AD/PITTS S-2/13 - Fuselage Mounted Main Fuel Tank Filler Cap - Modification

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

Legislation au F2006B06242 Not in force Legislative Instrument

Legislation content

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Pitts S-1 and S-2 Series Aeroplanes

 

AD/PITTS S-2/13  Fuselage Mounted Main Fuel Tank Filler Cap - Modification

Applicability: All model S-1 and S-2 series aeroplanes.


4/84

 

Requirement: Install a positive retention device for the main fuel tank cap using a means acceptable to the Secretary.

 

Compliance: Before further flight after 30 June 1984.

 

Background: Engine failure from fuel exhaustion has occurred when the main fuel tank cap was lost in-flight.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Interactions

Authorises

All Versions

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.