14 5 mccauley f 7 performance parte g

METRO III ICAO ANNEX 8 PART G – APPROACH AND LANDING PERFORMANCE CONTENTS ITEM

PAGE

Maximum Landing Weight Limitation Chart Bleed Air On .............................................................................................................................. 4G-2 Bleed Air Off .............................................................................................................................. 4G-3 Balked Landing Rate of Climb – Bleed Air On ................................................................................... 4G-4 Landing Distance Over 50 Foot Height B.F. Goodrich Single Rotor Brakes ........................................................................................... 4G-5 Goodyear Aerospace Dual Rotor Brakes .................................................................................. 4G-6 Landing Brake Energy Limits B.F. Goodrich Single Rotor Brakes ........................................................................................... 4G-7

FAA APPROVED: MAY 22/89

PERFORMANCE

4G-i 4MC

METRO III ICAO ANNEX 8

THIS PAGE LEFT BLANK INTENTIONALLY

4G-ii 4MC

PERFORMANCE

MANUFACTURER'S DATA ISSUED: MAY 22/89

METRO III ICAO ANNEX 8

THIS PAGE LEFT BLANK INTENTIONALLY

MANUFACTURER'S DATA FAA APPROVED: MAY 22/89 ISSUED: MAY 22/89

PERFORMANCE

4G-1 4MC

METRO III - ICAO ANNEX 8 MAXIMUM LANDING WEIGHT SINGLE ENGINE APPROACH ASSOCIATED

LIMITATION CHART CLIMB REQUIREMENT

EXAMPLE

CONDITIONS:

GIVEN:

POWER . . . .. . . . . . . .. . . . . . . .. . . . . . . . . . . . . . . . . . . . . TAKEOFF (DRY) PROPELLER .. . . . . . . .. . . .._.................

FEATHERED ON INOPERATIVE ENGINE GEN LOAD . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . .. . . 300 AMPS BLEED AIR . . .. . . . .. . .. .. . .. . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON . . . . . . . . . . . . . . . . . . . . . . . . . .. OFF (SEE NOTE) ENG ANTI-ICE CLIMB SPEEDS . . .. . . . . SEE LANDING APPROACH SPEEDS (FIGURE 4G4 OR 4G-5) AND GEAR . . . . .. . . . . . . .. . . . . . . . . . . . . . . . . . . . . . UP (APPROACH APPROACH CLIMB) FLAPS . . . . . . . . . . . .. . . . . . . .. .. . . . . .. . . . . . l/4 (APPROACH AND APPROACH CLIMB)

OBTAIN:

AIR ON

: OAT = 7°C PRESSURE ALTITUDE MAX LANDING WEIGHT

= 5,600 FEET = 13,750 POUNDS

(6240

kg)

NOTE l

l

l

FIGURE 4G-2 4MC

- BLEED

REDUCE MAXIMUM LANDING (435 kg) WITH ENGINE ANTI-ICE

WEIGHT ON.

MAXIMUM

ANTI-ICE

OAT

WITH

ENGINE

BY 960

ON

POUNDS

IS 5°C.

THIS WEIGHT RESULTS IN A MAXIMUM LANDING WEIGHT AT WHICH A CLIMB GRADIENT EQUAL TO OR GREATER THAN 2.1% CAN BE MAINTAINED IN THE CONFIGURATION STATED ABOVE WITH ONE ENGINE INOPERATIVE.

4G-1

PERFORMANCE

FAA APPROVED:

MAY 22189

METRO III - ICAO ANNEX 8 MAXIMUM LANDING WEIGHT SINGLE ENGINE APPROACH ASSOCIATED

LIMITATION CHART CLIMB REQUIREMENT

CONDITIONS:

POWER .........................................

TAKEOFF (DRY) GEN LOAD.. ................... .200 AMPS (SEE NOTE) BLEED AIR ........................................................

OFF ENG ANTI-ICE . . . . . . . . . . .. . . . .. . .. . . . .. . . OFF (SEE NOTE) CLIMB SPEEDS . . . . . . . . SEE LANDING APPROACH SPEEDS (FIGURE 4G-4 OR 4G-5) GEAR . . . . . . . . . . . . . . . .. . . . . . . .. . . . . . . . . . . UP (APPROACH AND APPROACH CLIMB) !=LAPS . . . . . . . . . . . . . . . . . . .. . . .. . . . .. . . . . . 114 (APPROACH AND APPROACH CLIMB)

- BLEED

EXAMPLE GIVEN: OBTAIN:

AIR OFF

: OAT = 16°C PRESSURE ALTITUDE MAX LANDING WEIGHT

= 5,600 FEET = 13,700 POUNDS

(6210

kg)

NOTE l

l

l

REDUCE MAXIMUM LANDING (385 kg) WITH ENGINE ANTI-ICE

WEIGHT ON.

MAXIMUM

ANTI-ICE

OAT

WITH

ENGINE

BY 850

ON

POUNDS

IS 5°C.

THIS WEIGHT RESULTS IN A MAXIMUM LANDING WEIGHT AT WHICH A CLIMB GRADIENT EQUAL TO OR GREATER THAN 2.1% CAN BE MAINTAINED IN THE CONFIGURATION STATED ABOVE WITH ONE ENGINE INOPERATIVE.

15

FIGURE FAA APPROVED:

MAY 22189

4G-2

PERFORMANCE

4G-3 4MC

METRO III - ICAO ANNEX 8 BALKED LANDING RATE OF CLIMB - BLEED AIR ON 60

ASSOC!ATED

CONDITIONS:

POWER . . . . . . . . . .._......... TAKEOFF (DRY) GEN LOAD . . . . . . . . .. . . . . . . . . . . . . . . . 3M) AMPS BLEED AIR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON ENG ANTI-ICE . . . . . . . OFF (SEE NOTE) CLIMB SPEED . . . . . . . . . SEE SCHEDULE GEAR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN FLAPS . . . . . . . ..I.............................

WWN EXAMPLE: GIVEN:

OBTAIN:

OAT - 10% PRESSURE ALTITUDE - 4.ooO FEET GROSS WEIGHT - 11$X POUNDS (5215 k9) CLIMB SPEED - 97 KIAS RATE OF CLIMB - 1.560 FEET PER MINUTE

. REDUCE RATE OF CLIMB BY 290 WITH ENGINE ANTCICE ON. * MAXIMUM

OAT

WITH

BALKED

ENGINE

LANDING SCHEDULE

ANTCICE CLIME (KIAS)

GROSS WEIGHT (POUNDS)

CLIMB SPEED (KIAS)

14,ca

102 100 97 96

12.m 10,003

FEET

PER

MINUTE

ON IS 5-C.

SPEED GROSS

WEIGHT w 6350 Ez 4500

6

500

1,000

1,500

2,000

2,500

3,000

3,500

RATE OF CLIMB (FEET PER MINUTE)

FIGURE 4G-4 4MC

4G-3

PERFORMANCE

FAA APPROVED:

MAY 22/89

LANDING DISTANCE OVER 50 FOOT HEIGHT B.F. GOODRICH SINGLE ROTOR BRAKES ASSOCIATED

CONDITIONS:

APPROACH SPEED . . . . . . .

SEE CHART POWER . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FLIGHT IDLE GEN LOAD . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED BLEED AIR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON OR OFF ENG ANTI-ICE . . . . . . . . . . . . . . . . . . . . ON OR OFF RUNWAY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DRY, LEVEL, HARD SURFACE GEAR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN FLAPS . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN BRAKING . . . .._ I-lEAVY DURING ROLLOUT ANTI-SKID . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON OR OFF NOSE WHEEL STEERlNG....ON OR OFF

EXAMPLE: GIVEN:

OBTAIN:

OAT = 18°C PRESSURE ALTITUDE = 7.000 FEET GROSS WEIGHT - 11,900 POUNDS (5400 kg) HEADWIND = 15 KNOTS APPROACH SPEED = 106 KIAS LANDING DISTANCE = 2,775 FEET (945 m)

LANDING

*

SINGLE ENGINE LANDING DISTANCES ARE SHOWN ALL CASES, ARE LONGER THAN TWO ENGINE DISTANCES.

-

IF APPLICABLE, SEE OPERATING OBTAIN REQUIRED FIELD LENGTH.

(1 DETERMINE THAT THE BRAKE ENERGY LIMIT NOT BE EXCEEDED FROM FIGURE 4G-6.

WILL

GROSS SO,00

WEIGHT 5500

GROUND

ROLL

NOTE IS 72%OF

*

LANDING

RULES

FOR

DISTANCE. AND, IN LANDING

FACTORS

TO

m -I 310 0

(kg) 5000

45po

4,000

12ot

z 8$

3,500 1000

E 3,000

-

g I.?

2 s* ii LA.

2.500

6 6 8 f ii E 4 9aJ

i2 cc F 0 Y

2,000

600

1,500 400

1,000

500 OAT (OC)

GROSS

WEIGHT

(POUNDS)

WIND

(KNOTS)

2 IE cl

P 53

-I c) D

0

D z z m X

00

$8 O&

LANDING DISTANCE OVER 50 FOOT HEIGHT GOODYEAR AEROSPACE DUAL ROTOR BRAKES ASSOCIATED

CONDITIONS:

APPROACH POWER

EXAMPLE:

SPEED . . .

. . . . . . . . SEE CHART 3” GLIDE PATH POWER AS REQUIRED GEN LOAD ,...........,..,.,_........ AS REQUIRED BLEED AIR . . . . . . . . . . . . ON OR OFF ENG ANTI-ICE . .._......_....... ON OR OFF RUNWAY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DRY, LEVEL, HARD SURFACE

GIVEN:

OBTAIN:

OAT = 19°C PRESSURE ALTITUDE = 7.000 FEET GROSS WEIGHT = 13.000 POUNDS (5900 kg) HEADWIND = 17.5 KNOTS APPROACH SPEED = 109 KIAS LANDING DISTANCE = 2.993 FEET (980 m)

FLAPS . . . . .._..__..__.__.............................. DOWN BRAKING HEAVY DURING ROLLOUT NOSE WHEEL STEERING . . . ..ON OR OFF

LANDING

*

TWO ENGINE LANDING DISTANCES CREASE LANDING DISTANCE BY 72% OPERATION.

-

IF APPLICABLE. SEE OPERATING OBTAIN REQUIRED FIELD LENGTH.

GROSS 65.00

6000

WEIGHT 5500

GROUND

ROLL

NOTE IS 62%OF

*

LANDING

RULES

DISTANCE.

ARE SHOWN. INFOR SINGLE ENGINE

FOR

FACTORS

TO

(kg) 5000

4500

600

-40

-20

0

20 OAT (OC)

40

60

14,000

13,000 GROSS

12,000 WEIGHT

11,000 (POUNDS)

10,000

0

10 WIND

(KNOTS)

20

-“-

FAA APPROVED:

4G-6 PERFORMANCE

FIGURE

METRO III - ICAO ANNEX 8

MAY 22189

4G-7 4MC

METRO III ICAO ANNEX 8

THIS PAGE LEFT BLANK INTENTIONALLY

4G-8 4MC

PERFORMANCE

MANUFACTURER'S FAA APPROVED: MAY DATA 22/89 ISSUED: MAY 22/89