AD/A320/30 - Seat Track Joints at Frame 64

Airworthiness Directive - AD/A320/30 - Seat Track Joints at Frame 64 Airworthiness Directive - AD/A320/30 - Seat Track Joints at Frame 64 CASA Airworthiness Directive Jurisdiction:Commonwealth of Australia;CorporateName:Civil Aviation Safety Authority; Issue 8/1993,Aircraft above 5700 kg,Airbus Industrie A319, A320 and A321 Series Aeroplanes,Seat Track Joints at Frame 64,30 DellaCa, Donna 2 0 2022-10-27T00:24:00Z 2022-10-27T00:24:00Z 1 150 860 Office of Parliamentary Counsel 7 2 1008 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/A320/30   Seat Track Joints at Frame 64   8/93 DM Applicability:   Aircraft S/nos 002 to 008, 010 to 014, 016 to 078, 080 to 122, 124 to 179, 183 to 194, 196 to 228, 230 to 251, 253 to 255 inclusive.   Requirement:   1. Inspect in accordance with Airbus Industrie AOT 53-01 dated 27 August 1992.   2. Modify in accordance with Airbus Industrie SB A320-53-1088 if the gap is greater than 2.8mm.   Note: DGAC AD 93-081-042(B) refers.   Compliance:   1. Prior to 31 July 1993. Thereafter, where the gap is greater than 2.8 mm, at each configuration change until modified.   2. Prior to 31 December 1995.   Background:   At frame 64 the seat track gap may be excessive. This may result in the release of seats and /or other attached equipment under the loads that may be experienced during an emergency landing.