Document ID: chunk:federal_register_of_legislation:F2006B07132:body:0
Version: federal_register_of_legislation:F2006B07132
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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.