APU Flashcards
What is the primary purpose of the APU?
To provide electrical power to the aircraft buses as a backup to the engine generators.
What is the secondary purpose of the APU?
To provide pneumatic pressure for engine start and air conditioning.
What kind of generator is connected to the APU?
A 40kva AC generator.
What is the maximum operating altitude of the APU?
41 000 ft.
What is the maximum height to start the APU?
37 000 ft.
What is the APU ECS bleed altitude limit?
25 000 ft.
What is the maximum altitude for an APU ground start.
15000 ft.
Air from the APU inlet door is ducted to where?
The APU compressor and the APU oil cooler.
Where is the APU air inlet door?
The upper right side of the fuselage.
What components are mounted onthe APU accessory gearbox?
The generator, oil pump and fuel pump.
ECU speed sensor, starter motor and fuel control unit.
What variables control the amount the APU air inlet door is opened?
APU speed, airspeed (MACH number) and weight on wheels (WOW) sensor.
If the inlet door position fails (or the door position is unknown), what limitations apply in flight?
Airspeed is limited to 220 kt unless the APU is running.
Where does the fuel for the APU come from?
The left collector box.
What does the APU load control valve safeguard against?
Excessive EGTs.
Is the APU able to supply anti-ice bleed air?
No.