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AD/CESSNA 210/54 - Wing Main Spar Attachment Fittings - Inspection
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AD/CESSNA 210/54 - Wing Main Spar Attachment Fittings - Inspection
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text Cessna 210 Series Aeroplanes
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.
Background: Cracking could occur in the wing attachment lugs, in particular the lower centre lugs.