34-04. (H) Performance Class 1 – Helicopters Certificated Under Cs 29
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1. In Performance Class 1 , for a multi-engine helicopter of a total length with the rotors turning of less than 15 m, it is not necessary to take into account obstacles whose lateral margin relative to the helicopter’s flight path with the critical engine failed is greater than a certain distance.
2. 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:
3. Performance Class 1 and 2 helicopters. An Operator shall ensure that if the flight will be conducted at any time out of sight with the surface (CPUI):
4. Assuming an engine failure has occurred during a VFR takeoff, a Performance Class 1 helicopter which plans a turn in the climb of more than 15° must be capable of clearing vertical obstructions by:
5. The part of the takeoff in both Performance Class 1 and 2 up to and including the TDPIDPATO shall be conducted in sight of the surface.
