AD/BELL 412/36 - Main Rotor Mast

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

Legislation au F2006B04670 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 412 Series Helicopters

 

AD/BELL 412/36 Main Rotor Mast 5/95

Applicability: All model 412 series helicopters fitted with main rotor mast P/N 412-040-101-105,

-109, -117, -121, -125, -127, -129 and spline plate P/N 412-010-167-101, -105 or

412-010-177-101, -105, -109, -113 or -117.

Requirement: Action in accordance with Bell Alert Service Bulletin 412-94-81 Revision A. Compliance:               Within 100 hours time in service from 27 April 1995 or by 27 August 1995,

whichever occurs first.

 

Background:  The manufacturer has revised the procedures for determining the retirement life of the main rotor mast and spline plate for the 412 and 412SP, which now has a retirement life of 10,000 hours or 80,000 maximum Retirement Index Numbers (RIN), whichever occurs first. For the 412HP and 412EP the retirement life is 10,000 hours or 60,000 RIN, whichever occurs first.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.