AD/PT6A/19 - Fuel Control Bypass Valve Diaphragm

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

Legislation au F2006B06359 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/19 Fuel Control Bypass Valve Diaphragm 10/85

Applicability: PT6A-38, -41 and 45A engines fitted with Aviation Electric Fuel Control Units P/No 3244723-3 thru -10, 3244738-5, 3244738-6, 3244752-6 thru -10, and 3244755-7 thru-

11.

 

Document: 1. Pratt & Whitney Aircraft of Canada SB No. 3103; 2. FAA AD 78-17-07, Amendment 39-3287; or

3. AD/UAC-T/31.

 

Compliance: Within the next 100 hours time in service after 30 November 1978.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.