31-04. (H) MASS AND BALANCE DETAILS OF AIRCRAFT
Всего заданий: 34
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1. To measure the mass and CG-position of an aircraft, it should be weighed with a minimum of:
2. From the attached data sheet, what is the forward CG limit for an aircraft with a mass of 3.500 Ib?
3. The following results were obtained after weighing a helicopter:
Mass at front point: 300 kg
Mass at right rear point: 1.100 kg
Mass at left rear point: 950 kg
It is given that the front point is located 0,30 m left of the longitudinal axis and the rear points are symmetrically located 1,20 m from this axis. The helicopter lateral CG position relative to the longitudinal axis is:
4. An aircraft 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 6.000 kg. The distance between the nose wheels and the main wheels is 10 meters. How far is the centre of gravity in front of the main wheels?
5. (Refer to figure 031-57)
Referring to the Pilot’s Flight Manual for the transport helicopter TETH1, the maximum load for the aft cargo bay in section B Is:
