Elec sources for starting?
Ground power
Engine driven generator
APU battery provided DC ESS bus powered
Key altitudes for function
Starts below FL200
Supplied bleed air and elec power <22,500’
Only 1 APU generator can operate in flight
Basic structure
2 rotors
N1 - Power rotor
N2 - High Pressure rotor
Air enters via the flap which closes automatically when APU not in use
2 APU generators (A and B) that supply constant 400Hz elec. Each cam replace any other generator and total AC can be supplied by both gens operating (although only 1 can operate in flight)
ECB? Electrical Control Box
Controls operation, start and shutdown of APU
How long wait between APU MASTER SW and APU START PB?
5 secs