(9)
Remove the adapter.
S 024-005
TASK 28-21-01-404-006
3. Install the Fueling Adapter (Fig. 401)
___________________________
A. References
(1)
AMM 06-44-00/201, Wings (Major Zones 500 and 600) Access Doors and Panels
(2)
AMM 12-11-01/301, Fuel Tank Pressure Fueling
(3)
AMM 27-81-00/201, Leading Edge Slat System
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MAINTENANCE MANUAL
B. Access
(1)
Location Zone
621 Leading Edge to Front Spar (Right)
(2)
Access Panel
621GB Fueling Station Door (Right)
C.
Procedure
S 424-007
(1)
Align the adapter with the fueling adapter body.
S 434-031
(2)
Install the screws (7 thru 12) in the sequence shown (View B).
S 434-032
(3)
Tighten the screws (7 thru 12) to 28-30 pound-inches in sequence.
NOTE: Screws 7 thru 12 attach the adapter to the fueling
____
adapter body.
S 654-034
(4)
Refuel the fuel tanks (AMM 12-11-01/301).
S 214-035
(5)
Make sure there are no fuel leaks at the fueling adapter.
S 414-036
(6)
Close the fueling station door, 621GB (AMM 06-44-00/201).
S 864-037
WARNING: DO THE ACTIVATION PROCEDURE FOR THE LEADING EDGE SLAT PROCEDURE
_______ (AMM 27-81-00/201) ACCIDENTAL SLAT OPERATION COULD CAUSE INJURY TO PERSONS.
(7) Do the activation procedure for the leading edge slat procedure (AMM 27-81-00/201).
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S 944-084
(8)
Remove the ropes and DANGER - OPEN FUEL TANKS signs from around the fueling station.
S 494-085
(9)
Connect the airplane battery and remove the OPEN FUEL TANK - DO NOT CONNECT signs.
S 914-086 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：757 AMM 飞机维护手册 燃油 CHAPTER 28 - FUEL 2(66)
