GreatNorthCollective/greatnorth-canada-federal-laws-text huggingface dataset:
Canadian Aviation Regulations — 521.104
521.104 (1) Unless an applicant demonstrates, at the time of submitting an application for a Canadian Technical Standard Order (CAN-TSO) design approval in respect of an appliance or a part, that a longer period is required for the design, development and testing of the appliance or part, and for that reason the Minister approves a longer period, the application is effective during one of the following periods, beginning on the date of the application: (a) two years, in the case of an appliance or a part other than a turbine-powered APU; or (b) three years, in the case of a turbine-powered APU. (2) If a Canadian Technical Standard Order (CAN-TSO) design approval is not issued within the applicable effective period referred to in subsection (1), the applicant may (a) submit a new application for a Canadian Technical Standard Order (CAN-TSO) design approval; or (b) apply for an extension of the effective period of the original application. (3) If the effective period of an application for a Canadian Technical Standard Order (CAN-TSO) design approval is extended under paragraph (2)(b), the standards of airworthiness applicable to the appliance or part are those in force on the date that precedes, by one of the periods referred to in subsection (1), the date of the issuance of the Canadian Technical Standard Order (CAN-TSO) design approval. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.105
521.105 The Minister shall establish, in respect of an appliance or a part, a certification basis consisting of (a) the applicable standards of airworthiness referred to in section 521.106 that are in force on the date of application for the Canadian Technical Standard Order (CAN-TSO) design approval; and (b) any finding of equivalent safety based on any factors or design features that provide for an alternate means of compliance with the standards of airworthiness in force on the date of application for the Canadian Technical Standard Order (CAN-TSO). SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.106
521.106 The standards of airworthiness for the issuance of or a change to a Canadian Technical Standard Order (CAN-TSO) design approval in respect of an appliance or a part are (a) those specified in Chapter 537 — Appliances and Parts of the Airworthiness Manual ; or (b) if no standards of airworthiness for the issuance of or a change to a Canadian Technical Standard Order (CAN-TSO) design approval in respect of the appliance or part are specified in Chapter 537 — Appliances and Parts of the Airworthiness Manual , the minimum performance standards specified by the Minister. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.107
521.107 An applicant for a Canadian Technical Standard Order (CAN-TSO) design approval in respect of an appliance or a part shall (a) demonstrate to the Minister that the appliance or part conforms to the certification basis established by the Minister under section 521.105; (b) submit to the Minister a declaration of design and performance that contains (i) the content of the certification basis, (ii) a declaration attesting to the demonstration of conformity of the appliance or part with its certification basis, (iii) information identifying the components of the type design of the appliance or part, (iv) the rated performance of the appliance or part, (v) a reference to the record documenting the means of demonstrating conformity with the certification basis, and (vi) a reference to the maintenance, overhaul and repair manuals; (c) make available to the Minister the means by which conformity is established; and (d) submit to the Minister for approval any manuals, instructions and limitations that are required by the certification basis established in respect of the appliance or part. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.108
521.108 An applicant for a Canadian Technical Standard Order (CAN-TSO) design approval in respect of an appliance or a part shall (a) ensure, before conducting a test, that the item to be tested conforms to the drawings, specifications and manufacturing processes proposed for the type design of the appliance or part and that the measuring device and test equipment to be used are appropriate and calibrated for the test; (b) conduct all the inspections, analyses and tests necessary to demonstrate to the Minister that the type design of the appliance or part conforms to its certification basis; (c) in accordance with the certification plan, submit to the Minister for review the data and reports resulting from the inspections, analyses and tests conducted under paragraph (b); and (d) provide the Minister with access to the appliance or part for the purpose of making any inspection, making any engineering assessment, or conducting or witnessing any test, (i) required to verify the applicant’s declaration attesting to the demonstration of conformity of the appliance or part with its certification basis, or (ii) required to make a determination of the conformity of the appliance or part with its certification basis. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.109
521.109 Subject to section 6.71 of the Act, the Minister shall issue a Canadian Technical Standard Order (CAN-TSO) design approval in respect of an appliance or a part if the applicant (a) meets the requirements set out in section 521.107; and (b) submits a signed undertaking to carry out the responsibilities specified in Division VIII. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.110
521.110 (1) The holder of a Canadian Technical Standard Order (CAN-TSO) design approval in respect of an appliance or a part who proposes to make a change to the appliance or part shall (a) in the case of a change to the type design, apply for a new Canadian Technical Standard Order (CAN-TSO) design approval under section 521.103; and (b) in any other case, establish procedures to ensure that the changed appliance or part continues to conform to its certification basis and make the change after the Minister accepts the procedures. (2) An individual or organization, other than the holder of a Canadian Technical Standard Order (CAN-TSO) design approval in respect of an appliance or a part, who proposes to make a change or repair to the appliance or part shall make an application in respect of that appliance or part for the issuance of a Canadian Technical Standard Order (CAN-TSO) design approval, a supplemental type certificate, or a repair design approval. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.151
521.151 This Division applies (a) in respect of the approval of a change to the type design of an aeronautical product; and (b) to applicants for an approval of a change to the type design of an aeronautical product. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.152
521.152 (1) Subject to section 521.153, no person shall undertake a change to the type design of an aeronautical product that has other than a negligible effect on the weight and centre-of-gravity limits, structural strength, performance, power plant operation, flight characteristics or other qualities affecting its airworthiness or environmental characteristics except in accordance with sections 521.155 to 521.160. (2) In any other case, no person shall undertake a change to the type design of an aeronautical product except in accordance with section 521.154. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.153
521.153 An applicant for the approval of a change to the type design of an aeronautical product shall submit an application for a new type certificate under section 521.28 if the Minister determines that the change is so extensive in relation to the design, configuration, power or weight of the product — including, in the case of an engine, its power limitations — that a substantially complete investigation by the applicant is necessary to determine conformity with the applicable certification basis. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.154
521.154 The holder of a design approval document who proposes to make a change to an aeronautical product, other than a change to the type design referred to in subsection 521.152(1), shall establish procedures to ensure that the changed aeronautical product continues to conform to its certification basis and make the change after the Minister accepts the procedures. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.155
521.155 An applicant for the approval of a change to the type design of an aeronautical product shall submit to the Minister (a) an application that contains the information specified on the form published by the Minister entitled Design Change Approval Application ; (b) a description of the change to the type design that identifies (i) all parts of the type design, including all parts of the approved manuals, that are affected by the change, and (ii) any re-investigations necessary to demonstrate the continued conformity of the aeronautical product with the applicable certification basis, by listing the standards of airworthiness that must be met and the means to be used to demonstrate conformity; (c) a proposed certification basis; and (d) a certification plan that identifies (i) the means to be used to demonstrate that the change to the type design of the aeronautical product conforms to the applicable certification basis, (ii) the documentation that demonstrates that the change to the type design of the aeronautical product conforms to the applicable certification basis, and (iii) the resources necessary for carrying out the demonstration of conformity referred to in subparagraph (i), and (iv) the schedule for carrying out the demonstration of conformity referred to in subparagraph (i). SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.156
521.156 (1) Unless an applicant demonstrates, at the time of submitting an application for the approval of a change to the type design of an aeronautical product, that a longer period is required for the design, development and testing of the product, and for that reason the Minister approves a longer period, the application is effective during one of the following periods, beginning on the date of the application: (a) five years, in the case of a transport category aeroplane or a transport category rotorcraft; or (b) three years, in the case of (i) an aircraft other than an aircraft referred to in paragraph (a), (ii) an aircraft engine, or (iii) an aircraft propeller. (2) If a change to the type design of an aeronautical product is not approved within the applicable effective period referred to in subsection (1), the applicant may (a) submit a new application for the approval of a change to the type design of the aeronautical product; or (b) apply for an extension of the effective period of the original application. (3) If the effective period of an application for the approval of a change to the type design of an aeronautical product is extended under paragraph (2)(b), the standards of airworthiness applicable to the change are those in force on the date that precedes, by one of the periods referred to in subsection (1), the date of the approval of the change to the type design. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.157
521.157 The Minister shall establish, in respect of a change to the type design of an aeronautical product, a certification basis consisting of the applicable standards referred to in sections 521.158 and 521.159. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.158
 to the type design of an aircraft results in the aircraft being reclassified as a restricted category aircraft, that aircraft must meet (a) the standards of airworthiness referred to in section 521.31 applicable to that category of aircraft that are in force on the date of the application for the change; or (b) the standards of airworthiness recorded in the type certificate data sheets, or an earlier amendment to a standard referred to in paragraph (a), if the standards or the amendment provide a level of safety appropriate for the intended use of that aircraft. (9) An applicant for the approval of a change to the type design of an aeronautical product may elect to include in the certification basis a later amendment to the standards of airworthiness specified in subsection (1), on the condition that the applicant comply with any other amendment that is directly related to those standards. SOR/2009-280, s. 26 SOR/2019-119, s. 20(F)
Canadian Aviation Regulations — 521.159
521.159 (1) Subject to subsection (2), an applicant for the approval of a change to the type design of an aeronautical product that results in a change in the noise levels of an aircraft shall demonstrate (a) that the aircraft meets the noise standards specified in Subchapter A of Chapter 516 — Aircraft Emissions of the Airworthiness Manual ; or (b) that the aircraft continues to meet the noise standards that applied before the change was undertaken and that are recorded in the type certificate data sheets or in a document that has been accepted by the Minister as being equivalent to a type certificate for that aircraft. (2) Subsection (1) does not apply in respect of (a) a restricted category aircraft for use in agricultural operations or fire prevention and suppression; (b) the installation or removal of floats or skis; (c) the installation or removal of external equipment on a rotorcraft; or (d) an aircraft whose certification basis does not contain noise standards, if the change to the type design does not involve (i) a change in the number or type of propellers, (ii) a change in the number of engines or in the principle of propulsion of the engines, or (iii) in the case of a rotorcraft, a change in the number of rotors or in the principle of operation of the rotors. (3) An applicant for the approval of a change to the type design of a turbine-powered aircraft shall demonstrate that the aircraft meets the standards respecting the prevention of intentional fuel venting specified in Subchapter B of Chapter 516 — Aircraft Emissions of the Airworthiness Manual . (4) An applicant for the approval of a change to the type design of an aircraft engine shall demonstrate that the aircraft engine meets the smoke and gaseous aircraft emissions standards specified in Subchapter B of Chapter 516 — Aircraft Emissions of the Airworthiness Manual . (5) An applicant for the approval of a change to the type design of an aircraft shall demonstrate that the aircraft meets the carbon dioxide (CO 2 ) emissions standards specified in Subchapter C of Chapter 516 — Aircraft Emissions of the Airworthiness Manual . SOR/2009-280, s. 26 SOR/2019-119, s. 21(F) SOR/2020-251, s. 2
Canadian Aviation Regulations — 521.160
521.160 (1) An applicant for the approval of a change to the type design of an aeronautical product shall (a) demonstrate to the Minister that the product conforms to the certification basis established by the Minister under section 521.157 by conducting the inspections and tests referred to in section 521.44; (b) submit to the Minister a declaration attesting to the demonstration of conformity of the product with its certification basis; (c) make available to the Minister the means by which conformity is established; (d) in the case of an aircraft, record the noise levels in its flight manual or in a supplement to that manual using the Guidelines for the Administration of Noise Certification Documentation set out in Attachment G of Annex 16, Volume I to the Convention; (e) submit a signed undertaking to carry out the responsibilities specified in Division VIII; and (f) submit to the Minister for approval any manual, instructions and limitations that are required by the certification basis established in respect of the product. (2) An applicant for the approval of a change to the type design of an aeronautical product other than a restricted category aircraft shall demonstrate to the Minister that (a) in the case of an aircraft, no feature or characteristic makes the aircraft unsafe, taking into account the category in which certification is requested; and (b) the type design of the product provides a level of safety at least equivalent to that provided by the certification basis that applied before the change was undertaken. (3) An applicant for the approval of a change to the type design of a restricted category aircraft shall demonstrate to the Minister that (a) no feature or characteristic makes the aircraft unsafe when that aircraft is operated within the limitations specified for its intended use; and (b) the aircraft has a type design that conforms to its certification basis. SOR/2009-280, s. 26 SOR/2019-119, s. 22(F)
Canadian Aviation Regulations — 521.161
521.161 Subject to section 6.71 of the Act, the Minister shall approve a change to the type design of an aeronautical product if the applicant meets the requirements set out in section 521.160. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.201
521.201 This Division applies (a) in respect of the issuance of a supplemental type certificate as a result of a change to the type design of an aeronautical product; and (b) to applicants for and holders of a supplemental type certificate in respect of an aeronautical product. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.202
521.202 An applicant for a supplemental type certificate in respect of a change to the type design of an aeronautical product shall have, or have access to, the technical capability to conduct the design analyses and tests required to demonstrate the conformity of the aeronautical product with its certification basis. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.203
521.203 Subject to section 521.153, an applicant for a supplemental type certificate in respect of a change to the type design of an aeronautical product for which the Minister has issued or accepted a type certificate shall submit an application to the Minister as specified in section 521.155. SOR/2009-280, s. 26 SOR/2019-119, s. 23(F)
Canadian Aviation Regulations — 521.204
521.204 The Minister shall establish, in respect of a change to the type design of an aeronautical product, a certification basis consisting of the applicable standards referred to in section 521.157. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.205
521.205 An applicant for a supplemental type certificate in respect of a change to the type design of an aeronautical product shall comply with the requirements set out in section 521.160 within the effective period referred to in section 521.156. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.206
521.206 Subject to section 6.71 of the Act, the Minister shall issue a supplemental type certificate in respect of a change to the type design of an aeronautical product if the applicant complies with the requirements set out in section 521.205. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.207
521.207 The holder of a supplemental type certificate in respect of an aeronautical product who proposes to make a change to the type design approved in the supplemental type certificate shall comply with the requirements set out in section 521.152. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.251
521.251 This Division applies (a) in respect of the issuance of a repair design approval as a result of a repair to an aeronautical product; and (b) to applicants for and holders of a repair design approval in respect of an aeronautical product. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.252
521.252 An applicant for a repair design approval in respect of an aeronautical product shall have, or have access to, the technical capability to conduct the design analyses and tests required to demonstrate the conformity of the aeronautical product with its certification basis. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.253
521.253 An applicant for a repair design approval in respect of an aeronautical product shall submit an application to the Minister as specified in section 521.155 if the repair is in respect of (a) an aeronautical product for which the Minister has issued or accepted a type certificate; or (b) an aircraft registered in a foreign state, or an aeronautical product intended for installation on an aircraft registered in a foreign state, with which Canada has an airworthiness agreement or similar arrangement in respect of the acceptance of the technical data used to repair the aeronautical product. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.254
521.254 The Minister shall establish a certification basis, in respect of a repair design approval for an aeronautical product, consisting of the applicable standards referred to in section 521.157. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.255
521.255 An applicant for a repair design approval in respect of an aeronautical product shall comply with the requirements set out in section 521.160 within the effective period referred to in section 521.156. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.256
521.256 Subject to section 6.71 of the Act, the Minister shall issue a repair design approval in respect of an aeronautical product if the applicant complies with the requirements set out in section 521.255. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.257
521.257 The holder of a repair design approval in respect of an aeronautical product who proposes to make a change to the repair design approved in the repair design approval shall comply with the requirements set out in section 521.152. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.301
521.301 This Division applies (a) in respect of the issuance of a part design approval for a replacement part that is intended to be installed on an aeronautical product; and (b) to applicants for and holders of a part design approval in respect of a replacement part. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.302
521.302 An applicant for a part design approval in respect of a replacement part shall have, or have access to, the technical capability to conduct the design analyses and tests required to demonstrate the conformity of the replacement part with its certification basis. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.303
521.303 (1) An applicant for a part design approval in respect of a replacement part for an aeronautical product for which the Minister has issued or accepted a type certificate shall submit an application to the Minister as specified in section 521.155. (2) A part design approval shall not be issued if the replacement part (a) is subject to an airworthiness limitation; (b) is a standard part or a commercial part; (c) constitutes a change to the type design of the aeronautical product; or (d) creates an airworthiness limitation. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.304
521.304 The Minister shall establish, in respect of a part design approval for a replacement part, a certification basis consisting of the applicable standards referred to in section 521.157. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.305
521.305 An applicant for a part design approval in respect of a replacement part shall comply with the requirements set out in section 521.160 within the effective period referred to in section 521.156. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.306
521.306 Subject to section 6.71 of the Act, the Minister shall issue a part design approval in respect of a replacement part if the applicant complies with the requirements set out in section 521.305. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.307
521.307 The holder of a part design approval in respect of a replacement part who proposes to make a change to the part design approved in the part design approval shall comply with (a) in the case of a change to the type design, the requirements set out in Division V; and (b) in any other case, the requirements set out in section 521.154. SOR/2009-280, s. 26
Canadian Aviation Regulations — 521.351
521.351 This Division applies to holders of a design approval document. SOR/2009-280, s. 26