AD/BELL 412/24 - Main Rotor Pitch Link to Pitch Horn Bolt

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

Legislation au F2006B04659 Not in force Legislative Instrument

Legislation content

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Bell Helicopter Textron 412 Series Helicopters

 

AD/BELL 412/24 Main Rotor Pitch Link to Pitch Horn Bolt 7/89

TX

 

Applicability: All model 412 series.

 

Requirement: Action in accordance with Bell Alert Service Bulletin 412-89-44. Compliance: Within 5 hours time in service after receipt of this Directive.

Background: A main rotor pitch link to pitch horn bolt was found broken during an accident investigation. An inspection of the subject bolt is required pending final investigation results.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.