AD/A320/73 - Frame 60 and 62 Cargo Door Frame

Airworthiness Directive - AD/A320/73 - Frame 60 and 62 Cargo Door Frame Airworthiness Directive - AD/A320/73 - Frame 60 and 62 Cargo Door Frame CASA Airworthiness Directive Jurisdiction:Commonwealth of Australia;CorporateName:Civil Aviation Safety Authority; Issue 2/1997,Aircraft above 5700 kg,Airbus Industrie A319, A320 and A321 Series Aeroplanes,Frame 60 and 62 Cargo Door Frame,73 DellaCa, Donna 2 1 2022-10-28T03:58:00Z 2022-10-28T03:59:00Z 1 184 1049 Office of Parliamentary Counsel 8 2 1231 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/A320/73   Frame 60 and 62 Cargo Door Frame   2/97 Applicability:   All Airbus A320 with bulk Cargo Door installed (Airbus Industrie Modification 20029), and without Airbus Industrie Modification 21277 or Airbus Industrie Service Bulletin A320-53-1021 incorporated.   Requirement:   Carry out an Eddy Current Inspection of the upper frame flanges at frames 60 and 62 between stringers 40 and 42 in accordance with Airbus Industrie Service Bulletin A320-53-1022 Revision 1.   If a crack is detected, repair as per Airbus Industrie Service Bulletin A320-53-1021 revision 1.   Note: French DGAC AD 96-238-091(B) refers.   Compliance:   Within 20,000 flights and within every 1,200 flights thereafter.   Note: Incorporation of Airbus Industrie Service Bulletin A320-53-1021 Revision 1 constitutes terminating action for this Directive.   This Amendment is effective from 30 January 1997.   Background:   During fatigue testing, cracking was found in the flanges of the affected frames. This directive requires inspecting for these cracks.