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Home > Training for exam quizzes ATPL, PPL(A), PPL(H), BPL Hot Air, BPL Gas, SPL - Sailplane, EASA 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 - The empty mass of an aircraft is recorded in The loading manifest. It differs from Dry Operating Mass by the value of the 'useful load'. The weighing schedule. If changes occur, due to modifications, the aircraft must be re-weighed always. The loading manifest. It differs from the zero fuel mass by the value of the 'traffic load'. The weighing schedule and is amended to take account of changes due to modifications of the aircraft.

2 - 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? 6899 kg 6420 kg 6129 kg 6870 kg

3 - An aeroplane, which is scheduled to fly an oceanic sector, is due to depart from a high altitude airport in the tropics at 1400 local time. The airport has an exceptionally long runway. Which of the following is most likely to be the limiting factor(s) in determining the take - off mass ? Maximum zero fuel mass. Altitude and temperature of the departure airfield. En route obstacle clearance requirements. Maximum certificated take - off mass.

4 - Basic Empty Mass is: Dry Operating Mass minus fuel load. Dry Operating Mass minus traffic load. A component of Dry Operating Mass. The actual take-off mass minus traffic load.

5 - An aeroplane is weighed and the following recordings are made: nose wheel assembly scale 5330 kgleft main wheel assembly scale 12370 kg right main wheel assembly scale 12480 kgIf the 'operational items' amount to a mass of 1780 kg with a crew mass of 545 kg, the empty mass, as entered in the weight schedule, is 28400 kg 31960 kg 30180 kg 32505 kg

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

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9232 kg 1568 kg 4187 kg 3062 kg

7 - A location in the aircraft which is identified by a number designating its distance from the datum is known as: Station. Index. MA Moment.

8 - 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: Increased to 191 KT, drag will increase and air distance per kg of fuel will decrease. Increased to 202 KT but, since the same angle of attack is used, drag and range will remain the same. Increased to 191 KT, drag will decrease and air distance per kg of fuel will increase. Unaffected as Vs always occurs at the same angle of attack.

9 - Considering only structural limitations, on very short legs with minimum take-off fuel, the Traffic Load is normally limited by: Maximum Zero Fuel Mass. Actual Landing Mass. Maximum Take-off Mass. Maximum Landing Mass.

10 - To measure the mass and CG-position of an aircraft, it should be weighed with a minimum of: 3 points of support 4 point of support 1 point of support 2 points of support

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