U.S. Type Certification Basis. (a) The FAA will develop its type certification basis using the applicable airworthiness standards (14 CFR) in effect on the date application was made to the CAA-NL for the Dutch type certificate. The applicable airworthiness requirements may be supplemented with the following additional requirements: (1) Special conditions: The FAA will 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 3.0.1.3.2
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Samples: Implementation Procedures
U.S. Type Certification Basis. (a) The FAA will develop its type certification basis using the applicable airworthiness standards (14 CFR) in effect on the date application was made to the CAA-NL UKCAA for the Dutch U.K. type certificate. The applicable airworthiness requirements may be supplemented with the following additional requirements: (1) Special conditions: The FAA will 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 3.0.1.3.2
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Samples: www.faa.gov
U.S. Type Certification Basis. (a) The FAA will develop its type certification basis using the applicable airworthiness standards (14 CFR) in effect on the date application was made to the CAA-NL LFV for the Dutch Swedish type certificate. The applicable airworthiness requirements may be supplemented with the following additional requirements: (1) Special conditions: The FAA will 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 3.0.1.3.2
Appears in 1 contract
Samples: www.faa.gov
U.S. Type Certification Basis. (a) The FAA will develop its type certification basis using the applicable airworthiness standards (14 CFR) in effect on the date application was made to the CAA-NL DGAC for the Dutch French type certificate. The applicable airworthiness requirements may be supplemented with the following additional requirements: (1) Special conditions: The FAA will 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 the DGAC to correct unsafe conditions. 3.0.1.3.2
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Samples: www.faa.gov