INDEX
BRACKET PLATE
7. O-RINGS COUPLING NUT
FUEL CROSSFEED VALVE
ACTUATOR2. COUPLING
(EXAMPLE)
B
FERRULE
1. VALVE BODY
6. MOUNTING BRACKET
INDEX
FUEL MARKS
TUBE FOR THE VALVE BODY
1. VALVE INDEX
BODY
RETAINER

MARKS
HALVES

FOR THE 5. ADAPTER
RETAINING RINGS  ADAPTER SHAFTSHAFT
A-A
1 PREPARE THE FAYING SURFACE OF THE VALVE BODY AND MATING SURFACE OF THE MOUNTING INDEX MARKS BRACKET FOR AN ELECTRICAL SURFACE BOND (SWPM 20-20-00). C
Fuel Crossfeed Valve Body Installation
Figure 401 (Sheet 2)

L36773
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 28-22-10
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 TASK 28-22-10-404-010
 3. Fuel Crossfeed Valve Body Installation (Fig. 401)
______________________________________
 A. References
 (1)  
AIPC 28-22-10 Fig. 1

 (2)  
AMM/28-00-00/201, Fuel

 (3)  
AMM 28-11-00/201, Fuel Tanks

 (4)  
AMM 28-11-00/801, Fuel Tanks

 (5)  
AMM 28-11-02/401, Reserve and Main Tank Access doors

 (6)  
AMM 28-22-00/501, Engine Fuel Feed System

 (7)  
AMM 51-21-04/701, Alodine Coating

 (8)  
SWPM 20-20-00, Electrical Ground and Bond

 B.
Equipment

 (1)  
Bonding Meter (SWPM 20-20-00) Approved for use in fuel vapor areas

 C.
Consumable Materials

 (1)
C00064 Coating - Alodine 600 chemical conversion coating for aluminum or aluminum alloy, (MIL-C-5541)

 (2)  
C00307 Corrosion Resistant Finish - BMS 10-20 Type II

 (3)  
D00128 Petrolatum - Technical, VV-P-236

 D.
Parts

 ~.............................................................................. | MM | | IPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 401 | 1 | Valve Body | 28-22-10 | 01 | 25 | | | 7 | O-ring (Packing) | | | 20 | 2......…........…...................................…..........….....….........1
 E. Access
 (1)  
Location Zones 542 Inbd Main Tank (Part), Front Spar to Mid Spar, Left 551 Outbd Main Tank (Part), Front Spar to Mid Spar, Left 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

 F.
Procedure

 S 164-025
 (1)  AIRPLANES WITH A BARE METAL SURFACE AT THE MOUNTING BRACKET; Prepare the mating surfaces of the valve body (1) and mounting bracket for a fay surface bond (SWPM 20-20-00) (View B).
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A 747-400 MAINTENANCE MANUAL
 (2)  S 864-011Make sure the actuator is in the closed position.
 (3)  S 424-012Install the valve body (1) with the TOP position indication on top of the valve (nearest the wing upper skin).
 (4)  S 424-028Engage the valve body (1) with the adapter shaft (5).
 (5)  S 824-020Make sure the index marks on the adapter shaft and the valve body align (View C).
 NOTE:____ The index marks on the valve body must be on top when the valve is closed (nearest the wing upper skin).
 (6)  S 434-026Do these steps to install the valve body (1): (a) Install the bolts (3) and washers (4) (four locations) that attach the valve body (1) to the mounting bracket (6). (b) AIRPLANES WITH A BARE METAL SURFACE AT THE MOUNTING BRACKET; Apply these protective finishes to any exposed areas on the mounting bracket: 1) Alodine 600 (AMM 51-21-04/701) 2) BMS 10-20 Type II primer (AMM 28-11-00/801). (c) Put lockwire on the bolts (3). (d) Install new O-rings (7) in the couplings (2) on the fuel line (View A-A).
　
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