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时间:2011-04-11 09:19来源:蓝天飞行翻译 作者:航空
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Access Panel
 454A Trailing Edge Fairing Doors - System 1
 484A Trailing Edge Fairing Doors - System 4


 E.
Procedure


 S 012-068
 (1)  
Open the fairing doors on the trailing edge of the applicable strut (AMM 54-62-00/201).

 S 862-044

 (2)  
Supply electrical power (AMM 24-22-00/201).

 S 482-069

 (3)  
Install the muffler for the air-driven pump on the turbine exhaust.

 S 792-070

 (4)  
Apply the leak detector to the tube fittings.

 (5)
Supply pressure to the pneumatic system (AMM 36-00-00/201).

 S 862-072

 (6)  
Put the applicable HYD DEMAND switch on the P5 panel in the ON position.

 S 792-073

 (7)  
Examine the fittings for leakage:

 (a)
Repair the cause of all the leakage you find.


 S 862-071
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 29-11-15
 ALL  ú ú 01 Page 214 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 862-074
 (8)  
Put the HYD DEMAND switch in the OFF position.

 S 862-075

 (9)
Release the pressure in the pneumatic system (AMM 36-00-00/201).

 S 082-076

 (10)
 Remove the muffler for the air-driven pump.


 S 412-077
 CAUTION: MAKE SURE YOU LATCH THE FAIRING DOORS ON THE TRAILING EDGE
_______ CORRECTLY. DAMAGE CAN OCCUR IF THE DOORS OPEN DURING A FLIGHT.
 (11)
 Close the fairing doors on the trailing edge of the applicable strut (AMM 54-62-00/201).

 S 862-078

 (12)
 Remove the electrical power if it is not necessary
 (AMM 24-22-00/201).

 

 TASK 29-11-15-102-001
 12. Clean the Water Separator Bleed Hole (Fig. 202)
____________________________________
 A. References
 (1)  
AMM 36-00-00/201, Pneumatic System

 (2)  
AMM 54-62-00/201, Nacelle Strut Access Panels

 B.
Access

 (1)  
Location Zone
 454 System 1 - Strut Trailing Edge Fairing
 484 System 4 - Strut Trailing Edge Fairing


 (2)  
Access Panel
 454A Trailing Edge Fairing Doors - System 1
 484A Trailing Edge Fairing Doors - System 4


 C.
Procedure


 S 012-079
 (1)  
Open the fairing doors on the trailing edge of the applicable strut (AMM 54-62-00/201).

 (2)
Release the pressure in the pneumatic system (AMM 36-00-00/201).


 S 862-080
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 29-11-15
 ALL  ú ú 01 Page 215 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
ENGINE NACELLE STRUT
SEE A
ACTUATOR FOR
THE SPEED
CONTROL VALVE

A
SHUTOFF/SPEED CONTROL VALVE
A
SEE B
FWD
WATER SEPARATOR
FOR THE SPEED
CONTROL VALVE

A
Water Separator Servicing Figure 202 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 29-11-15
 ALL  ú ú 01 Page 216 ú Feb 15/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

747-400 MAINTENANCE MANUAL
SHUTOFF AND SPEED CONTROL VALVE UNIT
SHUTOFF/SPEED
CONTROL VALVE

TYPICAL WATER SEPARATOR HOUSING
BLEED HOLEA-A
FWD WATER SEPARATOR FOR THE SHUTOFF VALVE
B
Water Separator Servicing Figure 202 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 
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