Ignition & Starting Systems: Powerplant practice questions
Five original questions on ignition & starting systems, each with the answer, an explanation and an FAA-H-8083-32B page reference.
- Starting without a battery under all conditions
- Only one spark plug per cylinder
- Variable spark timing based on engine conditions
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C. Variable spark timing based on engine conditions Spark timing varies over the operating range with engine load.
Reference: FAA-H-8083-32B, Ch. 4, p. 4-16
- Direct cranking electric starter
- Inertia starter
- Air turbine starter
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A. Direct cranking electric starter An electric motor engages a gear to turn the crankshaft directly.
Reference: FAA-H-8083-32B, Ch. 5, p. 5-2
- A starter with a backup battery
- A generator driven by the starter motor
- A unit that cranks a turbine engine for starting and then works as a generator
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C. A unit that cranks a turbine engine for starting and then works as a generator It switches to a generator after self-sustaining speed, saving weight and space.
Reference: FAA-H-8083-32B, Ch. 5, p. 5-10
- Compressed air from an APU, ground cart or another engine
- Hydraulic pressure from the engine pump
- The aircraft battery directly
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A. Compressed air from an APU, ground cart or another engine An axial turbine turns a drive coupling through reduction gears and a clutch.
Reference: FAA-H-8083-32B, Ch. 5, p. 5-12
- The engine fails to light off
- The exhaust temperature exceeds limits
- The engine lights off but does not accelerate to idle rpm
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C. The engine lights off but does not accelerate to idle rpm A hung start lights off but will not accelerate to idle rpm.
Reference: FAA-H-8083-32B, Ch. 10, p. 10-57
355 original questions with handbook citations, 385 flashcards, 20 interactive diagrams and timed mocks scored by ACS area. $29 one-time, 14-day refund. The free sample covers reciprocating engines and ignition, with no account or card needed.
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What does the Powerplant test cover on ignition & starting systems?
The Aviation Mechanic Powerplant ACS lists ignition & starting systems as one of its areas. The FAA reference for this material is FAA-H-8083-32B.