EASA Type Certification Basis Sample Clauses
The EASA Type Certification Basis clause defines the specific regulatory requirements and standards that an aircraft or aviation product must meet to obtain type certification from the European Union Aviation Safety Agency (EASA). This clause typically outlines the applicable certification specifications, amendments, and any special conditions that apply to the product in question. For example, it may reference particular EASA regulations or detail unique compliance items for a new aircraft model. Its core practical function is to ensure that all parties are clear on the exact certification criteria, thereby facilitating regulatory approval and reducing the risk of non-compliance during the certification process.
EASA Type Certification Basis. (a) EASA shall develop its type certification basis using the applicable airworthiness codes in effect on the date application was made to the FAA for its type certificate. The applicable airworthiness requirements may be supplemented with the following additional requirements:
(1) Special conditions: For the development of special conditions, EASA shall review:
EASA Type Certification Basis. (a) EASA shall develop its type certification basis using the applicable airworthiness codes in effect on the date application was made to the FAA for its type certificate. The applicable airworthiness requirements may be supplemented with the following additional requirements:
(1) Special conditions: For the development of special conditions, EASA shall review: (i) All novel or unusual design features, (ii) The intended use of the product, (iii) Its service history, and (iv) the experience from other similar products in service or products having similar design features, having shown that unsafe conditions may develop.
(b) Applicants must also comply with the applicable noise, fuel venting, and exhaust emission standards, as defined in EASA Part 21, that are in effect on the date of application for type certification to EASA.
EASA Type Certification Basis. (a) EASA shall develop its type certification basis using the applicable airworthiness codes in effect on the date application was made to the FAA for its type certificate. The applicable airworthiness requirements may be where applicable an AA, for its type certificate. (When 14 CFR part 26 applies to a European transport category airplane, the applicable standard is the amendment in effect on the date the FAA type certificate is issued.)
(b) The applicable airworthiness requirements may be supplemented with the following additional requirements:
(1) Special conditions: The FAA shall review all novel and unusual design features for development of special conditions.
(2) Technical requirements necessary in the interest of safety: These include requirements to preclude a potential unsafe condition finding for the product under 14 CFR §21.21(b)(2). These may be generated as a result of adverse service history of this product, or other products of a similar nature or design. This includes, but is not limited to, actions taken by EASA to correct unsafe conditions.