AD/BELL 212/49 - Tail Rotor Driveshaft Hangar Bearings

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

Legislation au F2006B04581 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 212 Series Helicopters

 

AD/BELL 212/49 Tail Rotor Driveshaft Hangar Bearings 1/92

DM

 

Applicability: All models fitted with tail rotor driveshaft bearings.

 

P/N 204-040-623-003 with a S/N prefix of either “T” or “N” prior to N4000 and all - 005 bearings with a S/N prefix of either “T” or “N”.

 

Requirement: Action in accordance with Bell Alert Service Bulletin 212-91-69 Revision A.

 

Note: FAA Priority Letter AD 91-24-16 refers.

 

Compliance: Daily before first flight of the day after 27 November 1991.

 

Background: A daily inspection of the tail rotor driveshaft bearings has been found necessary following a fatal accident which revealed the possibility of a production batch problem with these bearings.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.