Subpart 16[Repealed, SOR/2009-280, s. 26]
516.01 [Repealed, SOR/2009-280, s. 26]
516.02 [Repealed, SOR/2009-280, s. 26]
516.03 [Repealed, SOR/2009-280, s. 26]
Subpart 21 — Approval of the Type Design or a Change to the Type Design of an Aeronautical Product
Division I — General
521.01 The following definitions apply in this Subpart.
- “aeronautical product”
“aeronautical product” means an aircraft, aircraft engine, aircraft propeller or aircraft appliance or part, or a component part of any of those things. (produit aéronautique)
“applicant” means an individual or organization responsible for the design of an aeronautical product, or a representative of such an individual or organization, that makes an application for the issuance of or a change to a design approval document in respect of an aeronautical product. (demandeur)
- “design approval document”
“design approval document” means a type certificate, a supplemental type certificate, a repair design approval, a part design approval or a Canadian Technical Standard Order (CAN-TSO) design approval. (document d’approbation de la conception)
- “foreign aeronautical product”
“foreign aeronautical product” means an aeronautical product for which the state of design is a state other than Canada. (produit aéronautique étranger)
“VLA” or “very light aeroplane” means an aeroplane that has a single engine with a spark or compression ignition, has no more than two seats and is designed and manufactured to have
(a) a maximum certificated take-off weight not exceeding 750 kg; and
(b) a stall speed in the landing configuration (Vso) of 45 knots (52 mph) calibrated air speed (CAS), or less. (VLA ouavion très léger)
- SOR/2009-280, s. 26.
521.02 This Subpart applies to applicants for and holders of the following documents and applicants for a change to one of those documents:
(a) a type certificate issued under section 521.57 in respect of an aeronautical product;
(b) a Canadian Technical Standard Order (CAN-TSO) design approval issued under section 521.109 in respect of an appliance or a part;
(c) a supplemental type certificate issued under section 521.206 in respect of an aeronautical product;
(d) a repair design approval issued under section 521.256 in respect of an aeronautical product; and
(e) a part design approval issued under section 521.306 in respect of a replacement part for an aeronautical product.
- SOR/2009-280, s. 26.
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