34-04. (H) Performance Class 1 – Helicopters Certificated Under Cs 29
All questions: 34
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1. When enroute in a Performance Class 1 helicopter which has had an engine failure, the mass of the aircraft must be such that a rate of climb may be achieved and maintained. When not visual with the surface, that rate of climb is:
2. In Performance Class 1, with one engine failed and the others operating normally, the helicopter’s weight at the estimated time of landing must be such that a rate of climb of at least 150 ft/min at 1.000 ft above the altitude of:
3. Obstacles beyond 10R may be disregarded in Perfor¬mance Class 1:
4. In Performance Class 1, 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:
5. In performance class 1, having cleared the elevated heliport or heliplatform’s edge, in case of an engine failure after the takeoff decision point, the helicopter can clear any obstacle until the end of the takeoff required distance with a margin of:
