ENGINE FUEL DISTRIBUTION -FUNCTIONAL DESCRIPTION
BEJ ALL POST SB 777-71-0032 (Continued)
At low engine power, the FMU bypass fuel mixes with the boost stage fuel and goes through both cores of the FOC. At high engine power, the bypass fuel flows only through the engine core of the FOC.
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ENGINE FUEL DISTRIBUTION -FUNCTIONAL DESCRIPTION
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ENGINE FUEL CONTROL -INTRODUCTION
General
The engine fuel control system components control the flow of fuel to the engine for combustion (metered fuel). They also maintain the proper fuel temperature.
System sensors supply information that is necessary for proper operation.
Some components control the application of power to engine components. Others supply interfaces with the airplane.
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ENGINE FUEL CONTROL -INTRODUCTION
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ENGINE FUEL CONTROL -GENERAL DESCRIPTION
General
The EEC is the primary component of the engine fuel control system. The EEC uses data from engine sensors and airplane systems to control the engine operation.
Power
The EEC gets power from the airplane electrical system or the and permanent magnet alternator (PMA). The electrical load management system (ELMS) supplies airplane power to the EEC when any of these conditions occur:
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