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时间:2011-04-11 09:13来源:蓝天飞行翻译 作者:航空
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On the main power distribution panel, P6: 1) 6F17, CTR L & MAIN 3 JTSN VLV 2) 6G2, FUEL SHUTOFF VALVE ENG 2 3) 6L15, FUEL XFEED VALVE ENG 2

 (b)  
On the overhead circuit breaker panel, P7: 1) 7H21, FUEL XFR VLV MAIN 1 2) 7H23, FUEL XFR VALVE RES 2B & 3B


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 28-22-14
 ALL  ú ú 14 Page 404 ú Oct 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 (c)  
On the DC power distribution panel, P180: 1) 180B2 or 180M9, FUELING LTS - HOT

 or FUELING PWR - HOT BAT 2) 180C25, FUELING LTS PANEL 3) 180C26, FUELING LTS RECP

 (d)  
On the left power distribution center, P414: 1) 414F22, FUELING PWR


 S 914-035
 WARNING: DO NOT TOUCH THE CARD BEFORE YOU DO THE PROCEDURE FOR DEVICES
_______ THAT ARE SENSITIVE TO ELECTROSTATIC DISCHARGE. ELECTROSTATIC DISCHARGE CAN CAUSE DAMAGE TO THE CARD.
 (2)  
Do the procedure for devices that are sensitive to electrostatic discharge (AMM 20-41-02/201).

 S 024-028

 (3)  
Remove the card A9 from the fuel system card file
 (AMM 20-11-22/401).

 

 TASK 28-22-14-404-011
 5. Valve Position Logic Card A9 Installation (Fig. 401)
_________________________________________
 A. References
 (1)  
AMM 20-11-22/401, E/E Rack-Mounted Module

 (2)  
AMM 20-41-02/201, Electrostatic Discharge Sensitive Devices

 (3)  
AIPC 28-15-60 Fig. 1

 (4)  
SSM 28-16-01, SSM 28-16-02, SSM 28-21-07 Sht. 1, SSM 28-22-01, SSM 28-22-02, SSM 28-31-01

 (5)  
WDM 28-16-11, WDM 28-16-13, WDM 28-16-14, WDM 28-22-11, WDM 28-22-22 WDM 28-31-11

 B.
Access

 (1)  
Location Zone 115 Area Between Nose Gear Well and Fuselage, Left

 C.
Procedure


 S 914-038
 WARNING: DO NOT TOUCH THE CARD BEFORE YOU DO THE PROCEDURE FOR DEVICES
_______ THAT ARE SENSITIVE TO ELECTROSTATIC DISCHARGE. ELECTROSTATIC DISCHARGE CAN CAUSE DAMAGE TO THE CARD.
 (1)  Do the procedure for devices that are sensitive to electrostatic discharge (AMM 20-41-02/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 28-22-14
 ALL  ú ú 15 Page 405 ú Oct 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 424-029
 (2)  
Install the card in the fuel system card file at location A9 (AMM 20-11-22/401).

 S 414-013

 (3)  
Put the coverplate on the fuel system card file.

 S 434-034

 (4)  
Install the screws (10 locations) that attach the coverplate to the fuel system card file.

 S 864-014

 (5)
Remove the DO-NOT-CLOSE tags and close these circuit breakers:

 (a)  
On the main power distribution panel, P6: 1) 6F17, CTR L & MAIN 3 JTSN VLV 2) 6G2, FUEL SHUTOFF VALVE ENG 2 3) 6L15, FUEL XFEED VALVE ENG 2

 (b)  
On the overhead circuit breaker panel, P7: 1) 7H21, FUEL XFR VLV MAIN 1 2) 7H23, FUEL XFR VALVE RES 2B & 3B

 (c)  
On the DC power distribution panel, P180: 1) 180B2 or 180M9, FUELING LTS - HOT

 or FUELING PWR - HOT BAT 2) 180C25, FUELING LTS PANEL 3) 180C26, FUELING LTS RECP

 (d)  
On the left power distribution center, P414: 1) 414F22, FUELING PWR


 S 724-044
 (6)  Do this Task: Valve Position Logic Card A9 Operational Test (AMM 28-22-14/501).
 TASK 28-22-14-004-015
 6.  Valve Position Logic Card A11 Removal (Fig. 401)_____________________________________
 A. References
 (1)  
AMM 20-11-22/401, E/E Rack-Mounted Module

 (2)  
AMM 20-41-02/201, Electrostatic Discharge Sensitive Devices

 (3)  
AIPC 28-15-60 Fig. 1

 (4)  
SSM 28-16-01, SSM 28-16-02, SSM 28-21-07 Sht. 2, SSM 28-22-01, SSM 28-02-02, SSM 28-31-01


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