Document ID: chunk:federal_register_of_legislation:F2006B08103:body:0
Version: federal_register_of_legislation:F2006B08103
Segment Type: other
Provision Reference: 
Character Range: 0–714

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.