§29.65 Climb: all engines operating.

[(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 paragraph (a) of this section must provide a steady climb gradient of at least 1:6 under standard sea level conditions. (c) [[Removed.]]