AD/CESSNA 188/33 - Wing Front Spar, Boom Attach Holes
1AD/CESSNA 188/33 - Wing Front Spar, Boom Attach Holes
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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 188 (Agwagon) Series Aeroplanes
AD/CESSNA 188/33 Wing Front Spar, Boom Attach Holes 4/80
Applicability: All model 188 with S/Nos. 18801178 to 18802057. Requirement: Action in accordance with Cessna SIL No. SE80-18. Compliance: Within 100 hours time in service after 30 April 1980.
Background: The boom attach holes in the front spar lower front flange may wear in service causing elongation and/or oversizing of the holes.