In order to provide an adequate 'buffet boundary' at the commencement of the cruise a speed of 1.3 Vs is used. At a mass of 120000 kg this is a CAS of 180 KT. If the mass of the aeroplane is increased to 135000 kg the value of 1.3 Vs will be:4
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A mass of 500 kg is loaded at a station which is located 10 metres behind the present Centre of Gravity and 16 metres behind the datum. (Assume: g = 10 m/sΒ²). The moment for that mass used in the loading manifest is:4
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An aeroplane with a two wheel nose gear and four main wheels rests on the ground with a single nose wheel load of 500 kg and a single main wheel load of 6000 kg. The distance between the nose wheels and the main wheels is 10 m. How far is the centre of gravity in front of the main wheels?4
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Just prior to departure, you accept 10 passengers additional on board who will be seated in 'compartment OC' and you have 750 kg unloaded from cargo compartment 5.The take-off centre of gravity in MAC % (Mean Aerodynamic Chord) will be located at:4
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What are the standard masses used for crew?4
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The centre of gravity is the4
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The BEM of an aircraft is 30000 kg. Given the following data calculate the DOM: Catering = 300 kg. Crew = 600 kg. Trip Fuel = 1200 kg. Unusable Fuel = 30 kg. Traffic Load = 2500 kg4
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The operating mass of an aeroplane is:4
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The maximum intensity floor loading for an aeroplane is given in the Flight Manual as 650 kg per square metre. What is the maximum mass of a package which can be safely supported on a pallet with dimensions of 80 cm by 80 cm?4
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Given: Total mass 2900 kg. Centre of gravity (cg) location station: 115. Aft CG limit station: 116. The maximum mass that can be added at station 130 is:4
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Other exam subjects ATPL - Airline Transport Pilot license