AD/PT6A/12 - Improved Wire Rope Reversing Cable

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

Legislation au F2006B06353 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/12 Improved Wire Rope Reversing Cable 10/85

Applicability:  All PT6A-27 engines prior to S/N PC-E40273 except E40028, 40029, 40144, 40157, 40186, 40187, 40226, 40228, 40229 and 40241 to 40247, and PT6A-28 engines prior to S/No. PC-E50027.

 

Document: 1. UACL SB No. 173, Rev. 2; or

 

2.    UACL SB No. 1126; or

 

3.    AD/UAC-T/10A.

 

Compliance: Before installation in an aircraft following next reconditioning completed after 31 December 1971.

 

Note: The above AD number has been corrected with the addition of the letter “A” which had been inadvertently omitted from previous up-dates.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.