Commonwealth legislation

AD/S-PUMA/1 - Main Rotor Shaft

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Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

5/10 complexity

This airworthiness directive requires owners/operators and maintenance organisations of Eurocopter AS 332 C/C1/L/L1 helicopters fitted with specified main rotor shaft part numbers to carry out the actions set out in DGAC AD 83-095-006(B) Revision 1. Issued under Australia’s Civil Aviation framework, it enforces that foreign technical standard without reproducing the procedures, so affected operators bear the inspection/repair costs and administrative burden of obtaining and following the referenced document.

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AD/S-PUMA/1 - Main Rotor Shaft

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source 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.

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.