(a)
Start with this procedure: Fuel Pump Wire Terminal Assembly
Inspection. ú
K. Put the Airplane Back to the Usual Condition
S 096-029
WARNING: USE THE PROCEDURE IN AMM 32-00-15/201 TO REMOVE THE DOOR LOCKS.
_______ THE DOORS CAN OPEN AND CLOSE QUICKLY AND CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
(1) Remove the door locks from the landing gear doors and close the doors (AMM 32-00-15/201).
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S 416-068
(2) For the forward fuel boost pumps, install the applicable left or right access panel, 511FB or 611FB (AMM 06-44-00/201).
S 866-030
WARNING: DO THE ACTIVATION PROCEDURE FOR THE LEADING EDGE SLATS
_______ (AMM 27-81-00/201). THE SLATS CAN MOVE QUICKLY AND CAN CAUSE INJURY TO PERSONS.
(3)
Do the activation procedure for the leading edge slats (AMM 27-81-00/201).
S 866-034
(4)
Remove the DO-NOT-CLOSE tags and close these circuit breakers:
(a)
On the main power distribution panel, P6:
1) 6F14, L FUEL OVRD PUMP
2) 6H14, L AFT FUEL BOOST PUMP
3) 6H17, R FWD FUEL BOOST PUMP
4) 6F20, R FUEL OVRD PUMP
5) 6H20, R AFT FUEL BOOST PUMP
6) 6H23, L FWD FUEL BOOST PUMP
S 866-035
(5) Remove the electrical power if it is not needed for another task (AMM 24-22-00/201).
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ENGINE FUEL SHUTOFF VALVE - REMOVAL/INSTALLATION
________________________________________________
1. General_______
A. The engine fuel shutoff valve contains three parts: the actuator, the adapter shaft and the valve body.
B. The engine fuel shutoff valve is installed on the rear spar, aft of each fuel measuring stick No. 3 (AMM 28-44-00/001).
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本文鏈接地址：757 AMM 飛機維護手冊 燃油 CHAPTER 28 - FUEL 3(16)
