Document ID: chunk:federal_register_of_legislation:F2006B07089:body:0
Version: federal_register_of_legislation:F2006B07089
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Character Range: 0–706

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.