Document ID: chunk:federal_register_of_legislation:F2006B01922:body:0
Version: federal_register_of_legislation:F2006B01922
Segment Type: other
Provision Reference: 
Character Range: 0–1078

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.