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General requirements to be met by a CAMO are facilities (offices and documentation storage), a Continuing Airworthiness Management Exposition (CAME) which must be approved by the competent authority of the country or EASA and company procedures (to comply with Part M requirements). A CAMO can also be the operator of the aircraft.
As part of Single European Sky II (SES-II), an initiative to standardize and coordinate all air traffic control over the EU, the agency has been given additional tasks, [5] which were implemented before 2013. [6] [7] Since 4 December 2012, EASA is able to certify functional airspace blocks if more than three parties are involved. [7]
Similar standards are maintained by other aviation authorities. For example European Technical Standard Orders (ETSO) by EASA for the European Union, [3] with limited reciprocal equivalence on a per-country basis. [4] These often have the same numbers as FAA TSOs. For example, the FAA TSO for aviation headsets is C139.
With harmonization of technical content and guidance between EASA and the FAA, later advisory circulars also identify corresponding EUROCAE (ED) publications. [7] Some advisory circulars are only a few pages long and do little more than reference a recommended standard; for example, AC 20-152 referencing DO-254. [8]
FL Technics is a FAA-145 approved, as well as certified EASA Part-145, Part-CAMO, Part-147, Part-21 and GCAA certified company with hangars in Lithuania, Indonesia, and the United Kingdom, along with 70+ line stations around the world. [13]
c:"Import aircraft.") of this section is entitled to a standard airworthiness certificate if -- (1) He presents evidence to the Administrator that the aircraft conforms to a type design approved under a type certificate or a supplemental type certificate and to applicable Airworthiness Directives; (2) The aircraft (except an experimentally ...
The FAA's FAQ on Part 21 stated that PMA quality systems would be evaluated for compliance by the FAA during certificate management activity after the compliance date of the rule. [23] Today, all FAA production approvals – whether for complete aircraft or for piece parts – rely on a common set of quality assurance system elements.
EASA European Aviation Safety Agency: EAT expected approach time [1] EBOM engineering Bill of Material EBU engine build-up EC engineering control (also E/C) ECAM electronic centralised aircraft monitor ECET end of civil evening twilight: ECR Engineering Change Request ECS Environmental control system ECU Engine Control Unit (=EEC) EDR