Canadian Aviation Regulations (SOR/96-433)

Regulations are current to 2013-05-26 and last amended on 2012-07-04. Previous Versions

Eligibility Requirements

 An applicant for a repair design approval in respect of an aeronautical product shall have, or have access to, the technical capability to conduct the design analyses and tests required to demonstrate the conformity of the aeronautical product with its certification basis.

  • SOR/2009-280, s. 26.

Application for a Repair Design Approval

 An applicant for a repair design approval in respect of an aeronautical product shall submit an application to the Minister as specified in section 521.155 if the repair is in respect of

  • (a) an aeronautical product for which the Minister has issued or accepted a type certificate; or

  • (b) an aircraft registered in a foreign state, or an aeronautical product intended for installation on an aircraft registered in a foreign state, with which Canada has an airworthiness agreement or similar arrangement in respect of the acceptance of the technical data used to repair the aeronautical product.

  • SOR/2009-280, s. 26.

Certification Basis

 The Minister shall establish a certification basis, in respect of a repair design approval for an aeronautical product, consisting of the applicable standards referred to in section 521.157.

  • SOR/2009-280, s. 26.

Conformity with Certification Basis

 An applicant for a repair design approval in respect of an aeronautical product shall comply with the requirements set out in section 521.160 within the effective period referred to in section 521.156.

  • SOR/2009-280, s. 26.

Issuance of a Repair Design Approval

 Subject to section 6.71 of the Act, the Minister shall issue a repair design approval in respect of an aeronautical product if the applicant complies with the requirements set out in section 521.255.

  • SOR/2009-280, s. 26.

Change to a Repair Design Approved in a Repair Design Approval

 The holder of a repair design approval in respect of an aeronautical product who proposes to make a change to the repair design approved in the repair design approval shall comply with the requirements set out in section 521.152.

  • SOR/2009-280, s. 26.

[521.258 to 521.300 reserved]

Division VII — Part Design Approvals

Application

 This Division applies

  • (a) in respect of the issuance of a part design approval for a replacement part that is intended to be installed on an aeronautical product; and

  • (b) to applicants for and holders of a part design approval in respect of a replacement part.

  • SOR/2009-280, s. 26.

Eligibility Requirements

 An applicant for a part design approval in respect of a replacement part shall have, or have access to, the technical capability to conduct the design analyses and tests required to demonstrate the conformity of the replacement part with its certification basis.

  • SOR/2009-280, s. 26.