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Home > Training for exam quizzes ATPL, PPL(A), PPL(H), BPL Hot Air, BPL Gas, SPL - Sailplane, EASA Drone > Aircraft General Knowledge - Airframe, Systems, Powerplant - ATPL - Airline Transport Pilot license

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

Test 10 Questions ATPL - Airline Transport Pilot license - Aircraft General Knowledge - Airframe, Systems, Powerplant, no time limit

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1 - The principle of FAIL SAFE design of an aircraft is based on the: Replacement Of Parts After A Given Number Of Cycles Or Hours Of Use. Redundancy of the structure or equipment. Capability to withstand a certain amount of weakening of the structure without catastrophic failure. Monitoring Of Critical Parameters And The Replacement Of Parts If A Limit Value Is Exceeded.

2 - In a pressurized aircraft whose cabin altitude is 8000', a crack in a cabin window makes it necessary to reduce the differential pressure to 5 psi.The flight level to be maintained in order to keep the same cabin altitude is:

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Fl 230 FL 180 FL 280 Fl 340

3 - The modern anti-skid processes are based on the use of a computer whose input data is: 1. idle wheel speed (measured)2. braked wheel speed (measured)3. brake temperature (measured)4. desired idle wheel train slipping rate5. tire pressur The combination regrouping all the correct statements is: 1, 2, 4. 1, 3. 2, 4. 1, 2, 3, 4, 5.

4 - An aeroplane equipped with reversible flight controls: Need Not Be Equipped With A Separate Gust Lock System. Does not require an artificial feel system. Is Equipped With Simple Spring Type Feel Units. Does Not Have Mechanical Back-up.

5 - Regarding a jet engine: 1) The maximum thrust remains constant as the pressure altitude decreases. 2) The specific fuel consumption remains constant as the pressure altitude decreases at constant TAS. 1) Is Correct, 2) Is Correct. 1) is incorrect, 2) is correct. 1) is correct, 2) is incorrect. 1) is incorrect, 2) is incorrect.

6 - On a transport type aircraft the fuel tank system is vented through: A Pressure Regulator In The Wing Tip. Bleed air from the engines. Ram air scoops on the underside of the wing. The Return Lines Of The Fuel Pumps.

7 - In a gas turbine engine, the maximum gas temperature is attained: Across The Turbine In the cooling airflow around the flame tube Within the combustion chamber At The Entry To The Exhaust Unit

8 - In the cockpit of a transport airplane, at least one manual fire-extinguisher must be conveniently located containing: Powder. Halon. Special fluids. Water.

9 - The advantages of grounding the negative pole of the aircraft structure are: 1) weight saving 2) easy fault detection 3) increase of short-circuit risk 4) reduction of short-circuit risk 5) circuits are not single-wired linesThe combination regrouping all the correct statements is: 2, 3, 2005 1, 2, 2003 1, 3, 2005 1, 2, 4

10 - Which of these statements about a gust lock system are correct or incorrect? 1) Irreversible flight controls should have a gust lock. 2) Manual flight controls should have a gust lock. 1) Is Incorrect, 2) Is Incorrect. 1) Is Correct, 2) Is Incorrect. 1) Is Correct, 2) Is Correct. 1) is incorrect, 2) is correct.

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