Commonwealth legislation

AD/MU-2/35 - Horizontal Stabiliser Leading Edge Skin - Inspection and Modification

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This AD requires owners/operators of specified Mitsubishi MU-2 aeroplanes to inspect the horizontal stabiliser leading edge skin and, where cracks are found, replace and reinforce it in accordance with Mitsubishi Heavy Industries Service Recommendation No. 062A.

Compliance is mandatory by the next Maintenance Release after 31 May 1985 and at each subsequent Maintenance Release until modification is complete; owners/operators bear costs and CASA enforces the requirement.

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AD/MU-2/35 - Horizontal Stabiliser Leading Edge Skin - Inspection and Modification

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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-2/35 Horizontal Stabiliser Leading Edge Skin - Inspection and Modification

5/85

Applicability: All models referenced in Mitsubishi Heavy Industries Service Recommendation No 062A.

Requirement: Mitsubishi Heavy Industries Service Recommendation No. 062A.

Compliance: Prior to issue of the next Maintenance Release after 31 May 1985 and thereafter at each issue of a new Maintenance Release until modified.

Background: This Directive is issued to ensure cracked horizontal stabiliser leading edge skins are replaced and reinforced in accordance with the manufacturers repair scheme.

Source text

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