Document ID: chunk:federal_register_of_legislation:F2006B06128:body:0
Version: federal_register_of_legislation:F2006B06128
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Pilatus Porter PC-6 Series Aeroplanes

 AD/PC-6/25
 Amdt 1

 Aileron Balance Weight Arms - Inspection 11/72

 Applicability: All models fitted with aileron mass balance weight assembly P/No. 6106.11. Document:               Pilatus SB No. 89A.
            Compliance: Within 100 hours time in service after 30 November 1972 and there- after at intervals not exceeding 100 hours time in service until replaced by aileron balance weight assembly P/No. 111.45.08.001.