(8)
PWA 86197 Pin - Rig, Pratt and Whitney
(9)
M303, M305, or M307 Bergen Mechanical Crimper
Bergen Cable Technologies Inc
170 Gregg St
P.O. Box 1300
Lodi, NJ 07644-9982
B.
Consumable Materials
(1)
D00390 Oil - Engine
(2)
G00964 Compound - Antigalling, Fel-Pro C-200
(3)
G00597 Fluid - Calibrating, MIL-C-7024, Type II
(4)
G02334 Lockwire - AS3214-02
(5)
G02332 Ferrule - P05-292 (Optional)
(6)
G02335 Cable - Safety - P05-291 (Optional)
C.
References
(1)
AMM 70-24-05/201, Electrical Harnesses
(2)
AMM 71-00-00/501, Power Plant
(3)
AMM 71-11-04/201, Fan Cowl Panels
(4)
AMM 71-11-06/201, Core Cowl Panels
(5)
AMM 75-31-00/601, Compressor Stator Vane Control System
(6)
AMM 78-31-00/201, Thrust Reverser System
D.
Access
(1)
Location Zone
412 Engine 1 - HPC Fwd Case Right Side
422 Engine 2 - HPC Fwd Case Right Side
432 Engine 3 - HPC Fwd Case Right Side
442 Engine 4 - HPC Fwd Case Right Side
(2)
Access Panel
416 Right Thrust Reverser Half - Engine 1
426 Right Thrust Reverser Half - Engine 2
436 Right Thrust Reverser Half - Engine 3
446 Right Thrust Reverser Half - Engine 4
E.
Prepare the Aircraft
(1)
Open the right fan cowl panel (AMM 71-11-04/201).
S 015-107-N00
S 045-108-N00
WARNING: DO THE THRUST REVERSER DEACTIVATION PROCEDURE TO PREVENT THE
_______
OPERATION OF THE THRUST REVERSER. THE ACCIDENTAL OPERATION OF
THE THRUST REVERSER CAN CAUSE INJURIES TO PERSONS OR DAMAGE TO
EQUIPMENT.
(2) Do this procedure: Thrust Reverser Deactivation for Ground
Maintenance (AMM 78-31-00/201).
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75-31-00
ALL ú ú N02 Page 507 ú Jun 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
S 015-109-N00
(3) Open the right core cowl panel (AMM 71-11-06/201).
S 015-110-N00
WARNING: OBEY THE INSTRUCTIONS IN AMM 78-31-00 WHEN YOU OPEN THE THRUST
_______ REVERSERS. IF YOU DO NOT OBEY THE INSTRUCTIONS, INJURIES TO PERSONS OR DAMAGE TO EQUIPMENT CAN OCCUR.
(4)
Open the right thrust reverser (AMM 78-31-00/201).
F.
Procedure
S 025-112-N00
WARNING: DO NOT KEEP THE ENGINE FUEL ON YOUR SKIN FOR A LONG PERIOD OF
_______ TIME. PUT A CONTAINER, WITH A MINIMUM CAPACITY OF 5 GALLONS (19 LITERS) IN POSITION TO COLLECT THE FUEL. THE FUEL IS POISONOUS AND CAN BE ABSORBED THROUGH YOUR SKIN AND CAUSE INJURY.
WARNING: DO NOT PUT YOUR FINGERS NEAR THE LINKAGES, UNISON RINGS, OR
_______ LEVERS WHEN YOU OPERATE THE STATOR VANE SYSTEM. YOU CAN CAUSE INJURY TO YOUR HANDS IF YOU DO.
CAUTION:_______DO THIS ADJUSTMENT PROCEDURE WITH PRECISION. IF YOU DO NOT, THE HPC BLADE FATIGUE CAN INCREASE, INTERNAL ENGINE DAMAGE CAN OCCUR, OR POSSIBLE ENGINE FAILURE.
CAUTION: ALWAYS REMOVE THE RIG PINS BEFORE YOU MOVE THE STATOR VANE
_______ SYSTEM. IF YOU DO NOT DO THIS, DAMAGE TO THE STATOR VANE SYSTEM CAN OCCUR.
(1)
Remove the hydraulic tubes of the compressor stator:
(a)
Disconnect the hydraulic pressure tube of the compressor stator at the two ends.
(b)
Disconnect the hydraulic return tube of the compressor stator at the two ends.
(c)
Loosen the two clamp bolts which attach the hydraulic return tube and the hydraulic pressure tube.
(d)
Move the hydraulic pressure tube and the hydraulic return tube away from the actuator adapters.
(e)
Install the protection covers.
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本文链接地址：747-400 AMM 飞机维护手册 大气 AIR 2(23)
