Document ID: chunk:federal_register_of_legislation:F2006B01970:body:0
Version: federal_register_of_legislation:F2006B01970
Segment Type: other
Provision Reference: 
Character Range: 0–1090

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/A320/81 Connecting Angle Between Frame 56
                     and Frame Support at Stringer 38

 5/97

            Applicability: A320, all models and serial numbers without Airbus Industrie Mod 20941 embodied, or Airbus Industrie SB A320-53-1011 incorporated.

 Requirement: Inspect in accordance with A320-53-1084 Rev 1.

            Note: DGAC AD 96-237-090(B) refers.

            Compliance Before the accumulation of 20 000 flights; thereafter at intervals not exceeding 12 000 flights; unless cracking has been detected, in which case, in accordance with thresholds and intervals specified in the Requirement Document.

            This Airworthiness Directive becomes effective on 24 April 1997.

            Background:  This Directive is raised in order to detect cracking in the subject connecting angle, which could affect the structural integrity of the aircraft.