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

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B04707 In force Legislative Instrument

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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.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.