AD/PT6T/6 - Fuel Pump Coupling - Replacement

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

Legislation au F2006B06376 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 - PT6T Series

 

AD/PT6T/6 Fuel Pump Coupling - Replacement 10/85

Applicability:   PT6T-3, -3B, -6; ST6T-75, -76.

 

Document: 1. Pratt and Whitney Aircraft of Canada SB No. 5184; or

 

2. AD/UAC-T/36.

Compliance:  If not already accomplished the new drive coupling is to be fitted by 31 January 1981. Background:   In Australia and overseas, fuel pump decouples have occurred on some models of

PT6 engines with similar fuel pump drive couplings. This Directive is issued in order to preclude pump decouples on twin PT6 engines by replacing the existing fuel pump drive coupling with a new coupling incorporating a flange to restrict axial movement.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.