AD/CESSNA 185/35 - Vertical Fin Rear Spar

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

Legislation au F2006B05126 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 185 Series Aeroplanes

 

AD/CESSNA 185/35 Vertical Fin Rear Spar 12/80

Applicability: Model 185 with S/Nos. 18502311 to 18504070. Requirement:  Action in accordance with Cessna SIL No. SE80-85. Compliance:               Within 100 hours time in service after 31 December 1980.

Background: Overseas, cracks have been found in the flanges and web of the spar below the lower rudder hinge.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.