AD/BELL 206/5 - Cyclic Pitch Control System Lever - Inspection and Modification

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

Legislation au F2006B04505 Not 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 206/5  Cyclic Pitch Control System Lever - Inspection and Modification


7/68

 

Applicability: All model 206A with S/Nos. 6 to 10, 12 to 79, 81 to 83 85 to 91, 93 to 97 and 99 to

104.

 

Document: Bell SB No. 206A-2.

 

Compliance: Inspect within 10 hours time in service and modify within 100 hours time in service after 6 June 1968.

 

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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.