Canadian Aviation Regulations
571.07 (1) No person shall install a new part on an aeronautical product unless the part meets the standards of airworthiness applicable to the installation of new parts and, subject to subsections (2) and (3), has been certified in accordance with Chapter 561 of the Airworthiness Manual.
(2) No certification referred to in subsection (1) is required where
(a) a new part is a foreign-manufactured part that is certified pursuant to an agreement with Canada, which agreement provides for the acceptance of export airworthiness certification;
(b) a new part is a foreign-manufactured part that is obtained from a manufacturer holding a type design recognized in Canada and the part is certified in accordance with the laws of the state of manufacture;
(c) a new part, whose accompanying documentation has been verified, has been inspected in accordance with the requirements of Chapter 571 of the Airworthiness Manual;
(d) a new part is installed on an aircraft that is operated under a special certificate of airworthiness in the owner-maintenance or amateur-built classification; or
(e) a part is made in accordance with subsection 571.06(4).
(3) No certification referred to in subsection (1) is required in respect of a new part that bears markings identifying it as a part specified in the type design and that
(a) is a standard part;
(b) is a commercial part;
(c) was manufactured under a Parts Manufacturer Approval issued by the Federal Aviation Administration (United States), if that part meets the installation criteria specified in Chapter 571 of the Airworthiness Manual; or
(d) is a part that was not originally designed and manufactured for aeronautical use but has been approved for use on the aeronautical product in the type design.
- SOR/2002-112, s. 7
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