Document ID: chunk:federal_register_of_legislation:F2006B01943:body:0
Version: federal_register_of_legislation:F2006B01943
Segment Type: other
Provision Reference: 
Character Range: 0–845

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/A320/55 Centre Wing, Bracket Between Shroud Box and Fixed Shroud

 Applicability: As specified in the Requirement Document.

 Requirement: Action in accordance with Airbus Industrie SB A320-57-1034 Rev. 1.

            Note: DGAC AD 95-100-068(B) refers.

9/95

            Compliance: Prior to attaining 17 000 flight cycles, thereafter at the intervals specified in the Requirement Document.

            Note: Full incorporation of Airbus Industrie SB A320-57-1035 terminates this Directive.

            Background: This Directive is issued to detect and/or prevent any damage related to structural fatigue.