34-03. (H) Performance Class 2
All questions: 16
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Questions for exams: 10
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1. In performance class 2, when the wind measuring equipment has not received official approval, and there is a headwind component, to determine landing perfor¬mance an operator may take account of at:
2. In performance class 2 when there is a headwind compo¬nent, an operator, when calculating takeoff performance may take into account not:
3. In class 2 performance, with one engine failed and the others operating, a helicopter’s weight at the es¬timated landing time must allow it to climb at least at:
4. The part of the takeoff path during which, in a helicopter of Performance Class 2, an engine failure would result in a forced landing must be flown in:
5. In Performance Class 2, for a multi-engine helicopter of a total length with the rotors turning of less than 15 metres, it is not necessary to take into account ob¬stacles whose lateral margin relative to the helicopter’s flight path with the critical engine failed is greater than a certain distance (assume VFR operation at night).
