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Canadian Aviation Regulations (SOR/96-433)

Regulations are current to 2021-06-28 and last amended on 2021-06-06. Previous Versions

Part V — Airworthiness (continued)

Subpart 7 — Flight Authority and Certificate of Noise Compliance (continued)

[
  • SOR/2000-404, s. 1
]

Suspension of a Certificate of Noise Compliance

 A certificate of noise compliance is suspended and shall be surrendered to the Minister on request if the aircraft in respect of which it was issued no longer meets the noise emission levels referred to in section 507.20.

  • SOR/2000-404, s. 2

Validation of a Foreign Certificate of Noise Compliance

 In the process of validating a foreign flight authority in respect of an aircraft under section 507.05, if a foreign certificate of noise compliance is in effect in respect of the aircraft, the Minister shall validate the foreign certificate of noise compliance in the form and manner specified for the validation of the flight authority.

  • SOR/2000-404, s. 2

Subpart 9 — Export Airworthiness Certificates

Application

 This Subpart applies in respect of the following aircraft if they meet the export requirements specified in Chapter 509 of the Airworthiness Manual, except for aircraft that are operated under a special certificate of airworthiness in the owner-maintenance or amateur-built classification, remotely piloted aircraft having a maximum take-off weight of 25 kg (55 pounds) or less, ultra-light aeroplanes and hang gliders:

  • (a) new aircraft manufactured in Canada;

  • (b) Canadian aircraft in respect of which a Certificate of Airworthiness has been issued pursuant to Subpart 7; or

  • (c) aircraft that were last registered in Canada but are no longer registered in any state.

Application for an Export Airworthiness Certificate

  •  (1) A person who applies for an Export Airworthiness Certificate shall do so in the form and manner specified in Chapter 509 of the Airworthiness Manual.

  • (2) An applicant for an Export Airworthiness Certificate shall include with the application a declaration made by a person authorized to do so pursuant to section 509.04, attesting that the aircraft conforms to the certified type design specified in the application.

Authority for Export

  •  (1) Subject to subsection (2), the Minister shall issue an Export Airworthiness Certificate where the aircraft in respect of which the application is made conforms to

    • (a) the type design specified in a type certificate; or

    • (b) another type design specified in the application, where the aircraft is being exported to a state with which Canada has entered into an agreement that provides for the acceptance of Export Airworthiness Certificates and the aircraft conforms to any special requirements specified by that state.

  • (2) Where an aircraft does not meet the requirements of subsection (1), the Minister may issue an Export Airworthiness Certificate that specifies the non-conformity to the applicable type design or any special requirement and the acceptance of that non-conformity by the state to which the aircraft is being exported.

  • SOR/2009-280, s. 25

Persons Who May Attest to Condition and Conformity

 No person shall make a declaration of an aircraft’s condition or conformity to its certified type design for the purpose of obtaining an Export Airworthiness Certificate in respect of the aircraft, other than

  • (a) the holder of an aircraft maintenance engineer (AME) licence issued pursuant to Part IV that is applicable to that aircraft type; or

  • (b) in the case of a new aircraft manufactured in Canada, an authorized representative of the manufacturer.

Responsibilities of the Exporter

 Where an Export Airworthiness Certificate has been issued in respect of an aircraft, the owner of the aircraft shall, on transfer of its title,

  • (a) forward to the new owner all of the documents and information required by Chapter 509 of the Airworthiness Manual;

  • (b) where the exported aircraft is disassembled, forward to the new owner the manufacturer’s assembly instructions and the other documents relating to the aircraft specified in Chapter 509 of the Airworthiness Manual; and

  • (c) ensure that the temporary equipment, if any, incorporated into the aircraft for the purpose of the export delivery flight is removed and the aircraft is restored to the configuration approved in the type certificate.

SUBPART 11[Repealed, SOR/2009-280, s. 26]

 [Repealed, SOR/2009-280, s. 26]

 [Repealed, SOR/2009-280, s. 26]

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SUBPART 13[Repealed, SOR/2009-280, s. 26]

 [Repealed, SOR/2009-280, s. 26]

 [Repealed, SOR/2009-280, s. 26]

 [Repealed, SOR/2009-280, s. 26]

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 [Repealed, SOR/2009-280, s. 26]

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 [Repealed, SOR/2009-280, s. 26]

 [Repealed, SOR/2009-280, s. 26]

 [Repealed, SOR/2009-280, s. 26]

 [Repealed, SOR/2009-280, s. 26]

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 [Repealed, SOR/2009-280, s. 26]

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SUBPART 16[Repealed, SOR/2009-280, s. 26]

 [Repealed, SOR/2009-280, s. 26]

 [Repealed, SOR/2009-280, s. 26]

 [Repealed, SOR/2009-280, s. 26]

 
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