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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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 C. References
 (1)  
AMM 29-11-00/201, Main Hydraulic Supply System

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


 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 29-11-18
 ALL  ú ú 01 Page 212 ú Jun 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 D. Access
 (1)  
Location Zone
 454 System 1 - Strut Aft Fairing
 464 System 2 - Strut Aft Fairing
 474 System 3 - Strut Aft Fairing
 484 System 4 - Strut Aft Fairing


 (2)  
Access Panel
 454AL Trailing Edge Fairing Doors - System 1
 464AL Trailing Edge Fairing Doors - System 2
 474AL Trailing Edge Fairing Doors - System 3
 484AL Trailing Edge Fairing Doors - System 4


 E.
Procedure


 S 642-045
 (1)  
Lubricate all the packings and the component threads with hydraulic fluid.

 S 422-075

 (2)  
Install the check valve (10):

 (a)  
Install the packings (12 and 14) and the backup rings (11 and 13) on the check valve (10).

 (b)  
Install the check valve (10) in the module. 1) Tighten the check valve to 10-12 pound-inches (13-16 N.m).


 S 862-048
 (3)  
Pressurize the hydraulic system with the EDP or the demand pump (AMM 29-11-00/201).

 S 792-049

 (4)  
Examine the case drain module for leakage.

 (a)  
If you find leakage, repair the cause of the leakage.


 S 862-050
 (5)  Release the pressure in the hydraulic system if it is not necessary for other operations (AMM 29-11-00/201).
 S 412-052
 CAUTION: MAKE SURE YOU LATCH THE FAIRING DOORS ON THE TRAILING EDGE
_______ CORRECTLY. DAMAGE CAN OCCUR IF THE DOORS OPEN DURING A FLIGHT.
 (6)  Close the fairing doors on the trailing edge of the applicable strut (AMM 54-62-00/201).
 TASK 29-11-18-002-053
 8. Differential Pressure (.P) Indicator Removal (Fig. 201)
____________________________________________
 A. References
 (1)  
AMM 29-11-00/201, Main Hydraulic Supply System

 (2)  
AMM 36-00-00/201, Pneumatic System


 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 29-11-18
 ALL  ú ú 01 Page 213 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 (3)  
AMM 54-62-00/201, Nacelle Strut Access Panels

 (4)  
IPC 29-11-18 Fig. 1

 B.
Access

 (1)  
Location Zone
 454 System 1 - Strut Aft Fairing
 464 System 2 - Strut Aft Fairing
 474 System 3 - Strut Aft Fairing
 484 System 4 - Strut Aft Fairing


 (2)  
Access Panel
 454AL Trailing Edge Fairing Doors - System 1
 464AL Trailing Edge Fairing Doors - System 2
 474AL Trailing Edge Fairing Doors - System 3
 484AL Trailing Edge Fairing Doors - System 4


 C.
Procedure


 S 012-054
 (1)  Open the fairing doors on the trailing edge of the applicable strut (AMM 54-62-00/201).
 S 862-055
 WARNING: MAKE SURE YOU RELEASE THE PNEUMATIC SYSTEM PRESSURE BEFORE YOU
_______ OPEN THE HYDRAULIC SYSTEM. THE PNEUMATIC SYSTEM PRESSURIZES THE HYDRAULIC RESERVOIR. HYDRAULIC FLUID THAT HAS PRESSURE CAN CAUSE INJURY TO PERSONS.
 (2) Release the pressure in the pneumatic system (AMM 36-00-00/201).
 S 862-056
 WARNING: MAKE SURE YOU RELEASE THE HYDRAULIC SYSTEM PRESSURE BEFORE YOU
_______ OPEN THE HYDRAULIC SYSTEM. HYDRAULIC FLUID THAT HAS PRESSURE CAN CAUSE INJURY TO PERSONS.
 (3)
Release the pressure in the hydraulic system (AMM 29-11-00/201).

 S 022-057

 (4)  
Remove the differential pressure indicator (7):

 (a)  
Remove the screws (6) that attach the differential pressure indicator (7) to the module.
 
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