Document ID: chunk:federal_register_of_legislation:F2006B04707:body:0
Version: federal_register_of_legislation:F2006B04707
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Bell Helicopter Textron 47 (All Variants) Series Helicopters

AD/BELL 47/85 Engine Mount Strut Rod Ends - Replacement 3/81

 Applicability: All models 47 equipped with Soloy turbine conversion. Document:  Soloy Conversions Ltd. SB 03-660.
 Compliance: Within 100 hours time in service after 31 March 1981.

            Background: Replacement of stainless steel rod ends is necessary to assure the continued airworthiness of engine mount struts.