History — 704.46

704.46 (1) Subject to section 704.51, no air operator shall authorize a flight — and no person shall conduct a take-off — in an aeroplane unless the following conditions are met: (a) the weight of the aeroplane does not exceed the maximum take-off weight specified in the aircraft flight manual for the pressure-altitude and the ambient temperature at the departure aerodrome; and (b) after allowing for planned fuel consumption during the flight to the destination aerodrome or alternate aerodrome, the weight of the aeroplane does not exceed the maximum landing weight specified in the aircraft flight manual for the pressure-altitude and the ambient temperature at the destination aerodrome or alternate aerodrome. (2) In the determination of the maximum take-off weight referred to in paragraph (1)(a) for a propeller-driven aeroplane having an MCTOW of not more than 5 700 kg (12,566 pounds), (a) the required accelerate-stop distance specified in the aircraft flight manual shall not exceed the accelerate-stop distance available (ASDA) unless (i) the maximum take-off weight is not limited by the accelerate-stop distance requirements set out in the aircraft flight manual, and (ii) the aeropl…