Document ID: chunk:federal_register_of_legislation:F2024C01027:reg:15:p28
Version: federal_register_of_legislation:F2024C01027
Segment Type: reg
Provision Reference: reg 15 (pt 28/182)
Character Range: 209240–212112

in Parts 22, 23, 25, 26, 27, 29, 31, 32, 33 and 35, and the airworthiness standards prescribed by the Part 21 Manual of Standards, and as specified in the applicable airworthiness criteria for special classes of aircraft mentioned in subregulation 21.017(2);
 (e) for primary category aircraft, if maintenance on the aircraft is to be carried out by the pilot‑owner of the aircraft—a special inspection and preventive maintenance program designed to be accomplished by the pilot‑owner;
 (f) any other data necessary to allow, by comparison, the determination of the airworthiness of later aircraft, aircraft engines or propellers of the same type.
 (3) The type design for an aircraft type certificated under regulation 21.029A consists of the type design that was accepted by the national aviation authority of the recognised country that issued the foreign type certificate for the aircraft.
Source FARs section 21.31 modified.

21.033  Inspection and tests
 (1) CASA is not required to issue, under regulation 21.013A, a type certificate for an aircraft, aircraft engine or propeller unless the applicant allows CASA to make any inspection and any flight and ground test necessary to determine that the aircraft, aircraft engine or propeller complies with the applicable requirements of these Regulations. However:
 (a) no aircraft, aircraft engine, propeller, or part thereof may be presented to CASA for test unless compliance with paragraphs (2)(b), (c) and (d) has been shown for that aircraft, aircraft engine, propeller, or part thereof; and
 (b) no change may be made to an aircraft, aircraft engine, propeller, or part thereof between the time that compliance with paragraphs (2)(b), (c) and (d) is shown for that aircraft, aircraft engine, propeller, or part thereof and the time that it is presented to CASA for test.
 (2) Each applicant must make all inspections and tests necessary to determine:
 (a) compliance with the applicable airworthiness requirements; and
 (b) that the aircraft, aircraft engine or propeller and its materials conform to the specifications in the type design; and
 (c) that parts of the aircraft, aircraft engine or propeller conform to the drawings in the type design; and
 (d) that the manufacturing processes, construction and assembly conform to those specified in the type design.
 (3) For an aircraft with not more than 2 seats, a maximum take‑off weight not exceeding 750 kg and a 45 knots or less VS0 stall speed as defined in FARs section 23.49 that is to be type certificated in the primary category or intermediate category, an authorised person may make any determination, inspection, flight test or ground test necessary to establish whether the aircraft complies with the applicable requirements of these Regulations.
Source FARs section 21.33 modified.

21.035  Flight tests
 (1) Each applicant for a type certificate