AD/CESSNA 188/36 - Vertical Fin Rear Spar
1AD/CESSNA 188/36 - Vertical Fin Rear Spar
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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 188/36 Vertical Fin Rear Spar 12/80 Applicability: Model 188 with S/Nos. 18801375 to 18803725 and T18803307T to T18803725T. 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.