AD/S-PUMA/22 - Tail Rotor Shaft

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

Legislation au F2006B07099 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

 


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.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.