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  2. Continuing airworthiness management organization - Wikipedia

    en.wikipedia.org/wiki/Continuing_Airworthiness...

    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.

  3. Joint Aviation Requirements - Wikipedia

    en.wikipedia.org/wiki/Joint_Aviation_Requirements

    The European Aviation Safety Agency (EASA) was created in 2003 and reached full functionality in 2008, and has since taken over most of the JAA functions. JAA Certification Specifications, formerly known as JARs, are recognised by EASA as an acceptable basis for showing compliance with their national airworthiness codes.

  4. Parts Manufacturer Approval - Wikipedia

    en.wikipedia.org/wiki/Parts_Manufacturer_Approval

    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.

  5. European Union Aviation Safety Agency - Wikipedia

    en.wikipedia.org/wiki/European_Union_Aviation...

    EASA is responsible for new type certificates and other design-related airworthiness approvals for aircraft, engines, propellers and parts. EASA works with the EU member states' civil aviation authorities (CAAs) but has taken over many of their functions in the interest of aviation standardisation across the EU and in the non-EU member Turkey. [12]

  6. Airworthiness - Wikipedia

    en.wikipedia.org/wiki/Airworthiness

    One airworthiness regulation is found in ICAO international standard of Annex 8 to Chicago Convention on International Civil Aviation which defines "airworthy" - in respect of an aircraft, engine, propeller or part there of - as "The status of an aircraft, engine, propeller or part when it conforms to its approved design and is in a condition for safe operation".

  7. DO-160 - Wikipedia

    en.wikipedia.org/wiki/DO-160

    DO-160, Environmental Conditions and Test Procedures for Airborne Equipment is a standard for the environmental testing of avionics hardware. It is published by the Radio Technical Commission for Aeronautics (RTCA) and supersedes DO-138 .

  8. JAR-OPS 1 - Wikipedia

    en.wikipedia.org/wiki/JAR-OPS_1

    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.

  9. Certification Review item - Wikipedia

    en.wikipedia.org/wiki/Certification_Review_item

    Certification Review Item (CRI) is a document describing an item that requires disposition prior to the issuance of Type Certificate (TC), change to TC approval or Supplemental Type Certificate (STC) by European Aviation Safety Agency (EASA).