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时间:2011-04-17 09:17来源:蓝天飞行翻译 作者:航空
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 3)  Install lockwire or safety cable and safety cable ferrule on the tube nuts.
 (p)  At the rear of the No. 3 bearing oil pressure manifold (12), install a spray shield (4).
 NOTE: The spray shield goes to the inboard side of the
____
 manifold.

 1)  Attach the spray shield (4) with a clamp (2) and a bolt (1) to a bracket (3).
 NOTE: The bracket is attached to the flange of the cooling
____ air tube on the high compressor.
 a) Lubricate the threads of the bolt with engine oil. b) Torque the bolt to 36-40 pound-inches (4.067 - 4.519 newton meters).
 G.  Put the Airplane Back to Its Usual Condition.
 S 414-089-N00
 WARNING: OBEY THE INSTRUCTIONS IN THE PROCEDURE TO CLOSE THE THRUST
_______
 REVERSERS. IF YOU DO NOT OBEY THE INSTRUCTIONS, INJURIES TO
 PERSONS OR DAMAGE TO EQUIPMENT CAN OCCUR.

 (1)  
Close the left thrust reverser (AMM 78-31-00/201).

 (2)  
Close the left core cowl panel (AMM 71-11-06/201).

 (3)  
Close the left fan cowl panel (AMM 71-11-04/201).

 S 444-087-N00

 (4)  
Do the activation procedure for the thrust reverser
 (AMM 78-31-00/201).

 

 S 414-085-N00
 S 414-086-N00
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 79-21-16
 ALL  ú ú N01 Page 420 ú Jun 10/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
S 794-088-N00
 (5) Do the Test No. 3 - Ground Test - Idle Power (AMM 71-00-00/501).
 TASK 79-21-16-404-027-N00
 8. Install the Main and Angle Gearbox Last Chance Oil Strainer (Fig. 401)
___________________________________________________________
 A. Equipment
 (1)  
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)  
G02332 Ferrule, Safety Cable (P05-292)

 (3)  
G02334 Lockwire, (P05-289) 0.032 inch (0.813 mm) - AS3214-02

 (4)  
G02335 Cable, Safety (P05-291)

 C.
Parts


 ~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 401 | 3 | Strainer Element | 79-21-02 | 20 | 75 | | | 4 | Bolt | | | 70 | | | 5 | Packing | | | 80 | 2......…........…...................................…...........….....…........1
 D. References
 (1)  
AMM 71-00-00/501, Power Plant

 (2)  
AMM 71-11-04/201, Fan Cowl Panels

 (3)  
AMM 71-11-06/201, Core Cowl Panels

 (4)  
AMM 78-31-00/201, Thrust Reverser System

 E.
Access

 (1)  
Location Zone
 412 Engine 1 - HPC Case 9 o'clock
 422 Engine 2 - HPC Case 9 o'clock
 432 Engine 3 - HPC Case 9 o'clock
 442 Engine 4 - HPC Case 9 o'clock


 (2)  
Access Panel
 415 Left Thrust Reverser Half - Engine 1
 425 Left Thrust Reverser Half - Engine 2
 435 Left Thrust Reverser Half - Engine 3
 445 Left Thrust Reverser Half - Engine 4

 

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 79-21-16
 ALL  ú ú N01 Page 421 ú Jun 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
F. Procedure
 S 434-028-N00
 (1)  
Remove the protection cap.

 S 644-057-N00

 (2)  
Lubricate the packing (5) with engine oil.

 S 434-029-N00

 (3)  
Install the packing (5) to the groove at the bottom of the last chance oil strainer (3).


 
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