Document ID: chunk:federal_register_of_legislation:F2006B08743:body:0
Version: federal_register_of_legislation:F2006B08743
Segment Type: other
Provision Reference: 
Character Range: 0–949

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.