Document ID: chunk:federal_register_of_legislation:F2006B05243:body:0
Version: federal_register_of_legislation:F2006B05243
Segment Type: other
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Character Range: 0–913

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.