ED Decision 2003/16/RM
The take-off performance must be determined and scheduled so that, if one engine fails at any time after the start of take-off, the rotorcraft can:
(a) Return to and stop safely on, the take-off area; or
(b) Continue the take-off and climb-out, and attain a configuration and airspeed allowing compliance with CS 29.67(a)(2).
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