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时间:2011-09-29 14:27来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

Figure 601 (Sheet 1)

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 28-22-00
 ALL  ú ú 01 Page 602 ú Jun 20/96

F80625
A
757
MAINTENANCE MANUAL


Boost Pump and Override Pump Inspection
Figure 601 (Sheet 2)

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 ALL  ú ú 01 Page 603 ú Jun 20/96

F80637
A
757
MAINTENANCE MANUAL


Fuel Pump Inspection Data Sheet
Figure 602 (Sheet 1)

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 28-22-00
 ALL  ú ú 01.1 Page 604 ú Sep 28/02

G00604
A

757
MAINTENANCE MANUAL

PLEASE PROVIDE ADDITIONAL DATA HERE

PARTNUMBER  SERIALNUMBER COMMENTS


Fuel Pump Inspection Data Sheet
Figure 602 (Sheet 2)

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 ALL  ú ú 01.1 Page 605 ú Sep 28/02

G00269
A 757 MAINTENANCE MANUAL
 (2)  
Megohmmeter:

 (a)  
QuadTech 1864, (or equivalent): A special megohmmeter is necessary to do the electrical check with the fuel pump installed on the airplane. The megohmmeter must have 10 VDC and 500 VDC voltage supply options with a maximum short circuit current of 5 milliamperes. The QuadTech model 1864 megohmmeter is recommended.


 QuadTech (OPK96) 100 Nickerson Road Marlborough, Massachusetts USA 01752-4696 Phone: (800) 253-1230
 NOTE: Test equipment for the low voltage on-wing safety check
____ (initial check) must be limited to a maximum short circuit power dissipation of 0.05 Watts. Test equipment for the high voltage on-wing check (final check) must be limited to a maximum short circuit power dissipation of
 2.5 Watts.
 C. References
 (1)  
AMM 06-44-00/201, Wings (Major Zones 500 and 600) Access Doors and Panels

 (2)  
AMM 24-22-00/201, Manual Control
 
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本文链接地址:757 AMM 飞机维护手册 燃油 CHAPTER 28 - FUEL 3(9)