Document ID: chunk:federal_register_of_legislation:F2006B06134:body:0
Version: federal_register_of_legislation:F2006B06134
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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-6/30 Anti-Reverse System - Modification 11/70

 Applicability: All model PC-6/B1-H2 with S/Nos prior to 726.

 Requirement: 1. Modify anti-reversing circuit as per para 2.21 of Pilatus SB No. 101.

             2.    Test anti-reversing valve as per para 2.1 of Pilatus SN No. 101.

3.    Function test anti-reversing system as per para 2.22 of Pilatus SB No. 101. Compliance:              For Para. 1 - within 100 hours time in service after 31 December 1970.
            For Paras. 2 and 3 - Within 100 hours time in service after 31 December 1970 and thereafter at intervals not exceeding 100 hours time in service.