When changing power on engines equipped with constant-speed propeller, engine overload is avoided by:4
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When increasing true airspeed with a constant engine RPM, the angle of attack of a fixed pitch propeller:4
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For piston engines, mixture ratio is the ratio between the:4
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In a turbo-jet, the purpose of the turbine is to ...4
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For a fan jet engine, the by-pass ratio is the:4
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In a compressor stage of a jet engine, the sequence is:4
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In the axial flow compressor of a turbo-jet engine, the flow duct is tapered. Its shape is calculated so as to:4
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In the stator of a turbine, the speed V and static pressure Ps vary as follows:4
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The purpose of a compressor bleed valve is to prevent surging:4
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A 'fan' stage of a ducted-fan turbine engine is driven by:4
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Other exam subjects ATPL - Airline Transport Pilot license