31-04. (H) MASS AND BALANCE DETAILS OF AIRCRAFT
All questions: 34
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1. The aft centre of gravity limit is located at 2,945 m. The datum is located in front of the helicopter. Is it allowed to fly under otherwise identical conditions if a pilot is weighing 10 kg more as given?
2. (Refer to figure 031-47)
Where is the longitudinal centre of gravity at Basic Empty Mass (Delivered Weight) of the single engine piston helicopter SEPH1 located?
3. 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?
4. (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:
5. (Refer to figure 031-61)
Where has the longitudinal reference (datum plane) been defined on the twin engine transport helicopter TETH1?
