(3)
AMM 27-81-00/201, Leading Edge Slat System
(4)
AMM 28-22-03/401, Fuel Boost Pump
(5)
AMM 32-00-15/201, Landing Gear Door Locks
(6)
AMM 32-00-20/201, Landing Gear Downlocks
D.
Access
(1)
Location Zones
133 Wing Center Section, Left
134 Wing Center 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
(2)
Access Panels
134AZ Center Tank Access Door, Right
134BZ Baffle Door
134CZ Baffle Door
134DZ Baffle Door
511FB Leading Edge Access Panel, Left
611FB Leading Edge Access Panel, Right
531AB Center Tank Access Door, Left
631AB Center Tank Access Door, Right
E.
Prepare for the Check
(1)
Supply the electrical power if necessary (AMM 24-22-00/201).
S 866-002
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757 MAINTENANCE MANUAL
S 866-003
WARNING: DO THE DEACTIVATION PROCEDURE FOR THE LEADING EDGE SLATS
_______ (AMM 27-81-00/201). THE SLATS CAN MOVE QUICKLY AND CAUSE INJURY TO PERSONS.
(2)
Do the deactivation procedure for the inboard leading edge slats (AMM 27-81-00/201).
S 146-058
(3)
For the forward fuel boost pump, remove the applicable left or right leading edge access panel, 511FB or 611FB (AMM 06-44-00/201).
S 866-037
(4)
Make sure the downlocks are installed on the nose and main landing gear (AMM 32-00-20/201).
S 496-004
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.
(5)
Open the doors for the landing gear and install the door locks (AMM 32-00-15/201).
S 866-010
(6)
Open the applicable circuit breakers and attach DO-NOT-CLOSE tags:
(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
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本文鏈接地址：757 AMM 飛機維護手冊 燃油 CHAPTER 28 - FUEL 3(10)
