Commonwealth legislation

AD/MU-2/15 - Main Landing Gear Door Mechanism Support - Inspection

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This Airworthiness Directive from the Civil Aviation Safety Authority requires owners/operators of Mitsubishi MU-2B-30 and MU-2B-35 aircraft (S/N 501–585) to inspect the main landing gear door mechanism support within 100 hours TIS after 27 Feb 1976 and every 100 hours thereafter until modified per Mitsubishi Service Bulletin No. 172. Operators fund the inspections or can eliminate recurring checks by completing the SB 172 modification.

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AD/MU-2/15 - Main Landing Gear Door Mechanism Support - 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-2/15 Main Landing Gear Door Mechanism

Support - Inspection

Applicability: All model MU-2B-30/-35 with S/Nos. 501 to 585. Document: Mitsubishi SB No. 172.

1/76

Compliance: Within 100 hours time in service after 27 February 1976 and there- after at intervals not exceeding 100 hours time in service until modified in accordance with SB No. 172.

Source text

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