History — 521.30

521.30 (1) The Minister shall establish, in respect of an aeronautical product, a certification basis consisting of (a) subject to subsections (2) to (5), the applicable standards of airworthiness referred to in section 521.31 that are in force on the date of application for the type certificate, unless the applicant (i) elects to include in the certification basis later amendments to those standards of airworthiness, in accordance with subsection (5), or (ii) is required to comply with later amendments to the standards of airworthiness in accordance with subsection 521.29(3); (b) the applicable aircraft emissions standards referred to in section 521.32; (c) any special conditions that are necessary to ensure that the type design of an aeronautical product having a novel or unusual design feature provides a level of safety equivalent to that provided by the standards of airworthiness in force on the date of application for the type certificate; (d) 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 type certificate; and (e) any exem…