Document ID: chunk:federal_register_of_legislation:F2024C01027:reg:15:p98
Version: federal_register_of_legislation:F2024C01027
Segment Type: reg
Provision Reference: reg 15 (pt 98/182)
Character Range: 396826–399616

part is to be installed, unless the applicant shows that the design of the part is identical to the design of a part that is covered under a type certificate. If the design of the part was obtained by a licensing agreement, evidence of that agreement must be furnished;
 (e) subject to subregulation (3A), a copy of the system that the applicant proposes to use, if granted an APMA, to comply with the requirements of subregulation 21.303(11).
 (3A) An applicant is not required to include a copy of the system referred to in paragraph 21.303(3)(e) if the applicant has previously given CASA a copy of the same version of the system.
 (4) An applicant is entitled to an APMA for a replacement or modification part if CASA is satisfied that:
 (a) the design meets the airworthiness requirements of these Regulations that are applicable to the aircraft, aircraft engine or propeller on which the part is to be installed; and
 (b) the applicant would, if the APMA were to be granted, be able to comply with the requirements of subregulation (11).
 (4A) For paragraph (4)(a), CASA may satisfy itself that the design meets the applicable airworthiness requirements on the basis of any of the following:
 (a) an examination of the design;
 (b) the technical data for the design approved under regulation 21.009;
 (c) a certificate from an approved design organisation under subregulation (4C).
 (4B) Subregulation (4C) applies if, under regulation 21.251, CASA authorises a relevant approved design organisation to determine whether the design meets the airworthiness requirements of these Regulations that are applicable to the aircraft, aircraft engine or propeller on which the part is to be installed.
 (4C) If the approved design organisation is satisfied that the design meets the airworthiness requirements of these Regulations that are applicable to the aircraft, aircraft engine or propeller, the organisation may give CASA a certificate to that effect.

 (5) An applicant for an APMA must allow CASA or a relevant approved design organisation to make any inspection or test necessary to determine compliance with the applicable regulations.
 (6) CASA is not required to consider an application unless the applicant has complied with paragraphs (8)(b), (c) and (d).
 (7) The applicant must ensure that no change is made to a part between the time compliance with paragraphs (8)(b), (c) and (d) is shown for that part and the time the part is presented to CASA or a relevant approved design organisation for inspection or test.
 (8) An applicant for an APMA must make all inspections and tests necessary to determine the following:
 (a) compliance with the applicable airworthiness requirements;
 (b) that materials conform to the specifications in the design;
 (c) that the part conforms