Document ID: chunk:federal_register_of_legislation:F2006B11365:body:0
Version: federal_register_of_legislation:F2006B11365
Segment Type: other
Provision Reference: 
Character Range: 0–838

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 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.