History — 705.56

705.56 (1) No person shall conduct a take-off in an aircraft if the weight of the aircraft (a) exceeds the maximum take-off weight specified in the aircraft flight manual for the pressure-altitude and the ambient temperature at the aerodrome where the take-off is to be made; or (b) after allowing for planned fuel consumption during the flight to the destination aerodrome or alternate aerodrome, exceeds the 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 subsection (1) for an aeroplane, (a) the required accelerate-stop distance shall not exceed the accelerate-stop distance available (ASDA); (b) the required take-off run shall not exceed the take-off run available (TORA); and (c) the required take-off distance shall not exceed the take-off distance available (TODA). (3) For the purposes of subsection (2), the following factors shall be taken into account: (a) the pressure-altitude at the aerodrome; (b) the ambient temperature; (c) the runway slope in the direction of take-off; and (d) not more than 50 …