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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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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

Page: 3 of 3


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

Page 1 of 2


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

Page 5 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- 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

Page 6 of 23


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

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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

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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

Page 11 of 23


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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

HIGHLIGHTS

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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

Page 14 of 23


HHI

MAINTENANCE SCHEDULE ITEM

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

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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

Page 19 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 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

737-6

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.

Date: 23-Jul-2008

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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

737-6

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

737-6

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.

Date: 23-Jul-2008

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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

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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

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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

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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

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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

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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

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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

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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

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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

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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