AD/PC-6/30 - Anti-Reverse System - Modification

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B06134 In force Legislative Instrument

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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.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.