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ATPL - Airline Transport Pilot license - Aircraft General Knowledge - Airframe, Systems, Powerplant Pagina 64

Domande Aircraft General Knowledge - Airframe, Systems, Powerplant - ATPL Pagina 64

The use of igniters is necessary on a turbo-jet: 1 - throughout the operating range of the engine 2 - for ground starts 3 - for accelerations 4 - for in-flight relights 5 - during turbulence in flight 6 - in heavy precipitation or in icing conditions The combination which regroups all of the correct statements is:4
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On the ground, the Auxiliary Power Unit (APU) can be substituted for the:4
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The use of igniters is necessary on a turbo-jet 1 - throughout the operating range of the engine 2 - for ground starts 3 - for accelerations 4 - for in-flight relights 5 - during turbulence in flight 6 - in heavy precipitation or in icing conditions The combination which regroups all of the correct statements is:4
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About a twin spool compressor:4
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Engine temperature limitations of a gas turbine engine are usually imposed due to temperature limitations on the:4
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For a subsonic airflow, in a divergent duct the:4
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By-pass turbine engines are mainly used in commercial aviation, because:4
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The accessory units driven by the accessory gearbox of a turbo-jet engine are the 1. tacho-generator N1 2. tacho-generator N2 3. thrust reverser pneumatic motors 4. AC generator and its Constant Speed Unit (CSD) 5. oil pumps 6. hydraulic pumps 7. high pressure fuel pumps The combination regrouping all the correct statements is:4
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The compressor surge effect during acceleration is prevented by the:4
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Below its design speed an axial compressor:4
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