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时间:2011-04-02 05:51来源:蓝天飞行翻译 作者:航空
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 adjacent clamp.
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 28-22-21
 ALL  ú ú 02 Page 406 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 (d)  
Put the tape on the wire bundle with a 50% overlap to give protection from friction.

 (e)  
Install the layer of tape on the wire bundle from the plug to a location on the far side of the third clamp.


 S 434-030
 (6)  
Connect the bonding jumper to the actuator assembly.

 S 764-031

 (7)  
Do a check of the electrical bond (SWPM 20-20-00).


 (a)  The resistance must not be more than 0.01 ohm.
 S 864-032
 (8) Remove the DO-NOT-CLOSE tag and close this circuit breaker:
 (a)  P6 Main Power Distribution Panel 1) CROSSFD VALVE (for the fuel crossfeed valve)
 S 714-051
 (9)  Do the fuel crossfeed valve test (AMM 28-22-00/501).
 TASK 28-22-21-004-033
 6. Crossfeed Valve Port Adapter Assembly Removal (Fig. 401)
_____________________________________________
 A. References
 (1)  
AMM 28-10-00/201, Fuel Storage

 (2)  
AMM 28-11-11/401, Wing Fuel Tank Access Panels

 (3)  
AMM 28-11-31/401, Center Tank Access Panel

 (4)  
AMM 28-23-00/201, Defueling


 B. Access
 (1)  
Location Zone
 405 Right Fuel Tank


 (2)  
Access Panels
 7402 Fuel Tank Access Door

 

 C. Procedure
 S 654-034
 WARNING: CAREFULLY DO ALL OF THE SAFETY PROCEDURES TO DEFUEL THE FUEL
_______ TANKS. AN EXPLOSION, BAD INJURY TO PERSONS, AND DAMAGE TO EQUIPMENT CAN OCCUR.
 (1)  Do this task: "Fuel Tank Defueling" for the No. 2 tank (AMM 28-23-00/201).
 S 864-035
 WARNING: CAREFULLY DO ALL OF THE SAFETY PROCEDURES TO PREPARE TO GO INTO
_______ THE FUEL TANK. AN EXPLOSION, BAD INJURY TO PERSONS, AND DAMAGE TO EQUIPMENT CAN OCCUR.
 (2)  Do this task: "Purging (Air Ventilating)" (AMM 28-10-00/201) for the No. 2 tank.
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 28-22-21
 ALL  ú ú 02 Page 407 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 014-036
 (3)  Remove the access panel, No. 1, for the No. 2 fuel tank (AMM 28-11-11/401).
 NOTE: This gives you access to the front of the wing rear spar.
____
 S 014-037
 (4)  
Do this task: "Crossfeed Valve Gate Assembly Removal".

 S 014-038

 (5)  
Go into the No. 2 fuel tank through the opening for the access panel, No. 1 (7402).

 S 014-039

 (6)  
Get access to the crossfeed valve through the applicable rib access openings (AMM 28-11-11/401, AMM 28-11-31/401).

 S 034-040

 (7)  
Remove the bolts that attach the fuel line flanges to the port adapter assembly.


 S 024-041
 CAUTION:_______DO NOT LET THE PORT ADAPTER ASSEMBLY FALL. DAMAGE TO THE WING SKIN OR THE SEAL SURFACES ON THE FUEL TANK CAN OCCUR.
 (8)  Remove the port adapter assembly.
 NOTE: Two persons are necessary to do this step.
____
 (a)  
Put one person in the tank to hold the port adapter assembly up.

 (b)  
A second person must get access to the parts that attach the port adapter assembly out of the tank.

 (c)  
The second person must remove the bolts and the washers that attach the port adapter assembly.

 (d)  
The person in the tank must move the port adapter assembly from its position between the fuel line flanges.


 TASK 28-22-21-404-042
 7.  Crossfeed Valve Port Adapter Assembly Installation__________________________________________________
 A. Consumable Materials
 (1)  B00316 - Aliphatic Naphtha TT-N-95
 B. References
 
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本文链接地址:737-300 400 500 AMM 飞机维护手册 燃油 FUEL 2(125)