(2)
AMM 24-22-00/201, Electric Power-Control
(3)
AMM 27-81-00/201, Leading Edge Slat System
(4)
AMM 28-26-00/201, Defueling
(5)
AMM 32-00-15/201, Landing Gear Door Locks
(6)
AMM 32-00-20/201, Landing Gear Downlocks
C.
Access
(1)
Location Zones
133 Center Wing Section (Left)
134 Center Wing Section (Right)
511 Leading Edge To Front Spar (Left)
611 Leading Edge To Front Spar (Right)
531 Center Wing Tank (Left)
631 Center Wing Tank (Right)
733 Left MLG Oleo Door
743 Right MLG Oleo Door
D.
Procedure
S 864-028
WARNING:_______DO THE DEACTIVATION PROCEDURE FOR THE LEADING EDGE SLATS. THE SLATS CAN MOVE QUICKLY AND CAUSE INJURY TO PERSONS.
(1)
Do the deactivation procedure for the leading edge slats (AMM 27-81-00/201).
S 144-157
(2)
To remove the forward fuel boost pump, remove the applicable left or right leading edge access panel, 511FB or 611FB (AMM 06-44-00/201).
S 014-029
(3)
To get access to the motor impeller of the aft fuel boost pumps, go through the applicable left or right main shock strut door.
S 014-030
(4)
To get access to the motor impeller of the fuel override pumps, do the steps that follow:
(a)
Make sure the downlocks are installed on the nose and main landing gear (AMM 32-00-20/201).
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MAINTENANCE MANUAL
WARNING: USE THE PROCEDURE IN AMM 32-00-15/201 TO INSTALL THE DOOR
_______ LOCKS. THE DOORS OPEN AND CLOSE QUICKLY AND CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
(b) Open the doors for the landing gear and install the door locks (AMM 32-00-15/201).
S 864-023
(5)
Open this circuit breaker on the main power distribution panel, P6, and attach a DO-NOT-CLOSE tag:
(a)
For the left aft fuel boost pump,
6H15, L AFT FUEL BOOST PUMP
(b)
For the left forward fuel boost pump,
6H23, L FWD FUEL BOOST PUMP
(c)
For the left fuel override pump,
6F14, L FUEL OVRD PUMP
(d)
For the right aft fuel boost pump,
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本文鏈接地址：757 AMM 飛機維護手冊 燃油 CHAPTER 28 - FUEL 3(49)
