AD/CESSNA 310/50 - Wing Locker Fuel Tank Filler Cap - Rework

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Legislation au F2006B08178 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

 


Cessna 310 Series Aeroplanes

 

AD/CESSNA 310/50 Wing Locker Fuel Tank Filler Cap - Rework


11/79

 

Applicability: Model 310R with S/Nos. 310R0801 to 310R1658 fitted with wing locker auxiliary fuel tanks.

 

Document: Cessna SIL No. ME79-26.

 

Compliance: Within 100 hours time in service after 30 November 1979.

 

Background: A hole is to be drilled in the wing locker fuel tank filler cap to improve venting and to eliminate the possibility of fuel siphoning.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.