Transport category civil airplane weight limitations.

CFR · 2024-01-01 · US · Title 14

(a) No person may take off any transport category airplane (other than a turbine-engine-powered airplane certificated after September 30, 1958) unless— (1) The takeoff weight does not exceed the authorized maximum takeoff weight for the elevation of the airport of takeoff; (2) The elevation of the airport of takeoff is within the altitude range for which maximum takeoff weights have been determined; (3) Normal consumption of fuel and oil in flight to the airport of intended landing will leave a weight on arrival not in excess of the authorized maximum landing weight for the elevation of that airport; and (4) The elevations of the airport of intended landing and of all specified alternate airports are within the altitude range for which the maximum landing weights have been determined. (b) No person may operate a turbine-engine-powered transport category airplane certificated after September 30, 1958, contrary to the Airplane Flight Manual, or take off that airplane unless— (1) The takeoff weight does not exceed the takeoff weight specified in the (2) Normal consumption of fuel and oil in flight to the airport of intended landing and to the alternate airports will leave a weight on arrival not in excess of the landing weight specified in the Airplane Flight Manual for the elevation of each of the airports involved and for the ambient temperatures expected at the time of landing; (3) The takeoff weight does not exceed the weight shown in the Airplane Flight Manual to correspond

official document · source cfr-2024 · id 14:§ 91.605