Paragraphs (c) through (h) of Standard 571.07 Installation of New Parts read as follows:
"(c) Parts made to an FAA Parts Manufacturer Approval (hereinafter simply known as PMA) can be installed on aeronautical products for which the US has jurisdiction for the initial type design.
(d) Except as provided in (e), (f), (g) and (h), PMA parts can be installed on other aeronautical products only where specified in the type design, in the manufacturer's parts catalogue, or where approved by the Civil Aviation Authority of the country having jurisdiction over the initial type design.
(e) An aircraft that is not of US type design and that was operated with PMA parts installed while the aircraft was under the jurisdiction of another State, can be accepted as a Canadian aircraft provided the PMA parts were installed in compliance with the regulations of the other State.
(f) An aeronautical product, other than a complete aircraft, that is not of US type design but was operated with PMA parts installed while under the jurisdiction of another State, can remain in service on a Canadian aircraft provided the PMA parts were installed in compliance with the regulations of the other State.
(g) A PMA part accepted pursuant to (e) or (f) can remain in service until such time as its replacement is required by reason of deterioration of time in service. Such a part shall not, however, be replaced by another FAA PMA part.
(h) PMA parts are replacement parts and are acceptable on Canadian aircraft for which TC has jurisdiction over the initial design, if such parts are listed in the manufacturer's parts catalogue, or otherwise approved by the Minister.
Information Note:
Installation of an FAA PMA part not meeting these criteria constitutes a modification requiring compliance with Section 571.06 of the CARs."
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