Commonwealth legislation

AD/MU-2/16 - Main Landing Gear Drag Strut - Inspection

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legislative instrument

Plain English Summary

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This Civil Aviation Safety Authority airworthiness directive mandates inspection of the main landing gear drag strut on Mitsubishi MU-2 aeroplanes (S/N 005–337 and 501–692) in accordance with Mitsubishi Service Bulletin No. 173.

Inspections must be completed within 100 hours time-in-service after 31 May 1976; aircraft owners/operators and maintenance providers bear the costs and must follow the service bulletin or an approved alternative to maintain airworthiness.

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AD/MU-2/16 - Main Landing Gear Drag Strut - Inspection

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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 Mitsubishi MU-2 Series Aeroplanes

AD/MU-2/16 Main Landing Gear Drag Strut - Inspection 4/76

Applicability: All models with S/Nos. 005 to 337 and 501 to 692. Document: Mitsubishi SB No. 173.

Compliance: Within 100 hours time in service after 31 May 1976.

Source text

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