A torsion link assembly is installed on the landing gear to:4
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In a commercial transport aircraft the landing gear operating system is usually:4
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When a landing gear wheel is hydroplaning, its friction factor is equal to:4
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The purpose of cabin air flow control valves in a pressurisation system is to:4
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During level flight at a constant cabin pressure altitude (which could be decreased, even at this flight level), the cabin outflow valves are:4
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Cabin differential pressure means the pressure difference between:4
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The pneumatic ice protection system is mainly used for:4
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Concerning the sequential pneumatic impulses used in certain leading edge de-icing devices, one can affirm that 1 - They prevent ice formation. 2 - They are triggered from the flight deck after icing has become visible. 3 - A cycle lasts more than ten seconds. 4 - There are more than ten cycles per second. The combination which regroups all the correct statements is:4
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The air-conditioning pack of a present-day aircraft consists of several components: these include two heat exchangers the primary exchanger (P) and the secondary exchanger (S). The functions of these heat exchangers are as follows:4
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In flight, the most commonly used anti-icing method for the wings of modern commercial aircraft fitted with turbo-jet units is:4
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Other exam subjects ATPL - Airline Transport Pilot license