AD/BELL 206/50 - Main Rotor Pitch Link Tubes - Inspection

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

Legislation au F2006B04506 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 Canada (BHTC) 206 and Agusta Bell 206 Series Helicopters

 

AD/BELL 206/50 Main Rotor Pitch Link Tubes - Inspection 6/73

Applicability: All models.

 

Document: Bell SB No. 206-04-2-73-1.

 

Compliance: Initially within 25 hours time in service after 25 May 1973 and thereafter in accordance with the requirement document.

 

Background: AD/Agusta 206/36 equivalent.

 

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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.