Document ID: chunk:federal_register_of_legislation:F2006B04581:body:0
Version: federal_register_of_legislation:F2006B04581
Segment Type: other
Provision Reference: 
Character Range: 0–925

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.