COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES Cessna 206 Series Aeroplanes AD/CESSNA 206/38 Retirement Lives - Fatigue Critical Components 6/85 Applicability: All model U206G and TU206G which have been modified in accordance with US FAA STC SA2353NM (Soloy Turbine Conversion). Requirement: Action in accordance with Soloy Turbine Pac Maintenance and Overhaul Manual, Revision No. 2 dated 1 August 1984. Compliance: All life limited components listed in Table I-8 of the Requirement document shall be retired from service before exceeding the lives quoted. Background: The components listed have been assessed as critical to flight safety. Operation beyond their published retirement lives may increase the risk of failure.