CS 29.65 Climb: All engines operating
ED Decision 2003/16/RM
(a) The steady rate of climb must be determined:
(1) With maximum continuous power;
(2) With the landing gear retracted; and
(3) At VY for standard sea-level conditions and at speeds selected by the applicant for other conditions.
(b) For each Category B rotorcraft except helicopters, the rate of climb determined under sub-paragraph (a) must provide a steady climb gradient of at least 1:6 under standard sea-level conditions.
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