Commonwealth legislation

AD/CASA/8 - Flight Controls - Fail-Safe Requirements

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Commonwealth

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legislative instrument

Plain English Summary

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This AD requires modification of the elevator, rudder and aileron trim‑tab controls on all CASA‑212 aeroplanes, to be carried out per Construcciones Aeronauticas Service Bulletin SB 212‑27‑25.

Compliance is mandatory before a Certificate of Airworthiness will be issued in Australia; the party seeking that certificate must arrange and fund the modification, with CASA enforcing the requirement.

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AD/CASA/8 - Flight Controls - Fail-Safe Requirements

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source Casa 212 Series Aeroplanes

AD/CASA/8 Flight Controls - Fail-Safe Requirements 9/84

Applicability: All models CASA-212.

Document: Construcciones Aeronauticas SB 212-27-25. Compliance: Prior to issue of Certificate of Airworthiness.

Background: Modification of the elevator, rudder and aileron trim tab controls is required to meet Australian Certification Requirements.

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.