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时间:2011-04-17 09:13来源:蓝天飞行翻译 作者:航空
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 75-31-00
 ALL  ú ú N02 Page 528 ú Jun 10/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
NUT  WASHER  LEVER BELLCRANK  SHOULDER BOLT 
COTTER PIN  ROD END BEARING 
KEY WASHER 
JAMNUT 
SEAL  ACTUATOR ROD 
INITIAL 9/16 INCH (14.3 mm) APPROXIMATELY ADJUSTMENT ONLY FLAT 
ADAPTER "SD" SEAL DRAIN 

C
L-A6528
Variable Stator Vane Actuator Rigging Figure 503 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

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 ALL  ú ú N01 Page 529 ú Jun 10/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
(2) PWA 86097 Pin - Rig, Pratt & Whitney
 NOTE: The PWA 85675 Rigging Pin Kit contains
____
 these rig pins.

 (3)  
PWA 49030 Cart - Hydraulic (Pneumatic), Pratt & Whitney (Optional to CTE5100)

 (4)  
CTE5100 Cart - Hydraulic (Pneumatic), Pratt & Whitney (Optional to PWA 49030)

 (5)
PWA 86317 Box - Electrical Switch

 B.
Consumable Materials

 (1)
D00390 Oil - Engine

 (2)
G00964 Compound - Antigalling, Fel-Pro C-200

 (3)
G00597 Fluid - Calibrating, MIL-C-7024, Type II

 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 78-31-00/201, Thrust Reverser System

 D.
Access

 (1)  
Location Zone 412 Engine 1 - HPC Fwd Case 3:30 o'clock 422 Engine 2 - HPC Fwd Case 3:30 o'clock 432 Engine 3 - HPC Fwd Case 3:30 o'clock 442 Engine 4 - HPC Fwd Case 3:30 o'clock

 (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 for the Adjustment

 (1)
Open the right fan cowl panel (AMM 71-11-04/201).


 S 015-071-N00
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 75-31-00
 ALL  ú ú N02 Page 530 ú Feb 10/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
S 045-119-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).


 S 015-072-N00

 (3)  
Open the right core cowl panel (AMM 71-11-06/201).


 S 015-084-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 025-120-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 AND COLLECT THE ENGINE FUEL. THE FUEL
 IS POISONOUS AND CAN 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
 
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