complex motor-powered aircraft
as defined in Regulation (EC) No 216/2008 of the European Parliament and of the Council of 20…, Article 3, point (j) (Definitions)
(i) an aeroplane: — with a maximum certificated take-off mass exceeding 5 700 kg, or — certificated for a maximum passenger seating configuration of more than nineteen, or — certificated for operation with a minimum crew of at least two pilots, or — equipped with (a) turbojet engine(s) or more than one turboprop engine, or (ii) a helicopter certificated: — for a maximum take-off mass exceeding 3 175 kg, or — for a maximum passenger seating configuration of more than nine, or — for operation with a minimum crew of at least two pilots, or (iii) a tilt rotor aircraft;