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Old 19th Aug 2005, 07:27
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LEM
 
Join Date: May 2003
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Question B737 Fuel Pumps Dc Current Control

Each Fuel Pump is Ac powered and DC controlled.

For example, the left aft main pump is powered by TFR bus1, and controlled by DC Bus1.

If the DC Bus1 was failed (like in the case where TR1 is failed and you capture the Glideslope... , is the pump going to "stay in the last position", or is it going to fail?
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