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时间:2011-04-16 10:00来源:蓝天飞行翻译 作者:航空
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 (c)  Continue to motor the engine for five minutes.
 NOTE:____This will flow the engine oil through the engine. Make sure you do not operate the starter more than the starter operation time limits.
 S 862-101-N00
 (4)  
If you can start and operate the engine, do the Periodic Engine Run.

 S 862-102-N00

 (5)  
Do the engine shutdown procedure (AMM 71-00-00/201).

 S 032-103-N00

 (6)  
Remove the drain plugs from the bottom of the engine oil tank and the bottom of the main gearbox.


 (a)  Let the engine oil drain to a slow drip (approximately 30 minutes).
 S 432-104-N00
 (7)  
Install the drain plugs in the main gearbox and engine oil tank.

 S 032-105-N00

 (8)  
Remove the accessory drive pad covers from the main gearbox.

 S 622-106-N00

 (9)  
Spray the drive pads with engine oil.

 S 432-107-N00

 (10)
 Install the accessory drive pad covers on the main gearbox.

 S 972-108-N00

 (11)
 Make a record of the date of the preservation on a tag and attach it to the oil filler cap.


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 71-00-03
 ALL  ú ú N01 Page 207 ú Oct 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
TASK 71-00-03-632-046-N00
 3. Power Plant Depreservation
__________________________
 A. References
 (1)  
AMM 12-13-03/301, Engine Oil - Servicing

 (2)  
AMM 29-11-05/401, Engine Driven Pump

 (3)  
AMM 71-00-00/201, Power Plant

 (4)  
AMM 72-61-07/401, Hydraulic Pump Rear Drive Oil Seal

 (5)  
AMM 78-31-00/201, Thrust Reverser System

 B.
Access

 (1)  
Location Zone
 412 Engine 1
 422 Engine 2
 432 Engine 3
 442 Engine 4


 (2)  
Access Panel 415 and 416 Thrust Reverser Halves - Engine 1 425 and 426 Thrust Reverser Halves - Engine 2 435 and 436 Thrust Reverser Halves - Engine 3 445 and 446 Thrust Reverser Halves - Engine 4

 C.
Method I (8 to 30 Days)


 S 552-047-N00
 (1)  
Remove the cover from the engine, if it was installed.

 S 212-048-N00

 (2)  
Examine the main gearbox housing for corrosion caused by hydraulic fluid leaks.

 (a)  
If it is necessary, remove the hydraulic pump (AMM 29-11-05/401) to get better access to the main gearbox.

 (b)  
If any hydraulic fluid is found, replace the gearbox carbon seal (AMM 72-61-07/401).

 


 S 612-049-N00
 (3)  Do this task: "Engine Oil - Servicing (Oil Replenishing)" (AMM 12-13-03/301).
 NOTE: Do not do the Thrust Reverser Activation procedure after you
____ you do the oil servicing. This procedure will be done at a later time.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 71-00-03
 ALL  ú ú N01 Page 208 ú Oct 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
S 862-050-N00
 (4)  
Do the steps for the Periodic Engine Run in the task for the Power Plant Preservation (AMM 71-00-03/201).

 S 282-079-N00

 (5)  
If the oil system was not drained, do the steps in the Engine Oil Analysis in the Power Plant Preservation (AMM 71-00-03/201) to examine the oil for water and acid contamination.

 S 442-057-N00

 (6)  
Do this task: "Thrust Reverser Activation After the Ground Maintenance" (AMM 78-31-00/201).

 D.
Method II (31 to 90 Days)


 S 212-063-N00
 (1)  Examine the main gearbox housing for corrosion caused by hydraulic fluid leaks.
 (a)  
If it is necessary, remove the hydraulic pump (AMM 29-11-05/401) to get better access to the main gearbox.

 (b)  
If any hydraulic fluid is found, replace the gearbox carbon seal (AMM 72-61-07/401).
 
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本文链接地址:747-400 AMM 飞机维护手册 动力装置 POWER PLANT 2(31)