Document ID: chunk:federal_register_of_legislation:F2006B01920:body:0
Version: federal_register_of_legislation:F2006B01920
Segment Type: other
Provision Reference: 
Character Range: 0–1276

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

 Airbus Industrie A319, A320 and A321 Series Aeroplanes

 AD/A320/29
 Amdt 1

 Ram Air Turbine Bearing End-Float 9/95

            Applicability: All A320 series aircraft fitted with P/N 680203020 or 680203021 or 680203027 Ram Air Turbine and not incorporating Airbus Industries modification 24701 or Airbus Industries SB A320-29-1065.

 Requirement: 1. Action in accordance with Airbus Service Bulletin A320-29-1061.

             2. Unless previously carried out action in accordance with Airbus Service Bulletin A320-29-1065.

            Note: DGAC AD 93-057-041(B)R1 and Dowty Aerospace Hydraulics - Cheltam Service Bulletin No 600-29-171 refers.

             Compliance: 1. The effective date specified in the original issue remains unchanged at 13 July 1993.

            2. Prior to 30 June 1997.

            Note: Compliance with Airbus Industries SB A320-29-1065 provides terminating action for this directive.

            Background: The manufacturer has advised that a Ram Air Turbine became detached from its leg during a ground functional test. This amendment provides terminating action for this directive.