AD/A320/83 - Slats-Flaps Control Computer

Airworthiness Directive - AD/A320/83 - Slats-Flaps Control Computer Airworthiness Directive - AD/A320/83 - Slats-Flaps Control Computer CASA Airworthiness Directive Jurisdiction:Commonwealth of Australia;CorporateName:Civil Aviation Safety Authority; Issue 7/1997,Aircraft above 5700 kg,Airbus Industrie A319, A320 and A321 Series Aeroplanes,Slats-Flaps Control Computer,83 DellaCa, Donna 2 1 2022-10-28T04:25:00Z 2022-10-28T04:26:00Z 1 179 1026 Office of Parliamentary Counsel 8 2 1203 16.0000 2006-09-22T00:00:00Z Toolkit http://www.activepdf.com 2022-10-28T00:00:00Z 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/A320/83   Slats-Flaps Control Computer   7/97 Applicability:   All Airbus Industrie A320 models -111,-211, -212, -214, -231, -232, -233 not having Airbus Industrie modification No. 25094 or Airbus Industrie Service Bulletin A320- 27-1096 dated 14 March 1996 incorporated.   All Airbus Industrie A321 models -111,-112 and -131 not having Airbus Industrie modification No. 25360 or Airbus Industrie Service Bulletin A320-27-1103 dated 14 June 1996 incorporated.   Requirement:   Unless previously incorporated, modify the slats-flaps control computer standard in accordance with Airbus Industrie Service Bulletin A320-27-1096 for A320 or Airbus Industrie Service Bulletin A320-27-1103 for A321.   Note: DGAC AD 97-085-099(B) refers.   Compliance:   Prior to 19 June 1999.   This Airworthiness Directive becomes effective on 19 June 1997.   Background:   The action mandated by this AD is to avoid a possible uncommanded retraction of slats and/or flaps due to command sensor unit malfunction.