Commonwealth legislation

AD/L200/6 - Wing and Tailplane Structural Fatigue Life

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Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This Airworthiness Directive (AD/L200/6) requires all Morava L200 owners/operators to comply forthwith with the technical measures in Omnipol IB No. L200/114 to address wing and tailplane structural fatigue life. Issued by the Civil Aviation Safety Authority, it makes those inspections/repairs and any operational limits mandatory and places scheduling, execution and costs on the owners/operators.

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AD/L200/6 - Wing and Tailplane Structural Fatigue Life

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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 Morava L200 Series Aeroplanes

AD/L200/6 Wing and Tailplane Structural Fatigue Life 10/78

Applicability: All models.

Document: Omnipol IB No. L200/114. Compliance: Forthwith.

Source text

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