AD/PT6A/23 - Replacement of Compressor Delivery Heated Air Tube by a Non-Metallic Hose

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

Legislation au F2006B06362 Not in force Legislative Instrument

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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/23 Replacement of Compressor Delivery Heated

Air Tube by a Non-Metallic Hose


10/85

 

Applicability: PT6A-11AG engines with S/Nos. prior to PC-E10139. PT6A-15AG engines with S/Nos. prior to PC-E14012.

 

Document: 1. Pratt & Whitney Aircraft of Canada Ltd. SB No. 12024 R1, or

 

2. AD/UAC-T/38.

 

Compliance: At first opportunity consistent with availability of parts but not later than next HSI or next overhaul whichever is sooner.

 

Background: Overseas, failures of the rigid compressor delivery heated air tubes have occurred.

This Directive is issued in order to preclude further failures.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.