28-21-02
ALL ú ú 01 Page 404 ú Oct 10/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
C. Procedure
S 864-002
(1) If you remove the control unit for the center wing tank refuel valve, make sure the ground lockpins for the landing gear are installed.
S 494-003
WARNING: MAKE SURE YOU OBEY THE INSTRUCTIONS IN AMM 32-00-30/201 WHEN
_______ YOU INSTALL THE LOCKS. IF THE LOCKS ARE NOT CORRECTLY INSTALLED, THE FAST MOVEMENT OF THE DOORS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
(2)
If you remove the control unit for the center wing tank refuel valve, install the wing and body gear door locks (AMM 32-00-30/201).
S 864-004
(3)
Make sure the refuel control panel access door is in the closed position.
S 864-005
(4)
Open these circuit breakers and attach the DO-NOT-CLOSE tags:
(a)
On the DC power distribution panel, P180:
1) 180M8, FUELING VALVE 2
2) 180C25, FUELING LTS PANEL
3) 180C26, FUELING LTS RECP
(b)
On the left power distribution center, P414:
1) 414F17, FUELNG VALVE
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28-21-02
ALL ú ú 06 Page 405 ú Jun 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
S 014-006
(5) Remove the applicable access door or panel to get access to the refuel valve control unit.
NOTE: Refer to the subsequent table for the access data.
____
~................................................................. | | | | Location | Access Door/Panel | | | | ................................................................... | No. 1 Main Tank | 581EB | | No. 2 Main Tank - Inboard | 571AB | | No. 2 Main Tank - Outboard | 572GB | | No. 3 Main Tank - Inboard | 671AB | | No. 3 Main Tank - Outboard | 672GB | | No. 4 Main Tank | 681EB | | No. 2 Reserve Tank | 591AB | | No. 3 Reserve Tank | 691AB | 2......................................…..........................1
S 034-008
(6) Disconnect the electrical connector (4) from the control unit (3).
NOTE: Refer to the subsequent table for the equipment numbers.
____
~................................................................. | | Equipment Number | | Location ............................ | | Valve | Connector | ................................................................... | No. 1 Main Tank | V58 | DV58 | | No. 2 Main Tank - Inboard | V81 | DV81 | | No. 2 Main Tank - Outboard | V59 | DV59 | | No. 3 Main Tank - Inboard | V62 | DV62 | | No. 3 Main Tank - Outboard | V82 | DV82 | | No. 4 Main Tank | V63 | DV63 | | Center Wing Tank - Left | V60 | DV60 | | Center Wing Tank - Right | V61 | DV61 | | No. 2 Reserve Tank | V469 | DV469 | | No. 3 Reserve Tank | V470 | DV470 | 2......................................…...........…..............1
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28-21-02
ALL ú ú 03 Page 406 ú Oct 10/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
S 034-009
(7) Remove the bolts (5) and washers (6) (3 locations) that attach the control unit (3) to the valve unit mounting nuts.
NOTE: A check valve in the refuel valve will prevent fuel leaks
____
when the control unit is removed.
S 024-010
(8)
Remove the control unit (3).
S 034-025
(9)
Discard the packing (1 and 2).
TASK 28-21-02-404-011
3. Refuel Valve Control Unit Installation (Fig. 401)
______________________________________
A. Consumable Materials
(1)
D00128 Petrolatum, Technical VV-P-236
B.
Parts
~.............................................................................. | MM | | IPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 401 | 1 | Packing | 28-21-02 | 02 | 140 | | | 2 | Packing | | | 135 | | | 3 | Control Unit | | | 120 | | | 5 | Bolt | | | 125 | | | 6 | Washer | | | 130 | 2......…........…...................................…..........….....….........1
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本文鏈接地址：747-400 AMM 飛機(jī)維護(hù)手冊(cè) 燃油 FUEL 2(36)
