AD/PT6A/15 - Reversing Linkage Front End Clevis - Incorporation of Inspection Hole

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

Legislation au F2006B06356 Not in force Legislative Instrument

Legislation content

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Pratt and Whitney Canada Turbine Engines - PT6A Series

 

AD/PT6A/15  Reversing Linkage Front End Clevis - Incorporation of Inspection Hole


10/85

 

Applicability: PT6A-27, -28 engines incorporating solid link propeller reversing option prior to engine S/N PC-E40168 except S/N PC-E40153 and 40162.

 

Document: 1. UACL SB No. 166;

 

2.    UACL SB No. 1119, or

 

3.    AD/UAC-T/21.

 

Compliance: Within 100 hours time in service after 31 October 1974.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Interactions

Authorises

All Versions

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.