AD/BELL 222/4 - Tail Rotor Servo Control Linkage

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

Legislation au F2006B04619 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) 222 Series Helicopters

 

AD/BELL 222/4 Tail Rotor Servo Control Linkage 9/85

TX

 

Applicability: All model 222 and 222U Helicopters.

 

Requirement: Action in accordance with Bell Helicopter Textron Alert Service Bulletins 222-85-33 and 222U-85-8.

 

Note: Copies of the requirement documents may be obtained from Department of Aviation Regional Offices.

 

Compliance: Before further flight after 19 July 1985.

 

Background: A 222 overseas while hovering experienced an uncontrollable right turn. The cause was found to be a disconnect of the control linkage on the tail rotor servo. A linkage rivet was missing which allowed the pivot pin to fall out.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.