[F1ANNEX VI U.K. NON-COMMERCIAL AIR OPERATIONS WITH COMPLEX MOTOR-POWERED AIRCRAFT [PART-NCC]

SUBPART C AIRCRAFT PERFORMANCE AND OPERATING LIMITATIONS U.K.

NCC.POL.125 Take-off — aeroplanes U.K.

(a) When determining the maximum take-off mass, the pilot-in-command shall take the following into account: U.K.
(1)

the calculated take-off distance shall not exceed the take-off distance available with a clearway distance not exceeding half of the take-off run available;

(2)

the calculated take-off run shall not exceed the take-off run available;

(3)

a single value of V 1 shall be used for the rejected and continued take-off, where a V 1 is specified in the AFM; and

(4)

on a wet or contaminated runway, the take-off mass shall not exceed that permitted for a take-off on a dry runway under the same conditions.

[F2(b) Except for an aeroplane equipped with turboprop engines and a maximum take-off mass at or below 5 700 kg, in the event of an engine failure during take-off, the pilot-in-command shall ensure that the aeroplane is able: U.K.
(1)

to discontinue the take-off and stop within the accelerate-stop distance available or the runway available; or

(2)

to continue the take-off and clear all obstacles along the flight path by an adequate margin until the aeroplane is in a position to comply with NCC.POL.130.]]