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ATPL - Airline Transport Pilot license - Mass and Balance Pagina 12

Domande Mass and Balance - ATPL Pagina 12

Aeroplane Dry Operating mass 85000 kg Performance limited take-off mass 127000 kg Performance limited landing mass 98500 kg Maximum zero fuel mass 89800 kgFuel requirements for flight - Trip fuel 29300 kgContingency and final reserve fuel 3600 kg Alternate fuel 2800 kg.The maximum traffic load that can be carried on this flight is:4
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A revenue flight is to be made by a jet transport. The following are the aeroplane's structural limits:-Maximum Ramp Mass: 69 900 kg-Maximum Take Off Mass: 69 300 kg-Maximum Landing Mass: 58 900 kg-Maximum Zero Fuel Mass: 52 740 kgTake Off and Landing mass are not performance limited. Dry Operating Mass: 34 930 kgTrip Fuel: 11 500 kg Taxi Fuel: 250 kgContingency & final reserve fuel: 1 450 kg Alternate Fuel: 1 350 kgThe maximum traffic load that can be carried is:4
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Where is the centre of gravity of the aeroplane in the diagram?4
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Given are the following information at take-off____________________________________________________________ STATION....................MASS (kg)....ARM (cm)....MOMENT (kgcm)____________________________________________________________ Basic Empty Condition...12045.........+30......+361350Crew..................................145........-160.......-23200Freight ( 1)..........................570.......+200......+114000Freight ( 2)..........................410..........-40.......-16400Fuel.................................6045...........-8.......-48360Given that the flight time is 2 h and the estimated fuel flow will be 1050 litres per h. The specific density of fuel is 0.79. The 'Freight ( 2)' will be dropped during flight within the scope of a rescue action.Calculate the CG position at landing.4
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Given:Standard Empty Mass 1764 lbs Optional Equipment 35 lbs Pilot + Passenger 300 lbs Cargo 350 lbsRamp Fuel ( Block Fuel) 60 Gal Trip Fuel 35 GalTaxi Fuel 1.7 GalFinal Reserve Fuel 18 Gal Fuel density 6 lbs/GalDetermine the expected landing mass.4
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Length of the mean aerodynamic chord = 1 m Moment arm of the forward cargo: -0,50 m Moment arm of the aft cargo: + 2,50 mThe aircraft mass is 2 200 kg and its centre of gravity is at 25% MACTo move the centre of gravity to 40%, which mass has to be transferred from the forward to the aft cargo hold?4
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The Basic Empty Mass is 4800 kg, the Dry Operating Mass is 5050 kg and the Zero Fuel Mass is 6210 kg.If the take-off mass is 8010 kg the useful load is:4
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Given:The take-off mass of an aircraft is 8470 kgTotal fuel on board is 1600 kg including 450 kg reserve fuel and 29 kg of unusable fuel The traffic load is 770 kgWhat is the Zero Fuel Mass?4
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The maximum load per running metre of an aircraft is 350 kg / m. The width of the floor area is 2 metres. The floor strength limitation is 300 kg per square metre. Which one of the following crates (length x width x height) can be loaded directly on the floor?4
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At a given mass the CG position is at 15% MAC. If the leading edge of MAC is at a position625.6 inches aft of the datum and the MAC is given as 134.5 inches determine the position of the CG in relation to the datum.4
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ATPL - Airline Transport Pilot licenseAllenamento!
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