(a) The operating maneuvering speed, VO; and
(b) The maximum landing gear operating speed V
(c) For reciprocating multiengine-powered airplanes of more than 6,000 pounds maximum weight, and turbine engine-powered airplanes, the maximum value of the minimum control speed, VMC(one-engine-inoperative) determined under §23.149(b).
[Amdt. 23–7, 34 FR 13097, Aug. 13, 1969, as amended by Amdt. 23–45, 58 FR 42166, Aug. 6, 1993; Amdt. 23–50, 61 FR 5193, Feb. 9, 1996]
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