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

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B01943 In force Legislative Instrument

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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.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.