Navigate / EASA

21.A.35 Flight Tests

Regulation (EU) No 748/2012

(a)     Flight testing for the purpose of obtaining a type-certificate shall be conducted in accordance with conditions for such flight testing specified by the Agency.

(b)     The applicant shall make all flight tests that the Agency finds necessary:

1.       to determine compliance with the applicable type-certification basis and environmental protection requirements; and

2.       to determine whether there is reasonable assurance that the aircraft, its parts and appliances are reliable and function properly for aircraft to be certificated under this Annex I (Part 21), except for,

(i)      sailplanes and powered sailplanes,

(ii)     balloons and airships defined in ELA1 or ELA2,

(iii)     aeroplanes of 2 722 kg or less maximum take-off mass (MTOM).

(c)      (Reserved)

(d)     (Reserved)

(e)     (Reserved)

(f)      The flight tests prescribed in point (b)(2) shall include:

1.       for aircraft incorporating turbine engines of a type not previously used in a type-certificated aircraft, at least 300 hours of operation with a full complement of engines that conform to a type-certificate; and

2.       for all other aircraft, at least 150 hours of operation.