(1) |
An applicant for the issuing of a standard category certificate of airworthiness for an aircraft, or an amendment thereof, shall provide the Director with proof that— |
(a) |
in the case of a new aircraft type manufactured by the holder of a manufacturing organisation approval issued under Part 148— |
(i) |
the applicant is the manufacturer; and |
(ii) |
the applicant has issued a statement of conformity in terms of regulation 21.02.6; or |
(b) |
in the case of an imported aircraft— |
(i) |
a standard category type acceptance certificate has been issued for the aircraft type in terms of regulation 21.04.5; and |
(ii) |
a statement of conformity has been issued by, or in accordance with the laws of, the appropriate authority of the exporting State. |
(2) |
The applicant shall, in addition to the provisions of subregulation (1), provide the Director with proof that— |
(a) |
the aircraft conforms to an appropriate type certificate or type acceptance certificate; |
(aA) |
the aircraft complies with the noise standards prescribed in Part 36; |
[Regulation 21.08.4(2)(aA) inserted by regulation 2 of Notice No. R. 1026, GG 39339, dated 30 October 2015 (Tenth Amendment of the Civil Aviation Regulations, 2015)]
(b) |
any modification to the aircraft conforms to the design changes approved for the type; |
(c) |
the aircraft complies with the appropriate airworthiness directives issued in terms of regulation 21.01.4; |
(d) |
the aircraft is issued with the appropriate flight manual, and any logbooks, repair and alteration forms and documents which the Director may require; and |
(e) |
the aircraft is in a condition for safe operation. |