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28-21-13
ALL ú ú 04 Page 401 ú Jun 10/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
C. Procedure
S 654-002
(1)
Defuel the applicable fuel tank (AMM 28-26-00/201).
S 014-003
(2)
Remove the refuel valve control unit (AMM 28-21-02/401).
S 864-004
WARNING: CAREFULLY DO ALL THE SAFETY PROCEDURES TO DEFUEL AND TO GO INTO
_______ THE FUEL TANKS. INJURY TO PERSONS AND DAMAGE TO EQUIPMENT CAN OCCUR IF YOU DO NOT OBEY THE SAFETY PROCEDURES.
(3)
Purge and prepare the tank for entry (AMM 28-11-00/201).
S 034-005
(4)
Remove the nuts and washers (3 locations) that attach the valve unit to the rear spar.
S 014-006
(5)
Remove the fuel tank access doors, when it is necessary, to get access to the valve unit (AMM 28-11-02/401).
NOTE: Refer to the subsequent table for access data.
____
~................................................................. | | | | Location | Access Door/Panel | | | | ................................................................... | No. 1 Main Tank | 546BB | | No. 2 Main Tank - Inbd | 545AB | | No. 2 Main Tank - Outbd | 545BB | | No. 3 Main Tank - Inbd | 645AB | | No. 3 Main Tank - Outbd | 645BB | | No. 4 Main Tank | 646BB | | No. 2 Reserve Tank | 553BB | | No. 3 Reserve Tank | 653BB | 2......................................…..........................1
S 864-007
(6)
Go into the fuel tank (AMM 28-11-00/201).
S 034-008
(7)
Remove the bolt, washers, and nut that attach the bonding jumper to the grounding lug on the valve unit.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
28-21-13
ALL ú ú 01 Page 402 ú Oct 10/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
S 034-009
(8)
Remove the lockwire between the outlet flange bolt and the inlet tube coupling nut.
S 034-091
(9)
Remove the bolts (4 locations) that attach the outlet tube to the valve unit.
S 034-010
(10)
Disconnect the outlet tube and the valve unit.
S 034-092
(11)
Remove the orifice plate and the gasket seal.
S 034-011
(12)
Disconnect the inlet tube coupling from the valve unit.
S 034-093
(13)
Discard the O-ring.
S 024-012
(14)
Remove the valve unit and the gasket seal from the tank.
TASK 28-21-13-404-013
3. Main or Reserve Tank Refuel Valve Unit Installation (Fig. 401)___________________________________________________
A. Equipment
(1)
Bonding Meter (AMM 20-22-01/601)
B.
References
(1)
AMM 20-11-15/401, Bonding Jumpers and Ground Leads
(2)
AMM 20-22-01/601, Electrical Bonding
(3)
AMM 28-11-00/201, Fuel Tanks
(4)
AMM 28-21-02/401, Refuel Valve Control Unit
(5)
AIPC 28-21-02, Fig. 2
(6)
AIPC 28-21-02 Fig. 2
C.
Access
(1)
Location Zones 545 Inbd Main Tank (Part), Mid Spar to Rear Spar, Left 552 Outbd Main Tank (Part), Mid Spar to Rear Spar, Left 553 Reserve Tank, Front Spar to Rear Spar, Left 645 Inbd Main Tank (Part), Mid Spar to Rear Spar, Right 652 Outbd Main Tank (Part), Mid Spar to Rear Spar, Right 653 Reserve Tank, Front Spar to Rear Spar, Right
(2)
Access Panels
545AB Fuel Tank Access Door
553BB Fuel Tank Access Door
645AB Fuel Tank Access Door
653BB Fuel Tank Access Door
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú 中國航空網 www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：747-400 AMM 飛機維護手冊 燃油 FUEL 2(49)
