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时间:2011-04-11 09:00来源:蓝天飞行翻译 作者:航空
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AMM 28-11-09/401, Spanwise Beam Access Door

 D.
Access

 (1)  
Location Zones
 131 Center Section Wing Box, Left
 132 Center Section Wing Box, Right


 (2)  
Access Panels
 131EZ Center Wing Tank Access Door
 132CZ Center Wing Tank Access Door
 131AZ Spanwise Beam Access Door
 131BZ Spanwise Beam Access Door
 131CZ Spanwise Beam Access Door
 132AZ Spanwise Beam Access Door


 E.
Install the Float Valve(s)


 S 864-064
 WARNING:_______OBEY ALL THE FUEL TANK PURGING AND ENTRY PRECAUTIONS. YOU CAN CAUSE AN INJURY TO A PERSON AND CAUSE DAMAGE TO THE AIRPLANE.
 (1)  
Go into the center wing tank.

 S 394-068

 (2)  
Use the sealant to apply a faying surface seal between the float valve and the structure (bracket).


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 28-15-11
 ALL  ú ú 03 Page 403 ú Oct 10/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

747-400
MAINTENANCE MANUAL

FUEL SCAVENGE SYSTEM SEE A
CENTER WING TANK (REF)
JET PUMP 
FLOAT VALVE IN THE  (4 LOCATIONS) 
NO. 2 MAIN TANK  FLOAT VALVE IN THE 
SEE  C  NO. 3 MAIN TANK 
A  A
NO. 2 MAIN TANK  NO. 3 MAIN TANK 
(REF)  (REF) 

AA FUEL STRAINER HOUSING (2 LOCATIONS)
FLOAT VALVE IN THE CENTER WING TANK (2 LOCATIONS)
SEE B
FWD
FUEL SCAVENGE SYSTEM
OUTBD
A
REAR SPAR OF THE CENTER WING TANK (REF)INTERCOSTAL (REF)
FLOAT VALVE IN THE SPANWISE BEAM
MID-SPAR OF THE SPANWISE BEAM CENTER WING TANK
NO. 2 (REF) CENTER WING TANK NO. 1 (REF)
(REF) A-A Float Valves for the Fuel Scavenge System Figure 401 (Sheet 1)
A77292
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 28-15-11
 ALL  ú ú 03 Page 404 ú Feb 10/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

747-400
MAINTENANCE MANUAL


THE CENTER WINGTANK
B-B
Float Valves for the Fuel Scavenge System
Figure 401 (Sheet 2)

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 28-15-11
 ALL  ú ú 03 Page 405 ú Feb 10/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A77305
A
747-400
MAINTENANCE MANUAL


PUMPS
FLOAT VALVE IN THE NO. 2 MAIN TANK

FLOAT VALVE IN THE INBOARD MAIN TANK


Float Valves for the Fuel Scavenge System
Figure 401 (Sheet 3)

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 28-15-11
 ALL  ú ú 03 Page 406 ú Feb 10/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A78553
A
747-400 MAINTENANCE MANUAL
 S 424-079
 (3)  
Put the float valve in the correct location.

 S 424-081

 (4)  
Attach the bolt and the washer (2 locations) but do not tighten the bolts until the couplings are attached to the float valve.

 S 644-054

 (5)  
Lightly lubricated the new O-rings (for the couplings) with the petrolatum.

 S 434-055

 (6)  
Install the O-rings in the couplings.

 S 434-083

 (7)  
Manually tighten the coupling to the float valve (2 locations) until no threads are shown.

 S 434-085

 (8)  
Tighten the bolts.

 S 434-087

 (9)  
Install the lockwire through the couplings.

 S 434-089

 (10)
 
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