LANDING GEAR HOUSING ASSY P/N "ALL"

TSK

ATA: CM - 32

Page 5 of 15


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

CM3211 04000 MLG PIN - AXLE RETENTION P/N "ALL"

ZONE ACCESS 000

STRUCTURE

emp

THRESHOLD INTERVAL

REFERENCES CMR

000

emp

CMR

000

emp

CMR

000

emp

CMR

000

emp

CMR

000

emp

CMR

000

emp

CMR

ITEMS

I: 45000 CYC

Y

HHI 737-700

0 17-oct-02

I: 45000 CYC

Y

HHI 737-700

0 17-oct-02

I: 45000 CYC

Y

HHI 737-700

0 17-oct-02

I: 45000 CYC

Y

HHI 737-700

0 17-oct-02

I: 45000 CYC

Y

HHI 737-700

0 17-oct-02

I: 45000 CYC

Y

HHI 737-700

0 17-oct-02

STRUCTURAL SAFE LIFE PARTS DRW 161A0002

Date: 23-jul-08

0 17-oct-02

STRUCTURAL SAFE LIFE PARTS DRW 161A0002

CM3211 10000 MLG PIN - LWR TORSION LINK, P/N "ALL"

HHI 737-700

STRUCTURAL SAFE LIFE PARTS DRW 161A0002

CM3211 09000 MLG PIN - UPPER TORSION LINK, P/N "ALL"

Y

STRUCTURAL SAFE LIFE PARTS DRW 161A0002

CM3211 08000 MLG PIN - TORSION LINK APEX, P/N "ALL"

I: 45000 CYC

STRUCTURAL SAFE LIFE PARTS DRW 161A0002

CM3211 07000 MLG LOWER TORSION LINK ASSY, P/N "ALL"

R L ITEM BY E E REVISION P V DATE

STRUCTURAL SAFE LIFE PARTS DRW 161A0002

CM3211 06000 MLG UPPER TORSION LINK ASSY, P/N "ALL"

EFF

STRUCTURAL SAFE LIFE PARTS DRW 161A0002

CM3211 05000 MLG AXLE ASSY, P/N "ALL"

TSK

ATA: CM - 32

Page 6 of 15


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

CM3211 11000 MLG NUT - TORSION LINK APEX, P/N "ALL"

ZONE ACCESS 000

STRUCTURE

emp

THRESHOLD INTERVAL

REFERENCES CMR

000

emp

CMR

000

emp

CMR

000

emp

CMR

000

emp

CMR

000

emp

CMR

000

emp

CMR

ITEMS

I: 45000 CYC

Y

HHI 737-700

0 17-oct-02

I: 45000 CYC

Y

HHI 737-700

0 17-oct-02

I: 45000 CYC

Y

HHI 737-700

0 17-oct-02

I: 45000 CYC

Y

HHI 737-700

0 17-oct-02

I: 45000 CYC

Y

HHI 737-700

0 17-oct-02

I: 45000 CYC

Y

HHI 737-700

0 17-oct-02

STRUCTURAL SAFE LIFE PARTS DRW 161A0002

Date: 23-jul-08

0 17-oct-02

STRUCTURAL SAFE LIFE PARTS DRW 161A0002

CM3211 17000 MLG NUT - DAMPER, TORSION LINK APEX, P/N "ALL"

HHI 737-700

STRUCTURAL SAFE LIFE PARTS DRW 161A0002

CM3211 16000 MLG PIN - DAMPER, TORSION LINK APEX, P/N "ALL"

Y

STRUCTURAL SAFE LIFE PARTS DRW 161A0002

CM3211 15000 MLG PIN ASSY - AFT TRUNNION BEARING, P/N "ALL"

I: 45000 CYC

STRUCTURAL SAFE LIFE PARTS DRW 161A0002

CM3211 14000 MLG PIN - AFT TRUNNION CROSSBOLT, P/N "ALL"

R L ITEM BY E E REVISION P V DATE

STRUCTURAL SAFE LIFE PARTS DRW 161A0002

CM3211 13000 MLG PIN - FWD TRUNNION CROSSBOLT, P/N "ALL"

EFF

STRUCTURAL SAFE LIFE PARTS DRW 161A0002

CM3211 12000 MLG PIN ASSY - FWD TRUNNION BEARING, P/N "ALL"

TSK

ATA: CM - 32

Page 7 of 15


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

CM3211 18000 MLG UPPER SIDE STRUT ASSY, P/N "ALL"

ZONE ACCESS 000

STRUCTURE

emp

THRESHOLD INTERVAL

REFERENCES CMR

000

emp

CMR

000

emp

CMR

000

emp

CMR

000

emp

CMR

000

emp

CMR

000

emp

CMR

ITEMS

I: 45000 CYC

Y

HHI 737-700

0 17-oct-02

I: 45000 CYC

Y

HHI 737-700

0 17-oct-02

I: 45000 CYC

Y

HHI 737-700

0 17-oct-02

I: 45000 CYC

Y

HHI 737-700

0 17-oct-02

I: 45000 CYC

Y

HHI 737-700

0 17-oct-02

I: 45000 CYC

Y

HHI 737-700

0 17-oct-02

STRUCTURAL SAFE LIFE PARTS DRW 161A0002

Date: 23-jul-08

0 17-oct-02

STRUCTURAL SAFE LIFE PARTS DRW 161A0002

CM3211 24000 MLG PIN - SIDE STRUT TO REACTION LINK, P/N "ALL"

HHI 737-700

STRUCTURAL SAFE LIFE PARTS DRW 161A0002

CM3211 23000 MLG PIN - LOWER DOWN LOCK, P/N "ALL"

Y

STRUCTURAL SAFE LIFE PARTS DRW 161A0002

CM3211 22000 MLG PIN - SIDE STRUT ASSY APEX, P/N "ALL"

I: 45000 CYC

STRUCTURAL SAFE LIFE PARTS DRW 161A0002

CM3211 21000 MLG UPPER LOCK LINK ASSY, P/N "ALL"

R L ITEM BY E E REVISION P V DATE

STRUCTURAL SAFE LIFE PARTS DRW 161A0002

CM3211 20000 MLG LOWER DOWN LOCK LINK ASSY, P/N "ALL"

EFF

STRUCTURAL SAFE LIFE PARTS DRW 161A0002

CM3211 19000 MLG LOWER SIDE STRUT ASSY, P/N "ALL"

TSK

ATA: CM - 32

Page 8 of 15


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

CM3211 25000 MLG PIN - DOWNLOCK TO REACTION LINK, P/N "ALL"

ZONE ACCESS 000

STRUCTURE

emp

THRESHOLD INTERVAL

REFERENCES CMR

000

emp

CMR

000

emp

CMR

000

emp

CMR

000

emp

CMR

000

emp

CMR

000

emp

CMR

ITEMS

I: 45000 CYC

Y

HHI 737-700

0 17-oct-02

I: 45000 CYC

Y

HHI 737-700

0 17-oct-02

I: 45000 CYC

Y

HHI 737-700

0 17-oct-02

I: 45000 CYC

Y

HHI 737-700

0 17-oct-02

I: 45000 CYC

Y

HHI 737-700

0 17-oct-02

I: 45000 CYC

Y

HHI 737-700

0 17-oct-02

STRUCTURAL SAFE LIFE PARTS DRW 161A0002

Date: 23-jul-08

0 17-oct-02

STRUCTURAL SAFE LIFE PARTS DRW 161A0002

CM3211 31000 MLG PIN - REACTION LINK TO TRUNNION, P/N "ALL"

HHI 737-700

STRUCTURAL SAFE LIFE PARTS DRW 161A0002

CM3211 30000 MLG PIN - OUTER CYLINDER SIDE STRUT, P/N "ALL"

Y

STRUCTURAL SAFE LIFE PARTS DRW 161A0002

CM3211 29000 MLG PIN - SIDE OF BODY JOINT, P/N "ALL"

I: 45000 CYC

STRUCTURAL SAFE LIFE PARTS DRW 161A0002

CM3211 28000 MLG PIN - OUTBOARD DOWNLOCK SPRING ASSY, P/N "ALL"

R L ITEM BY E E REVISION P V DATE

STRUCTURAL SAFE LIFE PARTS DRW 161A0002

CM3211 27000 MLG PIN - DOWNLOCK ACTUATOR, P/N "ALL"

EFF

STRUCTURAL SAFE LIFE PARTS DRW 161A0002

CM3211 26000 MLG PIN - DOWNLOCK APEX, P/N "ALL"

TSK

ATA: CM - 32

Page 9 of 15


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

CM3211 32000 MLG REACTION LINK ASSY, P/N "ALL"

ZONE ACCESS 000

STRUCTURE

emp

THRESHOLD INTERVAL

REFERENCES CMR

000

emp

CMR

000

emp

CMR

000

emp

CMR

000

emp

CMR

000

emp

CMR

000

emp

CMR

ITEMS

I: 45000 CYC

Y

HHI 737-700

0 17-oct-02

I: 45000 CYC

Y

HHI 737-700

0 17-oct-02

I: 45000 CYC

Y

HHI 737-700

0 17-oct-02

I: 45000 CYC

Y

HHI 737-700

0 17-oct-02

I: 45000 CYC

Y

HHI 737-700

0 17-oct-02

I: 45000 CYC

Y

HHI 737-700

0 17-oct-02

STRUCTURAL SAFE LIFE PARTS DRW 161A0002

Date: 23-jul-08

0 17-oct-02

STRUCTURAL SAFE LIFE PARTS DRW 161A0002

CM3211 38000 MLG PIN - LINK ASSY ATTACHMENT, P/N "ALL"

HHI 737-700

STRUCTURAL SAFE LIFE PARTS DRW 161A0002

CM3211 37000 MLG PIN - WALKING BEAM ASSY, P/N "ALL"

Y

STRUCTURAL SAFE LIFE PARTS DRW 161A0002

CM3211 36000 MLG RETRACTION LINK ASSY, P/N "ALL"

I: 45000 CYC

STRUCTURAL SAFE LIFE PARTS DRW 161A0002

CM3211 35000 MLG RETRACTION WALKING BEAM, P/N "ALL"

R L ITEM BY E E REVISION P V DATE

STRUCTURAL SAFE LIFE PARTS DRW 161A0002

CM3211 34000 MLG PIN - HANGER LINK TO REACTION LINK, P/N "ALL"

EFF

STRUCTURAL SAFE LIFE PARTS DRW 161A0002

CM3211 33000 MLG HANGER LINK ASSY, P/N "ALL"

TSK

ATA: CM - 32

Page 10 of 15


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

CM3211 39000 MLG PIN - RETRACT ACTUATOR ATTACHMENT, P/N "ALL"

ZONE ACCESS 000

STRUCTURE

emp

THRESHOLD INTERVAL

REFERENCES CMR

000

emp

CMR

000

emp

MPD MPD MRB MRB

CM3221 00020 NOSE LANDING GEAR STRUT ASSY LOWER P/N "ALL"

000

emp

MPD MPD MRB MRB

CM3221 00030 NOSE LANDING GEAR LINK ASSY LOCK P/N "ALL"

000

emp

MPD MPD MRB MRB

CM3221 01040 AFT LOCK LINK P/N 162A2115-2 (NEXT HIGHER ASSY P/N 162A2115-3)

Date: 23-jul-08

000

emp

ITEMS

AAR

R L ITEM BY E E REVISION P V DATE

I: 45000 CYC

Y

HHI 737-700

0 17-oct-02

I: 45000 CYC

Y

HHI 737-700

0 17-oct-02

I: 18000 CYC I: 120 OPM

O

HHI 737-700

1 03-jun-04

I: 18000 CYC I: 120 OPM

O

HHI 737-700

1 03-jun-04

I: 18000 CYC I: 120 OPM

O

HHI 737-700

1 03-jun-04

I: 4200 CYC

Y

HHI 737-700

1 12-jun-01

STRUCTURAL SAFE LIFE PARTS DRW 161A0002

CM3221 00010 NOSE LANDING GEAR NOSE GEAR COMPONENT P/N "ALL"

EFF

STRUCTURAL SAFE LIFE PARTS DRW 161A0002

CM3211 40000 MLG PIN - WALKING BEAM ATTACHMENT, P/N "ALL"

TSK

32-090-00 32-750-00 MSI 32-090-00 RTE:8 MSI 32-750-00

32-090-00 32-750-00 MSI 32-090-00 RTE:8 MSI 32-750-00

32-090-00 32-750-00 MSI 32-090-00 RTE:8 MSI 32-750-00

CMR MPD PAGE 9.0-50

ATA: CM - 32

Page 11 of 15


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

CM3221 02000 NLG PIN - LEFT TRUNNION, P/N "ALL"

ZONE ACCESS 000

STRUCTURE

emp

THRESHOLD INTERVAL

REFERENCES CMR

000

emp

CMR

000

emp

CMR

000

emp

CMR

000

emp

CMR

000

emp

CMR

000

emp

CMR

ITEMS

I: 75000 CYC

Y

HHI 737-700

0 17-oct-02

I: 75000 CYC

Y

HHI 737-700

0 17-oct-02

I: 75000 CYC

Y

HHI 737-700

0 17-oct-02

I: 75000 CYC

Y

HHI 737-700

0 17-oct-02

I: 75000 CYC

Y

HHI 737-700

0 17-oct-02

I: 75000 CYC

Y

HHI 737-700

0 17-oct-02

STRUCTURAL SAFE LIFE PARTS DRW 162A0002

Date: 23-jul-08

0 17-oct-02

STRUCTURAL SAFE LIFE PARTS DRW 162A0002

CM3221 08000 NLG UPPER TORSION LINK ASSY, P/N "ALL"

HHI 737-700

STRUCTURAL SAFE LIFE PARTS DRW 162A0002

CM3221 07000 NLG PIN - TORSION LINK APEX, P/N "ALL"

Y

STRUCTURAL SAFE LIFE PARTS DRW 162A0002

CM3221 06000 NLG PIN - UPPER AND LOWER TORSION LINK, P/N "ALL"

I: 75000 CYC

STRUCTURAL SAFE LIFE PARTS DRW 162A0002

CM3221 05000 NLG INNER CYLINDER, P/N "ALL"

R L ITEM BY E E REVISION P V DATE

STRUCTURAL SAFE LIFE PARTS DRW 162A0002

CM3221 04000 NLG OUTER CYLINDER, P/N "ALL"

EFF

STRUCTURAL SAFE LIFE PARTS DRW 162A0002

CM3221 03000 NLG PIN - RIGHT TRUNNION, P/N "ALL"

TSK

ATA: CM - 32

Page 12 of 15


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

CM3221 09000 NLG LOWER TORSION LINK ASSY, P/N "ALL"

ZONE ACCESS 000

STRUCTURE

emp

THRESHOLD INTERVAL

REFERENCES CMR

000

emp

CMR

000

emp

CMR

000

emp

CMR

000

emp

CMR

000

emp

CMR

000

emp

CMR

ITEMS

I: 75000 CYC

Y

HHI 737-700

0 17-oct-02

I: 75000 CYC

Y

HHI 737-700

0 17-oct-02

I: 75000 CYC

Y

HHI 737-700

0 17-oct-02

I: 75000 CYC

Y

HHI 737-700

0 17-oct-02

I: 75000 CYC

Y

HHI 737-700

0 17-oct-02

I: 75000 CYC

Y

HHI 737-700

0 17-oct-02

STRUCTURAL SAFE LIFE PARTS DRW 162A0002

Date: 23-jul-08

0 17-oct-02

STRUCTURAL SAFE LIFE PARTS DRW 162A0002

CM3221 15000 NLG LOWER DRAG STRUT, P/N "ALL"

HHI 737-700

STRUCTURAL SAFE LIFE PARTS DRW 162A0002

CM3221 14000 NLG UPPER DRAG STRUT, P/N "ALL"

Y

STRUCTURAL SAFE LIFE PARTS DRW 162A0002

CM3221 13000 NLG STEERING PLATE, P/N "ALL"

I: 75000 CYC

STRUCTURAL SAFE LIFE PARTS DRW 162A0002

CM3221 12000 NLG PIN STRG COLLAR ATTACH, P/N "ALL"

R L ITEM BY E E REVISION P V DATE

STRUCTURAL SAFE LIFE PARTS DRW 162A0002

CM3221 11000 NLG STEERING SLEEVE, P/N "ALL"

EFF

STRUCTURAL SAFE LIFE PARTS DRW 162A0002

CM3221 10000 NLG STEERING COLLAR, P/N "ALL"

TSK

ATA: CM - 32

Page 13 of 15


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

CM3221 16000 NLG FWD LOCK LINK, P/N "ALL"

ZONE ACCESS 000

STRUCTURE

emp

THRESHOLD INTERVAL

REFERENCES CMR

000

emp

CMR

000

emp

CMR

000

emp

CMR

000

emp

CMR

000

emp

CMR

Date: 23-jul-08

000

emp

ITEMS

MRB

0 17-oct-02

I: 75000 CYC

Y

HHI 737-700

1 03-jun-04

I: 75000 CYC

Y

HHI 737-700

0 17-oct-02

I: 75000 CYC

Y

HHI 737-700

0 17-oct-02

I: 75000 CYC

Y

HHI 737-700

0 17-oct-02

I: 75000 CYC

Y

HHI 737-700

0 17-oct-02

I: 25000 FLH

F

HHI 737-700

1 22-mar-07

STRUCTURAL SAFE LIFE PARTS DRW 162A0002

CM3232 00010 MLG WHEEL WELL PROTECTION FUSE P/N "ALL"

HHI 737-700

STRUCTURAL SAFE LIFE PARTS DRW 162A0002

CM3221 21000 NLG PIN - DRAG STRUT ASSY, P/N "ALL"

Y

STRUCTURAL SAFE LIFE PARTS DRW 162A0002

CM3221 20000 NLG PIN - DRAG STRUT TRUNNION, P/N "ALL"

I: 75000 CYC

STRUCTURAL SAFE LIFE PARTS DRW 162A0002

CM3221 19000 NLG PIN - LOCK LINK APEX, P/N "ALL"

R L ITEM BY E E REVISION P V DATE

STRUCTURAL SAFE LIFE PARTS DRW 162A0002

CM3221 18000 NLG LOCK LINK SHAFT, P/N "ALL"

EFF

STRUCTURAL SAFE LIFE PARTS DRW 162A0002

CM3221 17000 NLG AFT LOCK LINK, P/N "ALL EXCEPT 162A2115-2

TSK

MSI 32-230-00 RTE:6

ATA: CM - 32

Page 14 of 15


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

CM3241 00020 WHEEL MAIN LANDING GEAR P/N "ALL" NOTE( I ) OVERHAUL AT EACH TIRECHANGE

CM3241 00030 WHEEL NOSE LANDING GEAR P/N "ALL" NOTE( I ) OVERHAUL AT EACH TIRECHANGE

Date: 23-jul-08

ZONE ACCESS 000

STRUCTURE

emp

MRB MRB

000

emp

ITEMS

THRESHOLD INTERVAL

REFERENCES

MRB

TSK

EFF

R L ITEM BY E E REVISION P V DATE

MSI 32-380-01 RTE:9 MSI 32-380-02 RTE:9 I: 1 s.N

O

HHI 737-700

1 03-jun-04

I: 1 s.N

O

HHI 737-700

1 03-jun-04

MSI 32-380-00 RTE:9

ATA: CM - 32

Page 15 of 15


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM CM - 33

DESCRIPTION

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

AIRCRAFT LIGHTING SYSTEM

R CM3351 00010 BATTERY PACK, EMERGENCY LIGHTS P/N AD-D717-01-100 P/N D 717-01-100 R

Date: 23-jul-08

ZONE ACCESS

000

emp

MRB

MSI 33-060-00 RTE:8 I: 24 OPM

ITEMS

ATA: CM - 33

O F

HHI 737-700

5 23-jul-08

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM CM - 34

DESCRIPTION

ZONE ACCESS

STRUCTURE

TSK

EFF

R L ITEM BY E E REVISION P V DATE

NAVIGATION

CM3410 00010 ALTIMETER, STAND-BY AND AIRSPEED P/N "ALL" N CM3453 00010 TRANSPONDER ATC, TPR-900 P/N "ALL"

000

000

emp

emp

N

Date: 23-jul-08

THRESHOLD INTERVAL

REFERENCES

ITEMS

empty

AAR

NFL II - 23/03

AAR

FAR 91.413 PART 43, APPEND. F

AAR

NFL II - 23/03

I: 24 OSM

F

HHI 737-700

2 29-apr-03

I: 12 MTH

F

HHI 737-700

0 23-jul-08

ATA: CM - 34

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM CM - 35

DESCRIPTION

ZONE ACCESS

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

OXYGEN

CM3510 00010 FF/QD MASK WITH REGULATOR P/N "ALL"

000

CM3512 00010 CYLINDER ASSY, OXYGEN, 115 CU/FT P/N "ALL" NOTE( J ) TASK TO INCLUDE HYDROSTATIC TEST

000

CM3512 01010 CYLINDER ASSY, OXYGEN, 115 CU/FT P/N "ALL" NOTE( I ) LIFE LIMIT 288 MTH REQUIRED BY DOT

000

CM3522 00110 GENERATOR, OXYGEN P/N "ALL"

000

R CM3531 00010 RESTORE PORTABLE OXYGEN CYLINDER ASSY P/N "ALL" NOTE( J ) R TASK TO INCLUDE HYDROSTATIC TEST

Date: 23-jul-08

STRUCTURE

000

emp

emp

emp

emp

emp

ITEMS

MPD MRB

AAR MRB

AAR MRB

MRB

AAR MRB

35-020-00 MSI 35-020-00 RTE:8 I: 16000 FLH

F

HHI 737-700

1 03-jun-04

I: 36 OSM

O

HHI 737-700

4 30-nov-05

I: 288 OSM

Y

HHI 737-700

1 03-jun-04

I: 144 OSM

Y

HHI 737-700

1 03-jun-04

I: 60 OSM

O

HHI 737-700

4 23-jul-08

49 CFR § 180.205 MSI 35-031-00

DOT MSI 35-040-00 RTE:8

MSI 35-070-00 RTE:9

49 CFR § 180.205 MSI 35-111-00

ATA: CM - 35

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM CM - 36

DESCRIPTION

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

PNEUMATIC

CM3610 00010 FUNCTIONALLY CHECK THE RIGHT AND LEFT PRECOOLER VALVE SENSOR. P/N "ALL"

CM3610 00020 FUNCTIONALLY CHECK THE PRECOOLER CONTROL VALVE AND SOLENOID P/N "ALL"

Date: 23-jul-08

ZONE ACCESS

000

emp

MRB MRB

000

emp

MRB MRB

ITEMS

MSI 36-030-01 RTE:8 MSI 36-030-02 RTE:8 I: 16000 FLH

F

HHI 737-700

2 18-mar-05

I: 16000 FLH

F

HHI 737-700

2 03-jun-04

MSI 36-020-01 RTE:8 MSI 36-020-02 RTE:8

ATA: CM - 36

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM CM - 49

DESCRIPTION

ZONE ACCESS

STRUCTURE

TSK

EFF

R L ITEM BY E E REVISION P V DATE

AUXILIARY POWER

R CM4900 01010 ENGINE COMPRESSOR IMPELLER NOTE( I ) INTERVAL IS 30000 APU CYCLES

000

emp

MPD MRB

R R CM4900 01020 FIRST STAGE TURBINE DISK NOTE( I ) INTERVAL IS 30000 APU CYCLES

R CM4900 01030 SECOND STAGE TURBINE ROTOR NOTE( I ) INTERVAL IS 30000 APU CYCLES

000

emp

MPD MRB

000

emp

MPD MRB

emp

R

MPD MRB

HHI 737-700

4 23-jul-08

I: 1 s.N

Y

HHI 737-700

3 23-jul-08

I: 1 s.N

Y

HHI 737-700

3 23-jul-08

I: 1 s.N

Y

HHI 737-700

3 23-jul-08

49-082-00 MSI 49-082-00 RTE:7 EM 49-00-00

ITEMS

Y

49-072-00 MSI 49-072-00 RTE:7 EM 49-00-00

000

I: 1 s.N

49-062-00 MSI 49-062-00 RTE:7 EM 49-00-00

R R CM4900 01040 TURBINE SHAFT NOTE( I ) INTERVAL IS 30000 APU CYCLES

49-052-00 MSI 49-052-00 RTE:7 EM 49-00-00

R

Date: 23-jul-08

THRESHOLD INTERVAL

REFERENCES

ATA: CM - 49

Page 1 of 1


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM CM - 72

DESCRIPTION

ZONE ACCESS

STRUCTURE

THRESHOLD INTERVAL

REFERENCES

EFF

R L ITEM BY E E REVISION P V DATE

ENGINE

R CM7200 20010 CFM56-7B22 & B24 FAN ROTOR PARTS FAN DISK P/N 340-000-410-0 NOTE( )

000

emp

AAR MRB MRB

ESM 05-11-01 MSI 72-030-01 RTE:5 MSI 72-030-02 RTE:5

R CM7200 20020 CFM56-7B22 & B24 FAN ROTOR PARTS BOOSTER SPOOL P/N 340-000-816-0

CM7200 20030 CFM56-7B22 & B24 FAN ROTOR PARTS FAN SHAFT P/N 335-006-414-0

CM7200 20040 CFM56-7B22 & B24 COMPRESSOR ROTOR PARTS FORWARD SHAFT P/N 1386M56P03

Date: 23-jul-08

TSK

000

emp

AAR MRB MRB

000

emp

AAR MRB MRB

000

emp

AAR MRB MRB

ITEMS

I: 1 s.N I: 17900 CYC

Y

HHI 737-700

4 23-jul-08

I: 23600 CYC

Y

HHI 737-700

3 22-mar-07

I: 30000 CYC

Y

HHI 737-700

3 22-mar-07

I: 20000 CYC

Y

HHI 737-700

2 18-mar-05

ESM 05-11-01 MSI 72-040-01 RTE:5 MSI 72-040-02 RTE:5

ESM 05-11-01 MSI 72-050-01 RTE:5 MSI 72-050-02 RTE:5

ESM 05-11-02 MSI 72-160-01 RTE:5 MSI 72-160-02 RTE:5

ATA: CM - 72

Page 1 of 6


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

CM7200 20050 CFM56-7B22 & B24 COMPRESSOR ROTOR PARTS STAGE 1 - 2 SPOOL P/N 1558M31G04

ZONE ACCESS 000

STRUCTURE

emp

AAR MRB MRB

CM7200 20051 CFM56-7B22 & B24 COMPRESSOR ROTOR PARTS STAGE 1-2 SPOOL P/N 1558M31G07

000

R CM7200 20060 CFM56-7B22 & B24 COMPRESSOR ROTOR PARTS STAGE 3 DISK P/N 1590M59P01 P/N 2116M23P01

000

emp

emp

THRESHOLD INTERVAL

REFERENCES

emp

CMM

05-11-02

AAR MRB

ESM 05-11-02 MSI 72-140-01 RTE:5 MSI 72-140-02 RTE:5

AAR MRB MRB

Date: 23-jul-08

000

emp

AAR MRB MRB

ITEMS

I: 20000 CYC

Y

HHI 737-700

3 22-mar-07

I: 20000 CYC

Y

HHI 737-700

0 22-mar-07

I: 20000 CYC

Y

HHI 737-700

3 23-jul-08

I: 20000 CYC

Y

HHI 737-700

4 23-jul-08

I: 1 s.N I: 20000 CYC

Y

HHI 737-700

5 23-jul-08

ESM 05-11-02 MSI 72-150-01 RTE:5 MSI 72-150-02 RTE:5

R R CM7200 20080 CFM56-7B22 & B24 COMPRESSOR ROTOR PARTS COMP REAR (CDP) AIR SEAL P/N 1523M35P01 P/N 2116M25P01 NOTE( ) R

R L ITEM BY E E REVISION P V DATE

empty

MRB

000

EFF

ESM 05-11-02 MSI 72-130-01 RTE:5 MSI 72-130-02 RTE:5

R R CM7200 20070 CFM56-7B22 & B24 COMPRESSOR ROTOR PARTS STAGE 4 - 9 SPOOL P/N 1588M89G03 P/N 2048M20G03

TSK

ESM 05-11-02 MSI 72-170-01 RTE:5 MSI 72-170-02 RTE:5

ATA: CM - 72

Page 2 of 6


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

R CM7200 20090 CFM56-7B22 & B24 HIGH PRESSURE TURBINE (HPT) ROTOR PARTS FRONT SHAFT P/N 1873M73P01 P/N 2048M21P03

ZONE ACCESS 000

STRUCTURE

emp

THRESHOLD INTERVAL

REFERENCES AAR MRB MRB

000

emp

AAR MRB MRB

000

R CM7200 20120 CFM56-7B22 & B24 HIGH PRESSURE TURBINE (HPT) ROTOR PARTS REAR SHAFT P/N 1498M45P06 P/N 1498M90P04 NOTE( ) R

000

Date: 23-jul-08

emp

AAR MRB MRB

emp

AAR MRB MRB

ITEMS

R L ITEM BY E E REVISION P V DATE

I: 20000 CYC

Y

HHI 737-700

4 23-jul-08

I: 20000 CYC

Y

HHI 737-700

4 23-jul-08

I: 1 s.N I: 20000 CYC

Y

HHI 737-700

5 23-jul-08

I: 1 s.N I: 20000 CYC

Y

HHI 737-700

4 23-jul-08

ESM 05-11-03 MSI 72-230-01 RTE:5 MSI 72-230-02 RTE:5

R R CM7200 20110 CFM56-7B22 & B24 HIGH PRESSURE TURBINE (HPT) ROTOR PARTS DISK P/N 1498M43P04 P/N 1498M43P06 P/N 1498M43P07 R NOTE( )

EFF

ESM 05-11-03 MSI 72-220-01 RTE:5 MSI 72-220-02 RTE:5

R R CM7200 20100 CFM56-7B22 & B24 HIGH PRESSURE TURBINE (HPT) ROTOR PARTS FRONT AIR SEAL P/N 1795M36P02 P/N 2116M20P02

TSK

ESM 05-11-03 MSI 72-240-01 RTE:5 MSI 72-240-02 RTE:5

ESM 05-11-03 MSI 72-250-01 RTE:5 MSI 72-250-02 RTE:5

ATA: CM - 72

Page 3 of 6


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

CM7200 20130 CFM56-7B22 & B24 LOW PRESSURE TURBINE (LPT) ROTOR PARTS STAGE 1 DISK P/N 336-001-804-0

CM7200 20140 CFM56-7B22 & B24 LOW PRESSURE TURBINE (LPT) ROTOR PARTS STAGE 2 DISK P/N 336-001-909-0

CM7200 20150 CFM56-7B22 & B24 LOW PRESSURE TURBINE (LPT) ROTOR PARTS STAGE 3 DISK P/N 336-002-006-0

CM7200 20160 CFM56-7B22 & B24 LOW PRESSURE TURBINE (LPT) ROTOR PARTS STAGE 4 DISK P/N 336-002-105-0

Date: 23-jul-08

ZONE ACCESS 000

STRUCTURE

emp

AAR MRB MRB

000

emp

AAR MRB MRB

000

emp

AAR MRB MRB

000

emp

AAR MRB MRB

ITEMS

THRESHOLD INTERVAL

REFERENCES

TSK

EFF

R L ITEM BY E E REVISION P V DATE

ESM 05-11-04 MSI 72-290-01 RTE:5 MSI 72-290-02 RTE:5 I: 25000 CYC

Y

HHI 737-700

2 18-mar-05

I: 25000 CYC

Y

HHI 737-700

2 18-mar-05

I: 25000 CYC

Y

HHI 737-700

2 18-mar-05

I: 25000 CYC

Y

HHI 737-700

2 18-mar-05

ESM 05-11-04 MSI 72-290-01 RTE:5 MSI 72-290-02 RTE:5

ESM 05-11-04 MSI 72-290-01 RTE:5 MSI 72-290-02 RTE:5

ESM 05-11-04 MSI 72-290-01 RTE:5 MSI 72-290-02 RTE:5

ATA: CM - 72

Page 4 of 6


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

ZONE ACCESS

CM7200 20170 CFM56-7B22 & B24 LOW PRESSURE TURBINE (LPT) ROTOR PARTS LPT SHAFT P/N 340-074-705-0 P/N 340-074-720-0 P/N 340-074-722-0

000

CM7200 20180 CFM56-7B22 & B24 LOW PRESSURE TURBINE (LPT) ROTOR PARTS LPT ROTOR SUPPORT P/N 338-077-502-0

000

emp

emp

AAR MRB

AAR MRB MRB

000

R CM7200 20210 CFM56-7B22 LOW PRESSURE TURBINE (LPT) STATOR PARTS R LPT REAR FRAME P/N 340-027-115-0 P/N 340-027-121-0

000

R CM7200 20230 CFM56-7B LOW PRESSURE TURBINE (LPT) STATOR PARTS LPT REAR FRAME P/N 340-166-205-0 P/N 340-166-206-0 R P/N 340-166-207-0 P/N 340-166-208-0 P/N 340-166-209-0 P/N 340-166-210-0

000

emp

emp

emp

ITEMS

THRESHOLD INTERVAL

REFERENCES

MRB

CM7200 20200 CFM56-7B22 LOW PRESSURE TURBINE (LPT) STATOR PARTS LPT REAR FRAME P/N 340-027-113-0

Date: 23-jul-08

STRUCTURE

AAR

AAR

TSK

EFF

R L ITEM BY E E REVISION P V DATE

ESM 05-11-04 MSI 72-280-01 RTE:5 MSI 72-280-02 RTE:5 I: 20000 CYC

Y

HHI 737-700

3 22-mar-07

I: 25000 CYC

Y

HHI 737-700

2 18-mar-05

I: 25000 CYC

Y

HHI 737-700

0 11-jan-01

I: 24200 CYC

Y

HHI 737-700

2 23-jul-08

T: 25000 CYC I: 4700 CYC

Y

HHI 737-700

1 23-jul-08

ESM 05-11-04 MSI 72-270-01 RTE:5 MSI 72-270-02 RTE:5

ESM 05-12-04

ESM 05-12-04

AAR AAR AAR AAR

2008-03-09 EAD 2007-0104 ESM 05-12-04 05-12-04

SB

72-0579

ATA: CM - 72

Page 5 of 6


HHI R E V

737-6

MAINTENANCE SCHEDULE ITEM

DESCRIPTION

N CM7200 20240 CFM56-7B22 & B24 HIGH PRESSURE TURBINE (HPT) ROTOR PARTS REAR SHAFT P/N 1498M45P07

ZONE ACCESS 000

STRUCTURE

emp

Date: 23-jul-08

AAR MRB MRB

N

THRESHOLD INTERVAL

REFERENCES

EFF

R L ITEM BY E E REVISION P V DATE

ESM 05-11-03 MSI 72-250-01 RTE:5 MSI 72-250-02 RTE:5 I: 11500 CYC

ITEMS

TSK

ATA: CM - 72

Y

HHI 737-700

0 23-jul-08

Page 6 of 6

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