AD/CESSNA 206/38 - Retirement Lives - Fatigue Critical Components
1AD/CESSNA 206/38 - Retirement Lives - Fatigue Critical Components
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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 206/38 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.