AD/A320/29 Amdt 1 - Ram Air Turbine Bearing End-Float (Cth)
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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.