APU Flashcards
The APU supplies bleed air and electrical power.
Electrical power has priority over bleed air.
The APU can be started and operated to the airplane maximum operating altitude.
Electrical power is available throughout the airplane operating envelope.
With the APU SEL in the OFF position;
the APU bleed air isolation valve is closed, a normal shutdown is initiated and the auto shutdown fault logic is reset.
ON is the APU operating position.
Moving the APU SEL to the ON position
opens the APU fuel valve and inlet door,
activates an AC or DC fuel pump and powers the APU controller.
START is a momentary position
spring-loaded to return to ON. It initiates the automatic start sequence.
The APU FAULT light is illuminated if
an APU fault and / or fire is detected,
if the APU has shutdown due to a fault and / or fire,
or momentarily during the APU controller self-test.
The APU is started either by
an electric start motor or an air turbine starter.
APU Battery
Main Battery for APU
APU Battery powers Electric Starter
Main Battery
Inlet Door
Fuel Valve
Fire Detection System
The air turbine starter uses
bleed duct pressure or ground air.
Starter selection is automatic.
The air turbine starter has
priority over the electric start motor when there is sufficient bleed air duct pressure.
APU fuel is supplied from
the left fuel manifold by any operating AC fuel pump or the DC fuel pump.
With AC power available and the APU SEL in the ON position,
the left forward fuel pump operates automatically.
If AC power is not available or no AC pump pressurizes the left fuel manifold
the DC pump in the left main tank provides APU fuel.
When the APU air inlet door reaches the full open position
the starter engages.
When the APU reaches approximately 50 % RPM
the starter disengages and ignition is turned off.