CAA NZ Basic Turbine Knowledge (Aeroplane) study materials
CAA NZ Basic Turbine Knowledge (Aeroplane) study resources

CAA NZ Basic Turbine Knowledge (Aeroplane): Auxiliary and Accessory Systems

CAA NZ Basic Turbine Knowledge (Aeroplane) · Work through your exam, one topic at a time.

All guide sections

Auxiliary and Accessory Systems

What this domain tests

This domain covers the APU, bleed air, anti-ice and accessory gearbox drives, and how they interact with engine operation.

Core rules

  • The APU is a small turbine that drives a generator and bleed-air compressor. It provides electrical power, air conditioning and bleed air for engine starting. It has altitude and bleed limits.
  • Bleed air is taken from the compressor for anti-ice, pressurisation and starting; using it reduces engine thrust and increases EGT.
  • The accessory gearbox drives the fuel pump, oil pump, hydraulic pump, generator, starter and tachometers. A gearbox failure can affect several systems at once.
  • Anti-ice uses hot bleed air on engine intakes and wings; it must be on before icing is encountered.

Worked example

An APU supplies 40 lb/min of bleed air. Each engine start needs 25 lb/min. Therefore only one engine can be started at a time; attempting both would starve the starter and cause a hung start. Reasoning: bleed air is a shared resource, and the APU's limit is the constraint, not the starter's capability.

Traps

  • Using APU bleed above its altitude limit.
  • Forgetting that engine anti-ice changes thrust and EGT.
  • Assuming the accessory gearbox only drives one pump.
  • Leaving anti-ice on in clear air; it wastes bleed air and fuel.

Key points

  • The APU supplies electrical power, air conditioning and start bleed air.
  • APU bleed has altitude and flow limits.
  • Bleed air for anti-ice and pressurisation reduces thrust and raises EGT.
  • The accessory gearbox drives fuel, oil and hydraulic pumps, the generator and starter.
  • Anti-ice must be on before icing conditions.