Large transport category airplanes: Turbine engine powered; Limitations; Destination and alternate airports.

CFR · 2024-01-01 · US · Title 14

(a) No program manager or any other person may permit a turbine engine powered large transport category airplane on a program flight to take off (b) Except as provided in paragraph (c) of this section, no program manager or any other person may permit a turbine engine powered large transport category airplane on a program flight to take off that airplane unless its weight on arrival, allowing for normal consumption of fuel and oil in flight (in accordance with the landing distance in the Airplane Flight Manual for the elevation of the destination airport and the wind conditions expected there at the time of landing), would allow a full stop landing at the intended destination airport within 60 percent of the effective length of each runway described below from a point 50 feet above the intersection of the obstruction clearance plane and the runway. For the purpose of determining the allowable landing weight at the destination airport, the following is assumed: (1) The airplane is landed on the most favorable runway and in the most favorable direction, in still air. (2) The airplane is landed on the most suitable runway considering the probable wind velocity and direction and the ground handling characteristics of that airplane, and considering other conditions such as landing aids and terrain. (c) A program manager or other person flying a turbine engine powered large transport category airplane on a program flight may permit that airplane to take off at a weight in excess of

official document · source cfr-2024 · id 14:§ 91.1037