AD/DAUPHIN/32 - Main Rotor Shaft

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

Legislation au F2006B08743 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 SA 360 and SA 365 (Dauphin) Series Helicopters

 

AD/DAUPHIN/32 Main Rotor Shaft 3/92

Applicability: All model SA 365 helicopters versions C, C1, C2, C3, N, N1 and N2 fitted with main rotor mast on which the manufacturer’s modification AMS 365A 07.62 B 47 or kit No 365A 09.1034 has not been incorporated.

 

Requirement: Action in accordance with the Technical Requirements of DGAC AD 91-268-035(B) or 91-267-031(B) as applicable.

 

Note: Aerospatiale Service Bulletins SB 05.19 refers to SA 365C and SB 05.29 refers to SA 365N.

 

Compliance: As specified in the Requirement documents except the date specified in paragraph 1.1 should read 30 May 1992.

 

Background: Corrosion has been found on the rotor shaft at the lift bearing seal holder.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.