S 014-048
(3)
Do these steps for access to the spar valve body (View A):
NOTE: Refer to the table for the access doors.
____
~................................................................. | | Access Door | | ............................................. | Location | Main Tank | Mid Spar | ................................................................... |No. 1 Main Tank | 552EB | 552FZ | ................................................................... |No. 2 Main Tank | 545BB | | ................................................................... |No. 3 Main Tank | 645BB | | ................................................................... |No. 4 Main Tank | 652EB | 652FZ | 2.....................….....................….....................1
(a)
Remove the applicable fuel tank access door (AMM 28-11-02/401).
(b)
Go into the fuel tank (AMM 28-11-00/201).
(c)
NO. 2 AND 3 ENGINE SPAR VALVES; Go to the front spar through the access hole in the midspar.
(d)
N0. 1 AND 4 ENGINE SPAR VALVES; Remove the applicable mid spar access door (AMM 28-11-25/401).
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28-22-05
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
S 034-049
(4)
Do these steps to remove the valve body:
(a)
Disconnect the couplings (4) from the valve body (5).
(b)
Discard the packings (9).
(c)
Remove the bolts (7) and washers (8) (four locations) that attach the valve body (5) to the mounting bracket (6).
(d)
Disengage the valve body (5) from the adapter shaft (3).
(e)
Remove the valve body (5).
TASK 28-22-05-404-010
3. Engine Spar Valve Body Installation (Fig. 401)
___________________________________
A. Equipment
(1)
Bonding Meter (SWPM 20-20-00) Approved for use in fuel vapor areas
B.
Parts
~.............................................................................. | MM | | IPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 401 | 9 | Packing | 28-22-05 | 01 | 166 | | | 9 | Packing | | | 169 | | | 9 | Packing | | | 407 | | | 9 | Packing | | | 408 | | | 5 | Valve Body | | | 181 | | | 5 | Valve Body | | | 415 | 2......…........…...................................…..........….....….........1
C. References
(1)
AMM 28-00-00/201, Fuel
(2)
AMM 28-11-00/201, Fuel Tanks
(3)
AMM 28-11-00/801, Fuel Tank Repair
(4)
AMM 28-22-00/501, Engine Fuel Feed System
(5)
AMM 51-21-04/701, Alodine Coating
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28-22-05
ALL ú ú 02 Page 403 ú Feb 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
ENGINE SPAR VALVE BODY SEE A
ENGINE NO. 2 SPAR VALVE
SEE B NO. 2 MAIN TANK
ENGINE NO. 1
CL
SPAR VALVE
INBOARD
SEE D NO. 1 MAIN TANK NACELLE
CL MIDSPAR DOOR,
OUTBOARD 552FZ
NACELLE (652FZ)
ACCESS DOOR, MIDSPAR ACCESS DOOR,
552EB
545BB
(652EB) (645BB)
NOTE: LEFT WING IS SHOWN, RIGHT WING IS OPPOSITE.
ENGINE SPAR VALVE BODY A
LEGEND
UNDERWING ACCESS DOOR ACCESS DOOR - MID SPAR ACCESS HOLE
NOTE: THE ENGINE NO. 1 AND 4 SPAR VALVES ARE INSTALLED TURNED 180`.
. INSTALL THE VALVE BODY WITH THE "TOP" POSITION MARKER POSITIONED DOWN.
. WHEN THE VALVE DISC IS CLOSED, THE ALIGNMENT ARROWS ON THE VALVE BODY
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