AD/S-PUMA/9 - Electrical Power System

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

Legislation au F2006B07132 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/9 Electrical Power System 11/92

Applicability: All AS 332 helicopters, versions C, C1, L and L1, not modified per AMS 332A

07.26.044 or by kit No 332A.08.8133.

 

Requirement: Action in accordance with Eurocopter France Service Bulletin AS 332 No 24.20 dated 2 June 1992.

 

Note: DGAC AD 92-143-048(B) dated 8 July 1992 refers.

 

Compliance: Within 300 hours time in service or three calendar months from 15 October 1992, whichever occurs first.

 

Background:  Eurocopter advises that that a pressurisation system hydraulic line was perforated, following continued interference with a wire harness. Compliance with this Directive removes the possibility of the wire harness interference with and subsequent failure of the hydraulic line.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.