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Home > Training for exam quizzes ATPL, PPL(A), PPL(H), BPL Hot Air, BPL Gas, SPL - Sailplane, EASA Drone, FAA Drone > Mass and Balance - ATPL - Airline Transport Pilot license

Quiz Mass and Balance - ATPL - Airline Transport Pilot license

Test 10 Questions ATPL - Airline Transport Pilot license - Mass and Balance, no time limit

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1 - . Allowed traffic load is the difference between: Allowed take off mass and basic empty mass. Allowed take off mass and basic empty mass plus trip fuel. Operating mass and basic empty mass. Allowed take off mass and operating mass.

2 - The centre of gravity of an aircraft Is in a fixed position and is unaffected by aircraft loading. May only be moved if permitted by the regulating authority and endorsed in the aircraft's certificate of airworthiness. Must be maintained in a fixed position by careful distribution of the load. Can be allowed to move between defined limits.

3 - Which of the following corresponds to zero fuel mass? Operating mass plus luggage of passengers and cargo. Operating mass plus passengers and cargo. The take-off mass of an aeroplane minus all usable fuel. Take-off mass minus fuel to destination and alternate.

4 - An aircraft is weighed prior to entry into service. Who is responsible for deriving the Dry Operational Mass from the weighed mass by the addition of the 'operational items' ? The Operator. The commander of the aircraft. The aircraft manufacturer or supplier. The appropriate Aviation Authority.

5 - From the Loading Manual for the transport aeroplane, the maximum load that can be carried in that section of the aft cargo compartment which has a balance arm centroid at:

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835.5 inches is 6752 kg 835.5 inches is 3062 kg 421.5 inches is 2059 lbs 421.5 inches is 4541 kg

6 - The Dry Operating Mass includes: Crew and crew baggage, catering, removable passenger service equipment, potable water and lavatory chemicals. Passengers baggage and cargo. Fuel and passengers baggage and cargo. Unusable fuel and reserve fuel.

7 - The maximum certificated take - off mass is: A take - off limiting mass which is governed by the gradient of climb after reaching V2 . A take - off limiting mass which is affected by the aerodrome altitude and temperature. Limited by the runway take off distance available. It is tabulated in the Flight Manual. A structural limit which may not be exceeded for any take - off.

8 - If individual masses are used, the mass of an aircraft must be determined prior to initial entry into service and thereafter Only if major modifications have taken place. At regular annual intervals. At intervals of 9 years. At intervals of 4 years if no modifications have taken place.

9 - The term 'useful load' as applied to an aircraft includes Traffic load plus usable fuel. The revenue-earning portion of traffic load plus useable fuel. The revenue-earning portion of traffic load only. Traffic load only.

10 - In determining the Dry Operating Mass of an aeroplane it is common practice to use 'standard mass' values for crew. These values are Flight crew 85 kg., cabin crew 75 kg. each. These do not include a hand baggage allowance. Flight crew 85 kg., cabin crew 75 kg. each. These are inclusive of a hand baggage allowance. Flight crew (male) 88 kg. (female) 75 kg., cabin crew 75 kg. each. These do not include an allowance for hand baggage. Flight crew (male) 88 kg. (female) 75 kg., cabin crew 75 kg. each. These include an allowance for hand baggage.

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