Document ID: chunk:federal_register_of_legislation:F2006B08737:body:0
Version: federal_register_of_legislation:F2006B08737
Segment Type: other
Provision Reference: 
Character Range: 0–745

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/26
 Amdt 1

 Tail Rotor Control Shaft 1/92

 Applicability: All model SA 360, 365C, C1, C2, C3, N and FS Helicopters. Requirement:  Action in accordance with Aerospatiale SB 05.15 or 05.24, as applicable.
            Note: D6AC AD 90-204-033(B) refers to SB 05.15 only.

 Compliance: As specified in the Requirement document.

            Background:  Excessive wear of the tail rotor control shaft bearings could result in loss of tail rotor control. This amendment extends the Requirement to all 365 series helicopters.