Document ID: chunk:federal_register_of_legislation:F2006B09046:body:0
Version: federal_register_of_legislation:F2006B09046
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Character Range: 0–971

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

 DHC-2 (Beaver) Series Aeroplanes

AD/DHC-2/28 Wing Strut Lower Steel End-Fitting 12/93
 Applicability: Model DHC-2 aircraft with steel end-fittings on C2W1115-1/-2 wing struts. Requirement:               Visually inspect the wing strut in accordance with de Havilland Alert Service Bulletin
            No. A2/48. If damage is detected, repair or replace the strut in accordance with the
            above mentioned Service Bulletin.

            Note: Transport Canada AD CF-93-21 refers.

            Compliance: Within 50 hours time in service after 11 November 1993, and thereafter at intervals not to exceed 12 calendar months.

            Background: Service difficulty reports received by Transport Canada indicated the occurrence of skin corrosion and fastener damage at the wing strut lower steel end-fittings.