CAA NZ Basic Turbine Knowledge (Helicopter) Exam study materials
CAA NZ Basic Turbine Knowledge (Helicopter) Exam study resources

CAA NZ Basic Turbine Knowledge (Helicopter) Exam: Starting and Engine Control Systems

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

All guide sections

Starting and Engine Control Systems

Starting and Engine Control Systems tests the start sequence, the electronic or hydromechanical control, and the protections that prevent a hot or hung start. The examiner expects sequence logic, not just button-pushing.

Core rules

  • Typical sequence: starter cranks, ignition on, fuel on, light-off, acceleration, starter cut-out, idle, generator online.
  • The control schedules fuel to keep TGT within limits while accelerating; it may use N1, N2, TGT and rate of change.
  • FADEC or EECU provides metering, limit protection, overspeed protection and fault recording; some installations retain hydromechanical backup.
  • A hot start is a rapid TGT rise above limit, often from excess fuel or low airflow.
  • A hung start is stagnation below idle, often from weak starter, low battery or fuel scheduling.
  • Starter duty cycles protect the starter and battery.

Worked example

The start limit is 900°C TGT. At 35% N1 the TGT passes 930°C and is still rising at 40°C/s. The correct action is to abort: fuel off, ignition off, continue cranking to clear fuel vapour, then investigate. Do not wait for 1000°C to confirm the trend. Record the peak TGT and duration for the maintenance manual exceedance check.

Traps

  • Continuing a start because the engine is almost there.
  • Re-engaging the starter before the duty cycle expires.
  • Assuming a hung start is always a fuel control fault.
  • Forgetting to clear unburned fuel after an aborted start.
  • Resetting a FADEC fault without recording it.