Commonwealth legislation

AD/MU-2/28 - Nose Landing Gear Eccentric BO - Inspection and Replacement

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Commonwealth

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legislative instrument

Plain English Summary

3/10 complexity

This directive requires owners/operators of Mitsubishi MU-2B-26A and MU-2B-40 aeroplanes (S/N 336SA–457SA) to inspect the nose-landing-gear drag-strut eccentric bolt within 100 flight hours after 31 Dec 1983 and every 100 hours thereafter until the bolt is replaced per Mitsubishi Service Bulletin SBO 38/32-002. It aims to prevent bolt failures; operators bear inspection, replacement and labor costs and must follow the manufacturer’s procedure to show compliance.

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AD/MU-2/28 - Nose Landing Gear Eccentric BO - Inspection and Replacement

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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-2/28 Nose Landing Gear Eccentric BO - Inspection

and Replacement Applicability: All models MU-2B-26A/-40 with S/Nos. 336SA thru 457SA. Document: Mitsubishi Aircraft International S.B. No. SBO 38/32-002.

12/83

Compliance: Unless already accomplished within 100 hours time in service after 31 December 1983 and thereafter at intervals not exceeding 100 hours time in service until replacement in accordance with requirement document.

Background: The manufacturer has received reports of failures of the nose landing gear drag strut eccentric bolt, and this inspection is intended to preclude such failures.

Source text

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