Common use of EASA Type Certification Basis Clause in Contracts

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 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 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.