GreatNorthCollective/greatnorth-canada-federal-laws-text huggingface dataset:
Canadian Aviation Regulations — 521.352
521.352 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
Canadian Aviation Regulations — 521.353
521.353 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
Canadian Aviation Regulations — 521.354
521.354 The holder of a design approval document in respect of an aeronautical product shall establish and maintain a service difficulty reporting system for the purpose of receiving, recording, analyzing and investigating reports and information concerning a reportable service difficulty related to the aeronautical product. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.355
521.355 (1) When the holder of a design approval document in respect of an aeronautical product receives notice that a service difficulty report has been submitted to the Transport Canada web service difficulty reporting system in relation to the aeronautical product, the holder shall (a) investigate the service difficulty and, if it results from a deficiency in the aeronautical product, develop a corrective action to rectify the deficiency; and (b) report to the Minister the progress of the investigation and any proposed corrective action. (2) Subject to section 521.356, if the Minister determines that a corrective action is required to rectify the deficiency, the holder of the design approval document in respect of the aeronautical product shall (a) submit the technical data in support of the proposed corrective action to the Minister; and (b) undertake any corrective action that the Minister determines is necessary to rectify the deficiency. SOR/2009-280, s. 26 SOR/2019-119, s. 24(F)
Canadian Aviation Regulations — 521.356
521.356 If the Minister determines that a corrective action is required to rectify an unsafe condition in an aeronautical product, the holder of the design approval document in respect of the aeronautical product shall (a) submit to the Minister for approval the corrective action required to rectify the unsafe condition; and (b) on approval of the corrective action, make available to each owner and each operator of the aeronautical product the information needed to rectify the unsafe condition. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.357
521.357 (1) Subject to subsection (2), the Minister shall approve the transfer of a design approval document in respect of an aeronautical product from the holder of the design approval document to a transferee if (a) the holder (i) notifies the Minister in writing of the intention to transfer the design approval document, (ii) provides the Minister with the legal name, address and telephone number of the transferee, (iii) provides the Minister with the number of the design approval document, the legal name of the manufacturer and the model designation of the aeronautical product that is the subject of the transfer, (iv) returns to the Minister the original design approval document signed by the holder, and (v) provides the transferee with the type design of the aeronautical product that is the subject of the transfer and the information recorded under paragraph 521.365(a); and (b) the transferee (i) applies for the issuance of an amended design approval document, (ii) complies with the requirements set out in section 521.352, and (iii) submits a signed undertaking to carry out the responsibilities specified in this Division. (2) If the transfer involves a foreign state, the holder of the design approval document and the transferee shall comply with the provisions of any airworthiness agreement or similar arrangement that exists between Canada and the foreign state involved in the transfer. SOR/2009-280, s. 26 SOR/2019-119, s. 25 SOR/2021-152, s. 8(F) SOR/2022-246, s. 11(F)
Canadian Aviation Regulations — 521.365
521.365 The holder of a design approval document in respect of an aeronautical product shall (a) establish and maintain a system for recording (i) the type design of the aeronautical product, (ii) the analyses, tests and inspections that were conducted to demonstrate the conformity of the aeronautical product with its certification basis, (iii) the certification plan and record and the declaration attesting to the demonstration of conformity of the aeronautical product with its certification basis, (iv) the data developed by the holder and required to maintain the aeronautical product in an airworthy condition, and (v) the distribution or initial sale of the aeronautical product; (b) at the request of the Minister, make available to the Minister the design approval document, the type design and any of the information recorded under paragraph (a); and (c) notify the Minister in writing if the holder no longer intends to make the information recorded under paragraph (a) available for the purpose of manufacture, modification, repair or installation of the aeronautical product or for maintaining the airworthiness of the aeronautical product. SOR/2009-280, s. 26 SOR/2019-119, s. 26
Canadian Aviation Regulations — 521.366
521.366 (1) No person shall dispose of or destroy the records containing the information recorded under paragraph 521.365(a) without the written authorization of the Minister. (2) The holder of a design approval document in respect of an aeronautical product shall notify the Minister in writing if the records containing the information recorded under paragraph 521.365(a) are lost or destroyed. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.367
521.367 (1) The holder of a design approval document in respect of an aeronautical product shall develop and maintain the manuals and their supplements that are required by the certification basis of the aeronautical product and are required to support the operation of the product in service, including (a) an installation manual; (b) an operating manual; (c) a maintenance manual; (d) an overhaul manual; (e) servicing instructions; (f) instructions for continued airworthiness; (g) an illustrated parts manual; and (h) service bulletins or equivalent documents. (2) The holder of a design approval document other than a Canadian Technical Standard Order (CAN-TSO) Design Approval in respect of an appliance or a part shall develop and maintain the manuals and their supplements that are required by the certification basis of the aeronautical product and are required to support the operation of the product in service, including (a) an aircraft flight manual; (b) a structural repair manual; (c) supplemental integrity instructions; (d) a master minimum equipment list; and (e) a maintenance review board report. (3) The holder of a design approval document in respect of an aeronautical product shall, on request, provide the Minister with up to six copies of the manuals and their supplements referred to in subsections (1) and (2), at no cost, in a format agreed to by the Minister. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.368
521.368 If the certification basis of an aeronautical product requires that instructions for continued airworthiness be developed, the holder of a design approval document in respect of the aeronautical product shall (a) provide the instructions for continued airworthiness (i) in the case of an aeronautical product other than an aircraft, to each owner of the aeronautical product on the date of its delivery, and (ii) in the case of an aircraft, to each owner of the aeronautical product on the later of the date of its delivery and the date of the issuance of its first certificate of airworthiness; (b) provide any change to the instructions for continued airworthiness (i) in the case of an aeronautical product other than an aircraft, to each of its owners, and (ii) in the case of an aircraft, to each of its operators; (c) make available to any person referred to in subsection 571.02(1) the instructions for continued airworthiness and any changes to those instructions; and (d) submit to the Minister a plan that identifies how changes to the instructions for continued airworthiness will be made available and distributed to any person referred to in paragraph (a), (b) or (c). SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.401
521.401 (1) A person who is required to report a service difficulty shall submit to the Minister, for each reportable service difficulty, a separate service difficulty report that contains the information specified in the form published by the Minister entitled Service Difficulty Report . (2) A service difficulty report shall be submitted (a) by electronic means, such as the Transport Canada web service difficulty reporting system; or (b) by mail or courier. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.402
521.402 (1) Subject to subsection (2), a person who is required to report a service difficulty shall submit a service difficulty report to the Minister within three working days after the day on which the reportable service difficulty is discovered. (2) If all of the information required under subsection 521.401(1) is not available within the period specified in subsection (1), an interim service difficulty report containing the following elements may be submitted to the Minister in a manner specified in subsection 521.401(2) within three working days after the day on which the reportable service difficulty is discovered: (a) the aircraft registration, if applicable; (b) the date of the occurrence of the reportable service difficulty; (c) a description of the reportable service difficulty; and (d) the name, mailing address, and telephone and fax numbers of the person submitting the report. (3) The person submitting the interim service difficulty report shall submit a complete service difficulty report that complies with the requirements set out in subsection 521.401(1) within 14 days after the day on which the reportable service difficulty is discovered. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.403
521.403 A service difficulty report is not required for a reportable service difficulty that has been reported by another person or organization. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.426
521.426 This Division applies in respect of aeronautical products for which a design approval document has been issued or accepted by the Minister. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.427
521.427 (1) The Minister shall issue an airworthiness directive in respect of an aeronautical product if (a) an unsafe condition exists in the aeronautical product and the condition is likely to exist or develop in other aeronautical products; (b) it is necessary to modify or cancel the requirements of an airworthiness directive issued by the foreign airworthiness authority having jurisdiction over the type design of the aeronautical product because the Minister considers the airworthiness directive inappropriate for reasons related to the environment, safety, the delayed receipt of an instruction issued by the foreign airworthiness authority or reliance on foreign legislation; or (c) it is necessary to modify or cancel a Canadian airworthiness directive that is in force, because a condition for issuance referred to in paragraph (a) or (b) has changed or ceased to exist. (2) The airworthiness directive shall (a) identify the unsafe condition; (b) identify the affected aeronautical products; (c) specify the corrective actions required; (d) specify the schedule for completion of the required corrective actions; and (e) specify its effective date. (3) This section does not apply if the unsafe condition referred to in paragraph 521.427(1)(a) is rectified by a corrective action taken under section 521.356. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.428
521.428 The Minister shall distribute an airworthiness directive to (a) the registered owner of a Canadian aircraft affected by the airworthiness directive; (b) the manufacturer of an aeronautical product and the holder of the design approval document in respect of the aeronautical product; and (c) the airworthiness authority of all known states of registry of the aircraft. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.451
521.451 This Division applies (a) in respect of the issuance of a design approval document for a foreign aeronautical product; and (b) to applicants for and holders of a design approval document in respect of a foreign aeronautical product. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.452
521.452 An applicant for a design approval document in respect of a foreign aeronautical product shall demonstrate to the Minister that the foreign airworthiness authority having jurisdiction over the type design of the foreign aeronautical product has issued or will issue a document equivalent to a design approval document in respect of that foreign aeronautical product. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.453
521.453 (1) Subject to subsection (2), an applicant for a design approval document in respect of a foreign aeronautical product shall submit an application to the Minister as specified in (a) section 521.28, in the case of a type certificate; (b) section 521.103, in the case of a Canadian Technical Standard Order (CAN-TSO) design approval; (c) section 521.203, in the case of a supplemental type certificate; (d) section 521.253, in the case of a repair design approval; and (e) section 521.303, in the case of a part design approval. (2) An applicant for a design approval document in respect of a foreign aeronautical product shall submit an application in accordance with the provisions of any airworthiness agreement or similar arrangement that exists between Canada and the state of design of the foreign aeronautical product. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.454
521.454 Paragraphs 521.44(a) and (b), section 521.47 and paragraph 521.108(a) do not apply in respect of a foreign aeronautical product. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.455
521.455 (1) Subject to subsection (2), if the foreign airworthiness authority having jurisdiction over the type design of a foreign aeronautical product has issued or will issue a document equivalent to a design approval document in respect of the foreign aeronautical product, the Minister shall issue a design approval document if the applicant (a) complies with the requirements set out in the division applicable to the design approval document that is the subject of the application; and (b) demonstrates that the foreign aeronautical product conforms to the standards of airworthiness and the aircraft emissions standards referred to in the division applicable to the design approval document that is the subject of the application and that (i) are in force on the date on which the application for the document equivalent to the design approval document was submitted to the foreign airworthiness authority having jurisdiction over the type design of the foreign aeronautical product, or (ii) are recorded by the foreign airworthiness authority in the type certificate data sheets in respect of that foreign aeronautical product. (2) If the airworthiness authority of a foreign state has entered into an airworthiness agreement or similar arrangement with Canada, the Minister shall conduct a type design examination of the foreign aeronautical product that is the subject of the application to determine if the type design of that foreign aeronautical product provides a level of safety equivalent to that specified in this Subpart. (3) If the Minister determines that the type design of the foreign aeronautical product provides a level of safety equivalent to that specified in this Subpart, the Minister shall, in accordance with the provisions of the airworthiness agreement or similar arrangement referred to in subsection (2), issue a design approval document or accept the design approval document issued by the foreign airworthiness authority in respect of the foreign aeronautical product. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.456
521.456 (1) If the holder of a design approval document issued under section 521.455 makes a change to the type design of a foreign aeronautical product that alters a condition or limitation prescribed for the foreign aeronautical product by the foreign airworthiness authority having jurisdiction over the type design of the foreign aeronautical product, the change shall be approved by that airworthiness authority and is subject to a type design examination by the Minister. (2) If the Minister determines that the change to the type design of the foreign aeronautical product provides a level of safety equivalent to that specified in this Subpart, the Minister shall, in accordance with the provisions of the airworthiness agreement or similar arrangement referred to in subsection 521.455(2), issue an amended design approval document or accept the design approval document issued by the foreign airworthiness authority in respect of the change to the type design of the foreign aeronautical product. SOR/2009-280, s. 26
Canadian Aviation Regulations — 549.01
549.01 A person who intends to construct an aircraft and obtain, under paragraph 507.03(b), a special certificate of airworthiness in the amateur-built category in respect of the aircraft must (a) before starting construction, (i) inform the Minister of the intention to construct the aircraft, (ii) show that the aircraft design meets the standards specified in Chapter 549 of the Airworthiness Manual , and (iii) show that the major portion of the aircraft will be constructed from raw material and assembled on a non-commercial, non-production basis for educational or recreational purposes; and (b) during construction and again before the first flight, make the aircraft available to the Minister for inspection. SOR/98-526, s. 3
Canadian Aviation Regulations — 561.01
561.01 In this Subpart, design approval means a type certificate, a supplemental type certificate, a part design approval, a Canadian Technical Standard Order (CAN-TSO) design approval or a document equivalent to any of those documents that is issued by the airworthiness authority of a foreign state; ( approbation de conception ) manual means the manual established under section 561.07; ( manuel ) Standard 561 means Standard 561 — Standard for Approved Manufacturers . ( norme 561 ) SOR/2005-348, s. 4; SOR/2009-280, s. 28
Canadian Aviation Regulations — Canadian Aviation Regulations
design approval means a type certificate, a supplemental type certificate, a part design approval, a Canadian Technical Standard Order (CAN-TSO) design approval or a document equivalent to any of those documents that is issued by the airworthiness authority of a foreign state; ( approbation de conception )
Canadian Aviation Regulations — Canadian Aviation Regulations
manual means the manual established under section 561.07; ( manuel )
Canadian Aviation Regulations — Canadian Aviation Regulations
Standard 561 means Standard 561 — Standard for Approved Manufacturers . ( norme 561 )
Canadian Aviation Regulations — 561.02
561.02 This Subpart applies in respect of the manufacture of an aeronautical product in respect of which a design approval has been issued but does not apply in respect of (a) maintenance; (b) the manufacture of standard parts; (c) the manufacture of commercial parts; or (d) the manufacture of parts during a repair or modification under subsection 571.06(4). SOR/2005-348, s. 4
Canadian Aviation Regulations — 561.03
561.03 (1) An applicant for the issuance or amendment of a manufacturer certificate respecting an aeronautical product shall submit an application to the Minister that includes the documents specified in section 561.03 of Standard 561. (2) An applicant for the issuance or amendment of a manufacturer certificate respecting an aeronautical product shall (a) be the holder of, or applicant for, a design approval for that aeronautical product; or (b) have written authorization from the holder of a design approval to manufacture that aeronautical product. (3) An applicant for the issuance or amendment of a manufacturer certificate respecting an aeronautical product shall demonstrate that they have access to all present and future design data, process specifications and other related information necessary for the continuing airworthiness of the aeronautical product. (4) The Minister shall issue or amend a manufacturer certificate authorizing an applicant to manufacture the aeronautical products set out in the manufacturer certificate if the applicant meets the requirements of this Subpart. (5) A manufacturer certificate may authorize the manufacture of a limited number of an aeronautical product where (a) an applicant has made an application for a design approval for that aeronautical product but it has not yet been issued; or (b) an applicant is about to enter into a license agreement with the holder of the design approval for that aeronautical product. (6) Unless an expiry date is specified in the manufacturer certificate issued under subsection (4), the certificate shall remain in effect until it is surrendered by the manufacturer or suspended or cancelled. (7) A manufacturer certificate is not transferable. (8) Except as provided in section 561.06, the final assembly facilities for an aeronautical product specified in a manufacturer certificate shall be located in Canada. SOR/2005-348, s. 4
Canadian Aviation Regulations — 561.04
561.04 (1) The holder of a manufacturer certificate shall (a) appoint a person to be responsible for all the activities performed under this Subpart and specified in the manual; and (b) ensure that the person appointed has acquired experience in the areas of responsibility set out in subsection 561.04(1) of Standard 561. (c) [Repealed, SOR/2022-246, s. 12] (2) [Repealed, SOR/2022-246, s. 12] (3) [Repealed, SOR/2022-246, s. 12] (4) [Repealed, SOR/2022-246, s. 12] (5) The holder of a manufacturer certificate shall provide the person appointed with the authority and the financial and human resources necessary to ensure that the requirements of this Subpart are met. (6) The person appointed may assign responsibility for the management of specific activities, systems or programs required by this Subpart to other persons, provided that the assignments and the scope of the assigned responsibilities are specified in the manual. (7) The holder of a manufacturer certificate shall ensure that no person is appointed under paragraph (1)(a) or remains responsible for the activities referred to in that paragraph if, at the time of their appointment or during their tenure, they have a record of conviction for (a) an offence under section 7.3 of the Act; or (b) two or more offences in respect of section 561.10 of these Regulations, not arising from a single occurrence. SOR/2005-348, s. 4 SOR/2019-119, s. 27(F) SOR/2022-246, s. 12
Canadian Aviation Regulations — 561.05
561.05 The holder of a manufacturer certificate shall have, and ensure that any supplier referred to in section 561.13 has, the financial and human resources necessary for the manufacture and inspection of any aeronautical product specified in the manufacturer certificate, including those specified in section 561.05 of Standard 561. SOR/2005-348, s. 4