AD/BELL 206/11 - Main Rotor Blade Retention Bolt - Inspection

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

Legislation au F2006B04423 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 206/11 Main Rotor Blade Retention Bolt - Inspection 2/69

Applicability: All model 206A prior to S/Nos. 175 and AB-206A prior to S/No. 8080, plus spare blade retention bolts P/N | 206-010-152-1.

 

Document: Bell SL No. 206A-55.

 

Note: Agusta SB No. BT206-21 refers.

 

Compliance: Within 100 hours time in service after 14 Feb. 1969 for installed bolts, and before installation in an aircraft for replacement bolts.

 

Background: AD/Agusta 206/3 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.