AMC1 NCC.POL.125 Take-off — aeroplanes
The following should be considered for determining the maximum take-off mass:
(a) the pressure altitude at the aerodrome;
(b) the ambient temperature at the aerodrome;
(c) the runway surface condition and the type of runway surface;
(d) the runway slope in the direction of take-off;
(e) not more than 50 % of the reported head-wind component or not less than 150 % of the reported tailwind component; and
(f) the loss, if any, of runway length due to alignment of the aeroplane prior to take-off.
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