Possible Cases Sample Clauses

Possible Cases. The table in Section A, Appendix 4 contains a summary of possible cases for acceptance of parts and return to service.
Possible Cases. The following table is a summary of possible cases for acceptance of parts and return to service: CAA Form 1 NEW EASA Form 1 NEW 8130-3 NEW C of C Standard Parts Bilateral Agreements CAA Form 1 NEW EASA Form 1 NEW 8130-3 NEW C of C Standard Parts Eligible Parts meeting FAA AC 20-62 Bilateral Agreements Acceptable Repaired Products/Articles Release Document For UK CAA (input) Final Higher Assembly Release document For UK CAA (output) Acceptable Repaired Components Release Document For FAA (input) Final Higher Assembly Release document For FAA (output) FAA Form 8130-3 (Single EASA) FAA Form 8130-3 (Single EASA) CAA or EASA Form 1 (Single FAA) FAA Form 8130-3 or CAA Form 1 (Single FAA) FAA Form 8130-3 (Dual FAA/EASA) FAA Form 8130-3 (Dual FAA/EASA) EASA Form 1 (Dual FAA/EASA) CAA Form 1 (Dual CAA/FAA) EASA Form 1 (Dual FAA/EASA) FAA Form 8130-3 (Dual FAA/EASA) FAA Form 8130-3 (Dual FAA/EASA) CAA Form 1 (Dual CAA/FAA) EASA Form 1 (Single EASA) FAA Form 8130-3 (Single EASA) FAA Form 8130-3 (Single FAA) FAA Form 8130-3 or CAA Form 1-(Single FAA) CAA Form 1 (Dual CAA/FAA) FAA Form 8130-3 (Single FAA) CAA Form 1 (Dual CAA/FAA) CAA Form 1 (Dual CAA/FAA) or FAA Form 8130-3 (Single FAA) CAA Form 1 (Single CAA) None. Fitment onto UK Registered aircraft only. CAA Form 1 (Single CAA) CAA Form 1 (Single CAA) 8. REPORTING OF UNAIRWORTHY CONDITIONS TO THE FAA. This section should explain the procedures the organization will use to report any serious failures, malfunctions, or defects on a component or part of an aircraft (e.g., powerplants, propellers, or appliances) that occur as a result of aircraft/system operation. The AMO may submit the reports in the form of a letter, e-mail, accessing the Service Difficulty Report (SDR) reporting system online (▇▇▇▇://▇▇-▇▇▇▇.▇▇▇.▇▇▇/SDRx/), CAA online reporting system, or in a form and manner acceptable to the FAA containing the information required by 14 CFR § 145.221.
Possible Cases. The following table is a summary of possible cases for acceptance of parts and return to service: Acceptable New Products/Articles: CAA Form 1 NEW EASA Form 1 NEW 8130-3 NEW C of C Standard Parts Eligible Parts meeting FAA AC 20-62 Bilateral Agreements FAA Acceptable New Components: CAA Form 1 NEW EASA Form 1 NEW 8130-3 NEW C of C Standard Parts Eligible Parts meeting FAA AC 20-62 Bilateral Agreements USED Products/Articles: Acceptable Used Products/Articles Release Document (input) Final Assembly Release document (output) USED Components: Acceptable Used Components Release Document (input) AC 20-62 Final Assembly FAA Release document (output) 8130-3 Single 8130-3 Single Form 1 Single FAA 8130-3 or Form 1 Single FAA release only 8130-3 Dual 8130-3 Dual Form 1 Dual* Form 1 Dual* Form 1 Dual* 8130-3 Dual 8130 Dual 8130-3 FAA single release or Form 1 Dual* Form 1 Single Form 8130-3 Single EASA release only 8130 Single FAA 8130-3, or Form 1-Single FAA release only NOTE: * For the purpose of the table above, multiple release mentioned in subparagraph c)2)v) above has the same status as CAA or EASA Form 1 Dual.