AD/CESSNA 400/59 - Fuselage Tailcone Structure - Modification

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

Legislation au F2006B08344 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 400/59 Fuselage Tailcone Structure - Modification 11/78

Applicability: All 401 and 411 series.

All model 402 with S/Nos. 402-0001 to 402B1361; All model 404 with S/Nos. 404-0001 to 404-0233; All model 414 with S/Nos. 414-0001 to 414A0071; All model 421 with S/Nos. 421-0001 to 421C0511; All model 441 with S/Nos. 441-0001 to 441-0059.

 

Document: Cessna SL ME78-24.

 

Compliance: Within 100 hours time in service after 30 November 1978.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.