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28-22-10
ALL ú ú 01 Page 407 ú Oct 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
G. Put the Airplane Back to the Usual Condition
S 864-016
(1)
Go out of and close the fuel tank (AMM 28-11-00/201).
S 414-029
(2)
Install the applicable main tank access door(s) (AMM 28-11-02/401).
H.
Crossfeed Valve Body Operational Test
S 714-022
(1) Do this task: Fuel Crossfeed Valves - Fuel Transfer Operational Test (AMM 28-22-00/501).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
28-22-10
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
FUEL CROSSFEED VALVE ADAPTER - REMOVAL/INSTALLATION
___________________________________________________
1. General_______
A. This procedure contains instructions to remove and install the engine fuel crossfeed adapter (referred to as the adapter) that connects the valve body with its actuator.
B. The valve adapter consists of the adapter plate, index plate and adapter shaft. The index plate and adapter plate are attached to the actuator on the outside of the tank at the front spar. The adapter shaft extends from the adapter plate through an opening in the front spar and engages with a receptacle in the valve body. To remove a valve adapter you must enter the applicable main fuel tank and remove the bolts that attach the adapter plate to the front spar.
C. To get access to the adapter plate, extend the leading edge flaps. Access to the bolts for the adapter is through a fuel tank access door installed below the wing.
D. When persons do maintenance in the area of the wing leading edge, install safety locks on all the extended leading edge flaps.
TASK 28-22-11-004-001
2. Fuel Crossfeed Valve Adapter Removal (Fig. 401)____________________________________
A. References
(1)
AIPC 28-22-11 Fig. 1
(2)
AMM 27-81-00/201, Leading Edge Flap Systems
(3)
AMM 28-11-00/201, Fuel Tanks
(4)
AMM 28-11-02/401, Reserve and Main Tank Access Door
(5)
AMM 28-22-02/401, Fuel Crossfeed Valve Actuator
(6)
AMM 28-26-00/201, Defueling
B.
Access
(1)
Location Zones 521 Leading Edge to Front Spar, Left 542 Inbd Main Tank (Part), Front Spar to Mid Spar, Left 551 Outbd Main Tank (Part), Front Spar to Mid Spar, Left 621 Leading Edge to Front Spar, Right 642 Inbd Main Tank (Part), Front Spar to Mid Spar, Right 651 Outbd Main Tank (Part), Front Spar to Mid Spar, Right
(2)
Access Panels
545AB Fuel Tank Access Door
546AB Fuel Tank Access Door
645AB Fuel Tank Access Door
646AB Fuel Tank Access Door
C.
Prepare for the Removal
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
28-22-11
ALL ú ú 01 Page 401 ú Oct 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
S 864-030
WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF THE LEADING
_______ EDGE AND TRAILING EDGE FLAPS AND FLAP DRIVE MECHANISMS BEFORE YOU MOVE THE FLAP CONTROL LEVER. WITH HYDRAULIC POWER REMOVED, THE FLAPS WILL MOVE AUTOMATICALLY BY ELECTRICAL POWER WHEN YOU MOVE THE FLAP CONTROL LEVER.
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