747-400 AMM 飞机维护手册 液压 HYDRAULIC 1(99)

曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

 4)  Install the gearbox bolt into the gearbox plug at a sufficient depth to start the nut on the bolt. Then install the nut and tighten it with your hand 1 1/2 to 2 turns.
 (b)  Install the plug and seal assembly on the end of the gearshaft.
 NOTE: The bolt head must engage the groove behind the
____ drive shaft splines before the plug engages the gear shaft splines.
 (c)  After the head of the bolt engages the gear shaft groove, push the plug fully into the gear shaft. 1) Make sure the plug splines engage with the gear shaft
 splines.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 29-11-05
 ALL  ú ú 01 Page 203 ú Oct 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 (d)  
Remove the nut and install the washer.

 (e)  
Install the nut on the bolt. 1) Tighten the nut to 36-40 pound-inches (4.1-4.5 N.m).

 S 032-004
 (4)  
Disconnect the drain line for the pump pad.

 S 032-072

 (5)  
Remove the adapter fitting that is installed in the drain boss. The drain tube B-nut attaches to this.

 S 432-005

 (6)  
Install the pump pad plug.

 S 432-006

 (7)  
Install the drive pad cover:

 (a)  
Install the drive pad cover and the gasket on the face of the drive pad for the hydraulic pump.

 (b)  
Install four locknuts on the mounting studs for the hydraulic pump. 1) Tighten the locknuts to 275-300 pound-inches (31.1-33.9

 N.m).
 S 432-008
 (8)  
Install the plugs on the inlet hose, the outlet hose, and the case drain hose.

 S 792-009

 (9)  
Run the engine at idle (AMM 71-00-00/501) and examine the installation for oil leakage.

 S 792-010

 (10)
 Pressurize the hydraulic system and examine for leakage (AMM 29-11-00/201).

 S 862-037

 (11)
 Release the pressure in the hydraulic system, if it is not necessary (AMM 29-11-00/201).

 S 412-038

 (12)
 Close the thrust reverser on the right side of the engine (AMM 78-31-00/201).

 TASK 29-11-05-402-012
 3.  Deactivated Engine-Driven Pump (EDP) Installation (Fig. 201)_________________________________________________
 A. Special Tools and Equipment
 (1)  
G29005-1 - EDP Dispatch Equipment. This equipment contains these parts:

 (a)  
1 drive cover

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 29-11-05
 ALL  ú ú 01 Page 204 ú Oct 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 (b)  
1 plug for the case drain hose

 (c)  
1 outlet hose plug

 (d)  
1 inlet hose plug

 (e)  
1 pump pad plug

 (f)  
1 gasket

 (g)  
1 plug and seal assembly. This assembly contains these parts: 1) 1 large packing 2) 1 small packing 3) 1 gearbox bolt 4) 1 gearbox plug 5) 1 washer 6) 1 nut.

 B.
Consumable Materials

 (1)  
D00071 Oil - Aircraft Turbine Engine Lubricating, MIL-L-7808 (optional to MIL-L-23699)

 (2)  
D00068 Oil - Aircraft Turbine Engine Lubricating, MIL-L-23699 (optional to MIL-L-7808)

 C.
References

 (1)  
AMM 29-11-00/201, Hydraulic Power

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

 (3)  
AMM 71-00-00/501, Power Plant

 D.
Access

 (1)  
Location Zones
 412 Engine 1 - Gearbox Forward Face 5:00 o'clock
 422 Engine 2 - Gearbox Forward Face 5:00 o'clock
 432 Engine 3 - Gearbox Forward Face 5:00 o'clock
 442 Engine 4 - Gearbox Forward Face 5:00 o'clock

 (2)  
Access Panels
 416 Right Thrust Reverser Half - Engine 1
 426 Right Thrust Reverser Half - Engine 2
 436 Right Thrust Reverser Half - Engine 3
　
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：747-400 AMM 飞机维护手册 液压 HYDRAULIC 1(99)