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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.
In 1965 CAR 1.55 became Federal Aviation Regulation section 21.303. [12] The 1965 regulatory change also imposed specific obligations on the PMA holder related to the Fabrication Inspection System. [13] Amendment 21-38 of Part 21 was published May 26, 1972. [14] This was the next rule change to affect PMAs.
An aircraft part is an article or component approved for installation on a type-certificated aircraft. Approval for these parts is derived from the jurisdictions of the countries that an aircraft is based. In the United States, the Federal Aviation Administration oversees the approval for these parts under Federal Aviation Regulation Part 21.
The USA Federal Aviation Regulations, Part 21, §21.183(d) has a procedural definition of airworthy: "other aircraft An applicant for a standard airworthiness certificate for aircraft not covered by paragraphs (a) through (c) (a:"New aircraft manufactured under a production certificate." b:"New aircraft manufactured under type certificate only."
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]
A flight deck manual, usually part of a Quick Reference Handbook: CLR Clear Seen on GFA and is used for sky coverage CMC central maintenance computer CMM component maintenance manual CMO Certificate Management Office: FAA CMV converted meteorological visibility: CMPA complex motor-powered aircraft CMU Communications Management Unit CNS
The A 211 is the follow on to the A 210. The A 211 is a low wing, side by side seating, single engine aircraft with tricycle landing gear. [1] The aircraft is certified under German/EASA Part 21.17 rules.
JAR-OPS 1 is the Joint Aviation Requirement for the operation of commercial air transport (aeroplanes). Any commercial airline within the European Union flying jet or propeller aircraft has to comply with this standard.