OpenLegislation

Division (6) In Annex VI to Regulation (EU) No 965/2012, point (b) of NCC.POL.125 is replaced by the following:

United Kingdom

Original text. Later amendments are not shown.

  1. (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:

    1. (1)

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

    2. (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.’.