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Mass and Balance - ATPL - Airline Transport Pilot Licence

Test 10 domande Mass and Balance, tempo libero

1 - In cruise flight, a centre of gravity moving aft will: Decrease longitudinal static stability Not change the manoeuvrability Have no effect on longitudinal static stability Increase longitudinal static stability

2 - The mass displacement caused by landing gear extension: Does not create a longitudinal moment Creates a pitch-up longitudinal moment Creates a pitch-down longitudinal moment Creates a longitudinal moment in the direction (pitch-up or pitch-down) determined by the type of landing gear

3 - The aeroplane has a Take Off Mass of 58 000 kg. At this mass the range of safe CG positions, as determined from the appropriate graph in the loading manual, is: Forward limit 8.2% MAC aft limit 26.2% MAC Forward limit 9.5% MAC aft limit 26.1% MAC Forward limit 8.0% MAC aft limit 26.5% MAC Forward limit 8.5% MAC aft limit 26.1% MAC[see Annex]

4 - The loaded centre of gravity (cg) of an aeroplane is 713 mm aft of datum. The mean aerodynamic chord lies between station 524 mm aft and 1706 mm aft. The cg expressed as% MAC (mean aerodynamic chord) is: 60 % 41 % 10 % 16 %

5 - The responsibility for determination of the mass of 'operating items' and 'crew members' included within the Dry Operating Mass lies with The authority of the state of registration. The commander. The person compiling the weighing schedule. The operator.

6 - The take-off mass of an aeroplane is 117 000 kg, comprising a traffic load of 18 000 kg and fuel of 46 000 kg. What is the dry operating mass? 64 000 kg 53 000 kg 99 000 kg 71 000 kg

7 - From the loading manual for the transport aeroplane, the aft cargo compartment has a maximum total load of:

9232 kg 1568 kg 4187 kg 3062 kg

8 - A load placed forward of the datum Has a negative arm and therefore generates a negative mass and moment Has a positive arm and therefore generates a positive mass and moment Has a negative arm and therefore generates a negative moment Has a positive arm and therefore generates a positive moment

9 - By adding to the basic empty mass the following fixed necessary equipment for a specific flight (catering, safety and rescue equipment, fly away kit, crew), we get: Zero fuel mass Take-off mass Landing mass Dry operating mass

10 - With respect to a single-engine piston powered aeroplane, determine the zero fuel moment (lbs.In./100) in the following conditions:Basic Empty Mass: 2415 lbs.Arm at Basic Empty Mass: 77,9 In. Cargo Zone A: 350 lbs.Baggage Zone B: 35 lbs.Pilot and front seat passenger: 300 lbs (total)

6675 2496,3 2548,8 2311,8

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