AD/CESSNA 210/54 - Wing Main Spar Attachment Fittings - Inspection

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

Legislation au F2006B08103 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 210 Series Aeroplanes

 

AD/CESSNA 210/54 Wing Main Spar Attachment

Fittings - Inspection

Applicability: All model 210/T210 with S/No. 21058819 thru 21058968, T210-0198 thru T210-0338.

 

Document: Cessna S.I.L. No. SE 83-28

 

Compliance: For fittings that have achieved 4000 hours T.I.S., inspect at next 100 hourly inspection and thereafter at intervals not exceeding 100 hours time in service.


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Background: Cracking could occur in the wing attachment lugs, in particular the lower centre lugs.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.