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时间:2011-04-11 09:07来源:蓝天飞行翻译 作者:航空
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 (1) Defuel the necessary inboard main tank (AMM 28-26-00/201).
 S 864-003
 WARNING:_______OBEY ALL THE FUEL TANK PURGING AND ENTRY PRECAUTIONS. YOU CAN CAUSE AN INJURY TO A PERSON AND CAUSE DAMAGE TO THE AIRPLANE.
 (2)  
Do the purge and enter the fuel tank task (AMM 28-11-00/201).

 (3)  
Go into the fuel tank.

 S 034-004

 (4)  
Remove the nuts and the washers that attach the airplane wires and the sensor wires to the terminal block (3 locations).

 (a)  
Write down the color of the wires for the installation task.


 S 864-015
 S 034-005
 (5)  Remove the screws and the washers (5 locations) that attach the cover bracket to the mounting bracket.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 28-16-07
 ALL  ú ú 01 Page 401 ú Oct 10/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

ASEE SENSOR SINGLE POINT 
GREEN WIRE (HI-Z SHIELD)  YELLOW WIRE (LO-Z) 
WHITE WIRE (HI-Z)  TERMINAL BLOCK 
THE RESERVE TANK TRANSFER SYSTEM SINGLE POINT SENSOR ASSEMBLY FOR 
SENSOR SINGLE POINT 
(2 LOCATIONS) WASHER 
MOUNTING BRACKET  COVER BRACKET 
(2 LOCATIONS) SCREW 
FOR THE FUEL SENSOR ASSEMBLY SINGLE POINT JETTISON SYSTEM (REF ONLY) FWD (5 LOCATIONS) (5 LOCATIONS) SCREW WASHER 
RIGHT WING OPPOSITE) (LEFT WING SHOWN, SINGLE POINT SENSOR A 
Figure 401 Reserve Tank Transfer Single Point Sensor 

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 28-16-07
 ALL  ú ú 01 Page 402 ú Feb 10/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 034-006
 (6)  
Remove the screws and the washers (2 locations) that attach the sensor to the mounting bracket.

 S 024-007

 (7)  
Remove the sensor wires through the hole in the mounting bracket.

 S 024-016

 (8)  
Remove the sensor from the airplane.


 TASK 28-16-07-404-008
 3.  Reserve Tank Transfer Single Point Sensor Installation (Fig. 401)______________________________________________________
 A. References
 (1)  
AMM 28-11-00/201, Fuel Tanks

 (2)  
AMM 28-16-08/501, Reserve Tank Transfer Single Point Sensor Control Card

 (3)  
AIPC 28-41-10 Fig. 1

 (4)  
AIPC 28-41-11 Fig. 2

 (5)  
SSM 28-44-01

 (6)  
WDM 28-44-11, 28-44-12

 B.
Access

 (1)  
Location Zones 544 Inbd Main Tank (Part), Mid Spar to Rear Spar, Left 644 Inbd Main Tank (Part), Mid Spar to Rear Spar, Right

 C.
Procedure


 S 424-009
 (1)  
Put the sensor wires up through the hole in the top of the mounting bracket.

 S 424-017

 (2)  
Put the SPS into its correct position.

 S 434-010

 (3)  
Install the screws and the washers (2 locations) that attach the sensor to the mounting bracket.

 (a)  
Tighten the screws.


 S 434-011
 (4)  
Install the screws and the washers (5 locations) that attach the cover bracket to the mounting bracket.

 (a)  
Tighten the screws.


 S 434-012
 (5)  
Connect the airplane wires and the sensor wires to the studs on the terminal block with the washers and the nuts.

 (a)  
Connect the white wire to the HI-Z stud.


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 28-16-07
 ALL  ú ú 01 Page 403 ú Jun 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 747-400 MAINTENANCE MANUAL
 (b) (c)  Connect the green wire to the HI-Z SHIELD stud.Connect the yellow wire to the LO-Z stud.
 
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本文链接地址:747-400 AMM 飞机维护手册 燃油 FUEL 2(3)