AD/CESSNA 400/69 - Wing Locker Fuel Tank Filler Cap - Rework

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

Legislation au F2006B08352 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 400 Series Aeroplanes

 

AD/CESSNA 400/69 Wing Locker Fuel Tank Filler Cap - Rework 11/79

Applicability: Model 402B with S/Nos. 402B1201 to 402B1384 and Model 414 with S/Nos. 414- 0901 to 414-0965 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.