Document ID: chunk:federal_register_of_legislation:F2006B07099:body:0
Version: federal_register_of_legislation:F2006B07099
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Eurocopter AS 332 (Super Puma) Series Helicopters

AD/S-PUMA/22 Tail Rotor Shaft  7/96 DM

 Applicability: All model AS 332 helicopters.

            Requirement: Action in accordance with Eurocopter Mandatory Service Bulletin 05.00.41 dated January 29, 1996.

            Note: DGAC AD 96-074-057(B) refers.

 Compliance: As specified in the Requirement Document.

            Background: The manufacturer has advised that a crack in one of the tail rotor flapping hinge retainers has been found.