EN
L 205/10
Official Journal of the European Union
5.8.2022
— conventional and simple design of structure, control system and ballonet system, — non-power assisted controls; (vi) a rotorcraft with an MTOM not exceeding 600 kg which is of a simple design, designed to carry not more than two occupants, not powered by turbine and/or rocket engines; restricted to VFR day operations; (k) “operational suitability data (OSD)” means data, which is part of an aircraft type certificate, restricted type certificate or supplemental type certificate, consisting of all of the following: (i)
the minimum syllabus of pilot type rating training, including determination of type rating;
(ii) the definition of scope of the aircraft validation source data to support the objective qualification of simulators or the provisional data to support their interim qualification; (iii) the minimum syllabus of maintenance certifying staff type rating training, including determination of type rating; (iv) determination of type or variant for cabin crew and type-specific data for cabin crew; (v) the master minimum equipment list.’; (3)
Article 2 is replaced by the following:
‘Article 2
Certification of products, parts and appliances 1.
Products, parts and appliances shall be issued certificates as specified in Annex I (Part 21).
2.
By way of derogation from paragraph 1 of this Article, certificates may be alternatively issued as specified in Annex Ib (Part 21 Light) for the following products: (a) an aeroplane with a maximum take-off mass (MTOM) of 2 000 kg or less and a maximum operational seating configuration of four persons; (b) a sailplane or powered sailplane of 2 000 kg MTOM or less; (c) a balloon; (d) a hot air airship; (e) a passenger gas airship designed for not more than four persons; (f) a rotorcraft of 1 200 kg MTOM or less and a maximum operational seating configuration of four persons; (g) a piston engine or fixed pitch propeller that is intended to be installed on an aircraft referred to in points (a) to (f); or (h) a gyroplane. 3.
By way of derogation from paragraphs 1 and 2 of this Article, a declaration of design compliance may alternatively be made, as specified in Annex Ib (Part 21 Light), for the following products: (a) an aeroplane of 1 200 kg MTOM or less that is not jet-powered and with a maximum operational seating configuration of two persons; (b) a sailplane or a powered sailplane of 1 200 kg MTOM or less; (c) a balloon designed for not more than four persons; (d) a hot air airship designed for not more than four persons.