CAT.POL.A.305 Take-off

(a)  The take-off mass shall not exceed the maximum take-off mass specified in the AFM for the pressure altitude and the ambient temperature at the aerodrome of departure.

(b)  The unfactored take-off distance, specified in the AFM, shall not exceed:

(1)  when multiplied by a factor of 1,25, the take-off run available (TORA); or

(2)  when stop way and/or clearway is available, the following:

(i)  the TORA;

(ii)  when multiplied by a factor of 1,15, the take-off distance available (TODA); or

(iii)  when multiplied by a factor of 1,3, the ASDA.

(c)  When showing compliance with (b), the following shall be taken into account:

(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;

(4)  the runway surface condition and the type of runway surface;

(5)  the runway slope in the direction of take-off; and

(6)  not more than 50 % of the reported headwind component or not less than 150 % of the reported tailwind component.