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

1 - The pressure usually produced by the Boost Pumps (BP) of the fuel supply system of a large jet transport airplane is within the following range:
2 - Which of these statements about rudder limiting are correct or incorrect? 1) A rudder ratio changer system reduces the rudder deflection for a given rudder pedal deflection as the IAS increases. 2) A variable stop system limits both rudder and rudder pedal deflection as the IAS decreases.
3 - Regarding the oxygen system of a CS 25 aeroplane:
4 - In an aeroplane utilising a constant frequency AC power supply, DC power is obtained from a:
5 - In large modern aircraft, in the air conditioning system, reduction of air temperature and pressure is achieved by:
6 - The fuel supply system on a jet engine includes a fuel heating device, upstream of the main fuel filter so as to:
7 - In a gas turbine engine, the maximum gas temperature is attained:
8 - 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:
9 - In hydraulic systems of large modern transport category aircraft the fluids used are:
10 - In flight, the most commonly used anti-icing method for the wings of modern commercial aircraft fitted with turbo-jet units is: