AD/A320/29 Amdt 1 - Ram Air Turbine Bearing End-Float

Airworthiness Directive - AD/A320/29 Amdt 1 - Ram Air Turbine Bearing End-Float Airworthiness Directive - AD/A320/29 Amdt 1 - Ram Air Turbine Bearing End-Float CASA Airworthiness Directive Jurisdiction:Commonwealth of Australia;CorporateName:Civil Aviation Safety Authority; Issue 9/1995,Aircraft above 5700 kg,Airbus Industrie A319, A320 and A321 Series Aeroplanes,Ram Air Turbine Bearing End-Float,29 Amdt 1 DellaCa, Donna 3 4 2022-10-27T00:14:00Z 2022-10-27T00:19:00Z 1 179 1024 Office of Parliamentary Counsel 8 2 1201 16.0000 2006-09-22T00:00:00Z Toolkit http://www.activepdf.com 2022-10-27T00:00:00Z 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.