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时间:2011-04-11 09:13来源:蓝天飞行翻译 作者:航空
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 (3)  S 434-037Tighten the pressure switch (2) to 95-105 pound-inches.
 (4)  S 434-033Install lockwire on the pressure switch (2).
 (5)  S 434-014Put a new packing (10), lightly lubricated with fuel, into the groove on the pump (7).
 S 424-015

 CAUTION: YOU MUST BE CAREFUL WHEN YOU INSTALL THE PUMP IN THE RECEIVER.
_______ YOU CAN CAUSE DAMAGE TO THE PACKING AND CAUSE FUEL LEAKS.
 (6)  
Install the boost pump (7) in the receiver.

 S 434-016

 (7)  
Install the bonding jumper (3) on the inboard mounting bolt (5).

 S 434-017

 (8)  
Install the bolts (5 and 9) and the washers (6) to attach the pump (7) to the receiver.

 S 434-034

 (9)  
Install lockwire on the bolts.

 S 944-020

 (10)
 Measure the resistance between the pump (7) and the spar web (SWPM 20-20-00).


 NOTE: The resistance must not be more than 0.001 ohm.
____
 S 434-018
 (11)
 Connect the electrical connector DM713 (8) to the pump motor (7).

 S 434-019

 (12)
 Connect the electrical connector DS435 (4) to the pump pressure switch S435 (2).


 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 28-25-01
 ALL  ú ú 03 Page 405 ú Oct 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 E. Operational Test
 S 864-021
 (1)  
Supply electrical power, if it is not already done
 (AMM 24-22-00/201).


 S 864-022

 (2)  
Remove the DO-NOT-CLOSE tag and close this circuit breaker:

 (a)  
P6 Main Power Distribution Panel
 1) 6H18, DC FUEL PUMP APU

 

 S 864-023
 (3)  
Open these circuit breakers and attach DO-NOT-CLOSE tags:

 (a)  
P414 Power Distribution Center-Left
 1) 414R18, FUEL BOOST PUMP MAIN AFT 2


 (b)  
P415 Main Power Distribution Panel
 1) 415M29, FUEL BOOST PUMP MAIN AFT 3

 

 S 754-024
 (4)  
Remove the DO-NOT-OPERATE tag and put the APU control switch to the ON position.

 S 754-035

 (5)
Make sure the pump operates (audible indication or vibration).

 S 864-039

 (6)  
Make sure this EICAS message does not show on the main EICAS display or the status page of the auxiliary EICAS display:

 (a)  
APU FUEL PUMP (STATUS)


 S 864-025
 (7)  
Put the APU control switch to the STOP position.

 S 864-026

 (8)  
Remove the DO-NOT-CLOSE tag and close these circuit breakers:

 (a)  
P414 Power Distribution Center-Left
 1) 414R18, FUEL BOOST PUMP MAIN AFT 2


 (b)  
P415 Main Power Distribution Panel
 1) 415M29, FUEL BOOST PUMP MAIN AFT 3

 

 S 094-027
 WARNING: USE THE PROCEDURE IN AMM 32-00-30/201 TO REMOVE THE DOOR LOCKS.
_______ THE DOORS OPEN AND CLOSE QUICKLY AND CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (9)  
Remove the wing and body gear door locks (AMM 32-00-30/201).

 (10)
 Remove electrical power if it is not necessary (AMM 24-22-00/201).


 S 864-028
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 28-25-01
 ALL  ú ú 01 Page 406 ú Oct 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 APU FUEL SHUTOFF VALVE ACTUATOR - REMOVAL/INSTALLATION
______________________________________________________
 1. General
_______
 A. This procedure has two tasks:
 (1)  
A task to remove the APU fuel shutoff valve actuator.

 (2)  
A task to install the APU fuel shutoff valve actuator.


 TASK 28-25-02-004-001
 2. APU Fuel Shutoff Valve Actuator Removal (Fig. 401)
_______________________________________
 
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