AD/CESSNA 206/41 - Rear Wing Spar Doubler
1AD/CESSNA 206/41 - Rear Wing Spar Doubler
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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 206 Series Aeroplanes
AD/CESSNA 206/41 Rear Wing Spar Doubler 8/85
Applicability: All Model U206 with S/Nos U20601701 to U20604649 (1972 to 1978).
(Normally aspirated and turbocharged models which have had a rear wing spar replaced with one shipped from Cessna Supply Division).
Requirement: Action in accordance with Cessna S.B. SEB85-9.
Compliance: Within 100 hours time in service after 31 August 1985 or at the next scheduled inspection for Maintenance Release issue after 31 August 1985 whichever is the later.
Background: The manufacturer suspects that a quantity of spare rear wing spar assemblies may have been shipped from the Cessna Supply Division without a doubler installed near the attach fitting.