Certification Basis Clause Samples
Certification Basis. 4.4.3.1. For the purpose of issuing a type certificate, the Validating Authority shall refer to the airworthiness standards for a similar product of its own that were in effect on the effective certification application date established by the Certificating Authority, complemented when applicable by additional technical conditions, as defined in the Technical Implementation Procedures.
4.4.3.2. The environmental protection requirements used during the validation process of a type certificate shall be the applicable requirements in effect in the Party of the Validating Authority on the date of application for validation to the Validating Authority.
4.4.3.3. The Validating Authority shall specify, when applicable, any:
(a) exemption to the applicable standards;
(b) deviation from the applicable standards;
(c) compensating factors that provide an equivalent level of safety when applicable standards are not complied with.
4.4.3.4. The Validating Authority shall specify any special condition applied or intended to be applied if the related airworthiness code does not contain adequate or appropriate safety standards for the product, because:
(a) the product has novel or unusual design features relative to the design practices on which the applicable airworthiness code is based;
(b) the intended use of the product is unconventional; or
(c) experience from other similar products in service or products having similar design features, has shown that unsafe conditions may develop.
4.4.3.5. When specifying exemptions, deviations, compensating factors or special conditions, the Validating Authority shall give due consideration to those of the Certificating Authority and shall not be more demanding for the products to be validated than it would be for similar products of its own. The Validating Authority shall notify the Certificating Authority of any such exemptions, deviations or special conditions.
Certification Basis. 3.2.1. For the purpose of issuing a Type Certificate, the Importing Party shall use for airworthiness the applicable standards for a similar product of its own that were in effect when the application for the original Type Certificate was submitted to the Exporting Party and for environmental protection the applicable standards for a similar product of its own that were applicable when the application for the Type Certificate was submitted to the Importing Party.
3.2.2. Subject to subparagraph 3.2.5 of this Procedure and for the purpose of approving a design change or repair design, the Importing Party shall specify a change to the certification basis established under subparagraph 3.2.1 of this Procedure when it considers such change appropriate for the design change or repair design.
3.2.3. Subject to subparagraph 3.2.5 of this Procedure, the Importing Party shall specify any special condition applied or intended to be applied to novel or unusual features not covered by the applicable airworthiness and environmental standards.
3.2.4. Subject to subparagraph 3.2.5 of this Procedure, the Importing Party shall specify any exemption to or deviation from the applicable standards.
3.2.5. When specifying special conditions, exemptions, deviations or changes to the certification basis, the Importing Party shall give due consideration to those of the Exporting Party and shall not be more demanding for the products of the Exporting Party than it would be for similar products of its own. The Importing Party shall notify the Exporting Party of any such special condition, exemption deviation or change to the certification basis.
Certification Basis. For the purpose of issuing a type certificate, the Validating Authority shall refer to the airworthiness standards for a similar product of its own that were in effect on the effective certification application date established by the Certificating Authority, complemented when applicable by additional technical conditions, as defined in the Technical Implementation Procedures. The environmental protection requirements used during the validation process of a type certificate shall be the applicable requirements in effect in the Party of the Validating Authority on the date of application for validation to the Validating Authority. The Validating Authority shall specify, when applicable, any: exemption to the applicable standards; deviation from the applicable standards; compensating factors that provide an equivalent level of safety when applicable standards are not complied with. The Validating Authority shall specify any special condition applied or intended to be applied if the related airworthiness code does not contain adequate or appropriate safety standards for the product, because: the product has novel or unusual design features relative to the design practices on which the applicable airworthiness code is based; or the intended use of the product is unconventional; or experience from other similar products in service or products having similar design features, has shown that unsafe conditions may develop. When specifying exemptions, deviations, compensating factors or special conditions, the Validating Authority shall give due consideration to those of the Certificating Authority and shall not be more demanding for the products to be validated than it would be for similar products of its own. The Validating Authority shall notify the Certificating Authority of any such exemptions, deviations or special conditions.
Certification Basis. (1) The subject of the validation is:
(a) any TCCA or CAAC Design Approval associated with an aeronautical product imported to either Canada or China; and,
(b) any subsequent issue of these Design Approvals that are validated by either Party.
(2) The certification basis for these Design Approvals is defined on the Design Approval and any supporting documentation.
(3) The certification basis for the purpose of the validation of the TCCA Design Approval, and issuance of a CAAC validated Design Approval or acceptance of Canadian Design Approval is the same as that of the TCCA Design Approval plus any Additional Technical Conditions (ATCs) notified. CAAC will notify in writing both TCCA and the Design Approval Holder of any ATCs necessary for the CAAC validation.
(4) The certification basis for the purpose of the validation of the CAAC Design Approval, and issuance of a TCCA validated Design Approval or acceptance of Chinese Design Approval is the same as that of the CAAC Design Approval plus any Additional Technical Conditions (ATCs) notified. TCCA will notify in writing both CAAC and the Design Approval Holder of any ATCs necessary for the TCCA validation.
Certification Basis. The regulatory basis for compliance with 14 CFR parts 34 and 36 is the effective amendment on the date of FAA certification. An applicant for a TC or Supplemental Type Certificate (STC) must show that the aircraft meets the applicable airworthiness standards, special conditions, fuel venting and exhaust emission standards of 14 CFR Part 34 and the noise standards of 14 CFR Part 36.
Certification Basis. 3.2.1. For the purpose of issuing a Type Certificate, the Importing Party shall use the applicable standards for a similar product of its own that were in effect when the application for the original Type Certificate was submitted to the Exporting Party.
3.2.2. Subject to subparagraph 3.2.5 and for the purpose of approving a design change or repair design, the Importing Party shall specify a change to the certification basis established under subparagraph 3.2.1. when it considers such change appropriate for the design change or repair design.
3.2.3. Subject to subparagraph 3.2.5., the Importing Party shall specify any special condition applied or intended to be applied to novel or unusual features not covered by the applicable airworthiness and environmental standards.
3.2.4. Subject to subparagraph 3.2.5., the Importing Party shall specify any exemption to or deviation from the applicable standards.
3.2.5. When specifying special conditions, exemptions, deviations or changes to the certification basis, the Importing Party shall give due consideration to those of the Exporting Party and shall not be more demanding for the products of the Exporting Party than it would be for similar products of its own. The Importing Party shall notify the Exporting Party of any such special condition, exemption deviation or change to the certification basis.