New Modification, Replacement, and Standard Parts. (a) An AA, when importing new U.S. modification and replacement parts for products and appliances, shall accept an FAA Authorized Release Certificate on those new modification and/or replacement parts only when the FAA certifies, by the issuance of the FAA Form 8130-3 signed on the left side, that each part: (1) Is eligible for installation in a product or appliance which has been granted an EASA design approval; (2) Conforms to design data approved by EASA and is safe for installation; (3) Is marked in accordance with paragraph 5.5.2(a) of these Implementation Procedures; and (4) Meets all additional requirements prescribed by XXXX, as notified.
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Samples: Technical Implementation Procedures, Technical Implementation Procedures
New Modification, Replacement, and Standard Parts. (a) An AA, when importing new U.S. modification and replacement parts for products and appliances, shall accept an FAA Authorized Release Certificate on those new modification and/or replacement parts only when the FAA certifies, by the issuance of the FAA Form 8130-3 signed on the left side, that each part:
: (1) Is eligible for installation in a product or appliance which has been granted an EASA design approval;
; (2) Conforms to design data approved by EASA and is safe for installation;
; (3) Is marked in accordance with paragraph 5.5.2(a) of these Implementation Procedures; and
and (4) Meets all additional requirements prescribed by XXXX, as notified.by
Appears in 2 contracts
Samples: Technical Implementation Procedures, Technical Implementation Procedures
New Modification, Replacement, and Standard Parts. (a) An AA, when importing new U.S. modification and replacement parts for products and appliances, shall accept an FAA Authorized Release Certificate on those new modification and/or replacement parts only when the FAA certifies, by the issuance of the FAA Form 8130-3 signed on the left side, that each part:
: (1) Is eligible for installation in a product or appliance article which has been granted an EASA design approval;
; (2) Conforms to design data approved by EASA and is safe for installation;
; (3) Is marked in accordance with paragraph 5.5.2(a) of these Implementation Procedures; and
and (4) Meets all additional requirements prescribed by XXXXEASA, as notified.
Appears in 1 contract
Samples: Technical Implementation Procedures