Commonwealth legislation

AD/MU-2/13 - Main Landing Gear Forward Door Emergency Cable - Inspection

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legislative instrument

Plain English Summary

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This directive requires operators of specified Mitsubishi MU-2B-30/35 aeroplanes (limited serial-number ranges, excluding aircraft fitted with Cable P/N 030A-38558-41/51) to inspect the main landing-gear forward door emergency cable per Mitsubishi Service Bulletin No. 170.

Inspections start within 100 hours TIS after 31‑Dec‑1975 and recur every 100 hours; owners/operators bear inspection and downtime costs and must consult SB No. 170 for the technical procedure and any corrective actions.

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AD/MU-2/13 - Main Landing Gear Forward Door Emergency Cable - 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-2/13 Main Landing Gear Forward Door Emergency Cable - Inspection

11/75

Applicability: All models MU-2B-30 with S/Nos. 502 to 547, and MU-2B-35 with S/Nos. 501 and 548 to 615. Not fitted with Cable P/N 030A-38558-41/51.

Document: Mitsubishi SB No. 170.

Compliance: Within 100 hours time in service after 31 December 1975 and there- after at intervals not exceeding 100 hours time in service.

Source text

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