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时间:2011-04-11 09:15来源:蓝天飞行翻译 作者:航空
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 (5)
AMM 28-41-02/401, Fuel Quantity Compensator

 (6)
AMM 28-41-11/401, Fuel Quantity Densitometer

 (7)
AMM 51-31-01/201, Seals and Sealing

 (8)
AMM 57-12-01/401, Inspar Removable Rib

 (9)
SRM 51-50-02, Support of Airplane in Jigged Position

 (10)
 AIPC 28-41-02, Fig. 1

 (11)
 AIPC 28-41-02, Fig. 2

 (12)
 AIPC 28-41-03, Fig. 1

 (13)
 AIPC 28-41-09, Fig. 1

 (14)
 AIPC 28-41-12, Fig. 1


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 28-41-09
 ALL  ú ú 01 Page 414 ú Oct 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
 D.

E.
F.
A
747-400 MAINTENANCE MANUAL
 (15)
 SWPM 20-20-00, Electrical Bond and Ground

 (16)
 SSM 28-41-01Access

 (1)  
Location Zones 544 Inbd Main Tank (Part), Mid Spar to Rear Spar, Left 545 Inbd Main Tank (Part), Mid Spar to Rear Spar, Left 546 Outbd 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 644 Inbd Main Tank (Part), Mid Spar to Rear Spar, Right 645 Inbd Main Tank (Part), Mid Spar to Rear Spar, Right 646 Outbd 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


Prepare the Airplane for FQIS Wire Bundle Installation
 S 864-020
 WARNING:_______OBEY THE PURGING AND FUEL TANK ENTRY PRECAUTIONS. FAILURE TO OBEY THE PRECAUTIONS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
 (1)  
Purge and prepare to go into the applicable fuel tank(s), if it is not accomplished (AMM 28-11-00/201).

 S 864-021

 (2)  
Make sure that the airplane is in the configuration prepared for the wire bundle removal.

 S 434-022

 (3)  
Make sure that an O-ring is installed in the groove of the FQIS wire


 bundle connector.Procedure
 S 944-023
 WARNING:_______OBEY THE FUEL TANK ENTRY PRECAUTIONS. FAILURE TO OBEY THE FUEL TANK ENTRY PRECAUTIONS COULD CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
 (1)  
Obey the fuel tank entry precautions (AMM 28-11-00/201).

 S 944-024

 (2)  
Go into the inboard fuel tank to where the wire bundle connector is to be installed on the spar.

 S 394-025

 (3)  
Make sure that the mating surface on the spar and the receptacle is clean (AMM 51-31-01/201).


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 28-41-09
 ALL  ú ú 01 Page 415 ú Oct 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 424-026
 (4)  Put the wire bundle connector in the hole in the spar.
 S 434-027
 (5)  Hold the connector in its position while other persons out of the
 tank install the connector jamnut.
 S 434-028
 (6)  Tighten the connector jamnut to 200-250 pound-inches.
 S 394-029
 (7)  Apply the sealant around the edge of the connector flange in the
 tank.
 S 434-032
 (8)  Put the wire bundle in its position from the connector to all of the
 applicable tank components.
 (a)  Loosely attach the wire bundle in its position with clamps.
 NOTE:____ Do not tighten the clamps.

 S 394-034
 (9)  
Make sure that before the wire bundle goes through the electrical seal areas the remaining seal material is removed.

 (a)  
Clean and prepare the seal area (AMM 51-31-01/201).


 S 434-035
 (10)
 If the wire bundle is for the outboard tanks, put the remaining wire through the tank divider seal area.

 S 434-036

 (11)
 Examine the wire bundle for critical installation point flag markers in the inboard tank.

 (a)  
One or two flag markers are used.
 
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