AD/MU-2/35 - Horizontal Stabiliser Leading Edge Skin - Inspection and Modification
1AD/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
Image unavailable in extracted text 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.