(a) Standard repairs are repairs:
(1) in relation to:
(i) aeroplanes of 5 700 kg Maximum
Take-Off Mass (MTOM) or less;
(ii) rotorcraft of 3 175 kg MTOM or less;
(iii) sailplanes and powered sailplanes,
balloons and airships as defined in ELA1 or ELA2.
(2) that follow design data included in
certification specifications issued by the Agency, containing acceptable
methods, techniques and practices for carrying out and identifying standard
repairs, including the associated instructions for continued airworthiness;
and
(3) that are not in conflict with TC holders
data.
(b) Points 21.A.432A to 21.A.451 are not applicable to standard repairs.
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