AD/BELL 206/112 Amdt 1 - Tail Rotor Yoke

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

Legislation au F2006B04426 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 206/112

Amdt 1


Tail Rotor Yoke 4/89

 

Applicability: All model 206A, 206B11, 206B111, 206L, 206L-1, 206L-3, Agusta Bell AB206A and AB206B.

 

Requirement: Inspect in accordance with Bell Helicopter Alert Service Bulletin 206-88-41 or 206L-88-51, as applicable.

 

Note: FAA AD 88-23-03 and Italian AD 88-215/AB206-121 refer.

 

Compliance: Unless already accomplished, within 100 hours time in service from 30 April 1989.

 

Background: A number of tail rotor yokes have been manufactured with the blade attaching bolt holes incorrectly located.

 

This amendment raised to include the Agusta Bell 206 series.

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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.