28-22-41
 ALL  ú ú 02 Page 415 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 FUEL SYSTEM MODULE, P5-2 - REMOVAL/INSTALLATION
_______________________________________________
 1.  General_______
 A. This procedure contains three tasks:
 (1)  
Removal of the Fuel System Module, P5-2

 (2)  
Installation of the Fuel System Module, P5-2

 (3)  
Operational Test of the Fuel System Module, P5-2.

 TASK 28-22-43-034-001
 2.  Removal of the Fuel System Module, P5-2_______________________________________
 A. Access
 (1)  Location Zones
 101 Control Cabin Left
 102 Control Cabin Right

 B. Procedure
 S 864-002
 (1) Open these circuit breakers and attach DO-NOT-CLOSE tags:
 (a)  P6 Main Power Distribution Panel 1) SHUTOFF VALVE - ENG 1 2) SHUTOFF VALVE - ENG 2 3) FUEL SHUTOFF VALVE 4) FUEL TEMPERATURE IND 5) FUEL CROSSFEED VALVE 6) MASTER DIM SECTION 1 7) MASTER DIM SECTION 6 8) TANK-1 FWD BOOST PUMP 9) TANK-2 FORWARD BOOST PUMP 10) TANK-1 AFT BOOST PUMP 11) TANK-2 AFT BOOST PUMP 12) CENTER TANK BOOST PUMP LEFT 13) CENTER TANK BOOST PUMP RIGHT 14) FUEL CONT-1 AFT-2 FORWARD CTR LEFT 15) FUEL CONT-1 FWD-2 AFT CTR RIGHT
 S 034-003
 (2)  
Loosen the six quick-release fasteners on the baseplate of the P5-2 module.

 S 034-004

 (3)  
Disconnect the connectors D626, D628, and D616 from the rear of the P5-2 module.

 (4)  
Remove the P5-2 module from the P5 panel.

 S 034-005
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 28-22-43
 ALL  ú ú 01 Page 401 ú Nov 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
ENGINE FUEL

CAUTION ANNUNCIATORS  CAUTION ANNUNCIATORS 
(LEFT)  (RIGHT) 
MASTER CAUTION LIGHTS 
B 
Fuel System Module, P5-2 
Figure 401 

K67424
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 28-22-43
 ALL  ú
 ú  01  Page 402
 ú  Nov 12/99 

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 TASK 28-22-43-434-041
 3. Installation of the Fuel System Module, P5-2
____________________________________________
 A. Access
 (1)  Location Zones
 101 Control Cabin Left
 102 Control Cabin Right

 B. Procedure
 S 434-006
 (1)
Move the P5-2 module close to its position in the P5 panel.

 S 434-007

 (2)  
Connect the connectors D616, D626, and D628 to the rear of the P5-2 module.

 S 434-008

 (3)  
Install the P5-2 module in its position with the six quick-release fasteners on the baseplate.

 S 714-009

 (4)
Do this task: Operational Test of the Fuel System Module, P5-2.

 TASK 28-22-43-714-010
 4. Operational Test of the Fuel System Module, P5-2
________________________________________________
 A. References
 (1)  AMM 24-22-00/201, Manual Control
 B. Access
 (1)  Location Zones
 101 Control Cabin Left
 102 Control Cabin Right

 C. Procedure
 S 864-011
 (1)  
Supply external power to the airplane if power is not supplied (AMM 24-22-00/201).

 S 864-012

 (2)
Remove the DO-NOT-CLOSE tags and close these circuit breakers:

 (a)  P6 Main Power Distribution Panel
 1) SHUTOFF VALVE - ENG 1
 2) SHUTOFF VALVE - ENG 2
 3) FUEL SHUTOFF VALVE
 4) FUEL TEMPERATURE IND

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 燃油 FUEL 2(142)