AD/PA-25/22 - Fuel Tank Vent System - Modification

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

Legislation au F2006B05560 Not in force Legislative Instrument

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Piper PA-25 (Pawnee) Series Aeroplanes

 

AD/PA-25/22 Fuel Tank Vent System - Modification 11/67

Applicability: Model PA-25-235 which incorporate the modified fuel tank installation (Kit No. 514- 1-235) provided by Ansett General Aviation.

 

Requirement: 1. Install a new vent fitting P/N 514-1-8 in accordance with Ansett General Aviation SL No. 2, Revision A.

 

2.    Re-position the fuel tank vent fitting in accordance with Ansett General Aviation SL No. 4.

 

3.    Drill vent holes in the tank outer skin in accordance with Ansett General Aviation SL No. 5.

 

Compliance: Before 1 September 1971.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.