Common use of EASA Acceptance of FAA Alteration Data Clause in Contracts

EASA Acceptance of FAA Alteration Data. (a) Except for alterations on critical components, FAA approved or accepted alterations per 14 CFR Part 43, installed on an aircraft exported from the U.S., regardless of the State of Design of the aircraft, are considered approved by the EASA at the time of import to the European Union. EASA shall accept such FAA alteration data when substantiated via an appropriately executed FAA Form 8110-3, 8100-9, or FAA Form 337 or logbook entry.

EASA Acceptance of FAA Alteration Data. (a) Except for alterations on critical components, FAA FAA-approved or accepted alterations per 14 CFR Part 43, 43 installed on an a used aircraft exported from the U.S., regardless of the State of Design of the aircraft, are considered approved by the EASA at the time of import to the European Union. EASA shall accept such FAA alteration data when substantiated via an appropriately executed FAA Form 8110-3, FAA Form 8100-9, or FAA Form 337 or logbook entry. (b) Alterations on critical components must be EASA-approved via STC in accordance with paragraph 2.2.

EASA Acceptance of FAA Alteration Data. (a) Except for alterations on critical components, FAA FAA-approved or accepted alterations per 14 CFR Part 43, 43 installed on an a used aircraft exported from the U.S., regardless of the State of Design of the aircraft, are considered approved by the EASA at the time of import to the European Union. EASA shall accept such FAA alteration data when substantiated via an appropriately executed FAA Form 8110-3, FAA Form 8100-9, or FAA Form 337 or logbook entry. Note: An FAA STC whose installation is documented on a Form 337 must be approved in accordance with TIP paragraph 2.2. (b) Alterations on critical components must be EASA-approved via STC in accordance with paragraph 2.2.