Document ID: chunk:federal_register_of_legislation:F2006B08772:body:0
Version: federal_register_of_legislation:F2006B08772
Segment Type: other
Provision Reference: 
Character Range: 0–1251

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/6
 Amdt 2

  Tail Rotor Head - Rotating Fairings and Hub Body

 6/87

            Applicability: All models SA 360, SA 361 and SA 365 equipped with the following: Rotating Fairings P/Nos:              360A33.1033.01 to .05
                                      360A33.1034.20 to .27

                                      360A33.1080.00 to .05

                                      360A33.1081.00 to .05

 Tail Rotor Hub P/Nos: 360A33.1010.02 to .15 Requirement: Inspect in accordance with Aerospatiale SA 360/365 S.B. No. 05.05.R1.
            Note: DGAC AD 83-200-19(b) refers.

 Compliance: As detailed in the Requirement Document.

            Note: This Directive shall be entered on the Maintenance Release as maintenance required. The inspection required by Para 1C(1) may be performed by the pilot in command, in which case certification is not required. A copy of the Requirement document shall be carried in the aircraft.

 Background: Amendment 2 to this Directive amends the inspection certification requirements.