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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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
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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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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
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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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 m.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)
