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Bob Moore wrote in
46.128: Bertie the Bunyip wrote Losing one in either is theoretically about the same. Same goes for a three engined airplane. Some additional information. (b) Takeoff; landing gear retracted. In the takeoff configuration existing at the point of the flight path at which the landing gear is fully retracted, and in the configuration used in §25.111 but without ground effect: (1) The steady gradient of climb may not be less than 2.4 percent for two- engine airplanes, 2.7 percent for three-engine airplanes, and 3.0 percent for four-engine airplanes, at V2with: (i) The critical engine inoperative, the remaining engines at the takeoff power or thrust available at the time the landing gear is fully retracted, determined under §25.111, unless there is a more critical power operating condition existing later along the flight path but before the point where the airplane reaches a height of 400 feet above the takeoff surface; I was going to say that ![]() Bertie |
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