Canadian Aviation Regulations (SOR/96-433)

Regulations are current to 2013-04-29 and last amended on 2012-07-04. Previous Versions

Application for a Part Design Approval

  •  (1) An applicant for a part design approval in respect of a replacement part for an aeronautical product for which the Minister has issued or accepted a type certificate shall submit an application to the Minister as specified in section 521.155.

  • (2) A part design approval shall not be issued if the replacement part

    • (a) is subject to an airworthiness limitation;

    • (b) is a standard part or a commercial part;

    • (c) constitutes a change to the type design of the aeronautical product; or

    • (d) creates an airworthiness limitation.

  • SOR/2009-280, s. 26.

Certification Basis

 The Minister shall establish, in respect of a part design approval for a replacement part, a certification basis consisting of the applicable standards referred to in section 521.157.

  • SOR/2009-280, s. 26.

Conformity with Certification Basis

 An applicant for a part design approval in respect of a replacement part 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 Part Design Approval

 Subject to section 6.71 of the Act, the Minister shall issue a part design approval in respect of a replacement part if the applicant complies with the requirements set out in section 521.305.

  • SOR/2009-280, s. 26.

Change to a Part Design Approved in a Part Design Approval

 The holder of a part design approval in respect of a replacement part who proposes to make a change to the part design approved in the part design approval shall comply with

  • (a) in the case of a change to the type design, the requirements set out in Division V; and

  • (b) in any other case, the requirements set out in section 521.154.

  • SOR/2009-280, s. 26.

[521.308 to 521.350 reserved]

Division VIII — Responsibilities of a Design Approval Document Holder

Application

 This Division applies to holders of a design approval document.

  • SOR/2009-280, s. 26.

Technical Capability

 The holder of a design approval document in respect of an aeronautical product shall have, or have access to, the technical capability

  • (a) to conduct design analyses and tests in order to develop the data required to maintain the aeronautical product in an airworthy condition; and

  • (b) to carry out the responsibilities specified this Division.

  • SOR/2009-280, s. 26.

Service Difficulty Reporting

 The holder of a design approval document in respect of an aeronautical product shall report to the Minister, in accordance with Division IX, any reportable service difficulty related to the aeronautical product.

  • SOR/2009-280, s. 26.