AD/S-PUMA/1 - Main Rotor Shaft

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

Legislation au F2006B07089 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/1 Main Rotor Shaft 2/91

Applicability: Versions C, C1, L and L1 which are fitted with main rotor shafts P/Nos 330A31 1222.05 or .06 modified per AMS 07.43069 and 330A31 1222.08, .09, .11 or .12.

 

Requirement: Action in accordance with the technical requirements of DGAC AD 83-095-006(B) Revision 1, dated 19 September 1990.

 

Note: Aerospatiale AS 332 SB No 05.01 R2 approved 31 August 1990, refers.

 

Compliance: In accordance with the Requirement Document.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.