AD/PITTS S-2/13 - Fuselage Mounted Main Fuel Tank Filler Cap - Modification
1AD/PITTS S-2/13 - Fuselage Mounted Main Fuel Tank Filler Cap - Modification
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text 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.
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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.