Division (d) When showing compliance with (a) to (c), the following shall be taken into account:
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- (1)
the mass of the aeroplane at the commencement of the take-off run;
- (2)
the pressure altitude at the aerodrome;
- (3)
the ambient temperature at the aerodrome; and
- (4)
not more than 50 % of the reported headwind component or not less than 150 % of the reported tailwind component.