Document ID: chunk:federal_register_of_legislation:F2006B01855:body:0:p2
Version: federal_register_of_legislation:F2006B01855
Segment Type: other
Provision Reference: 
Character Range: 2838–3930

Series Aeroplanes

 AD/A320/106 Amdt 3 (Continued)

           The original issue of this Directive required the introduction of modified electrical bonding within the fuel tanks, to alleviate the risk of electrical discharges occurring.

           Amendment 1 clarified the requirement by ensuring the rework of the bonding bolts was also addressed.

           Amendment 2 required the completion of additional work for those aircraft incorporating SB A320-28-1077 at the original issue.

           This Amendment clarified the extra work required by Amendment 2 and introduced additional requirements (modification of bonding in ACT fuel tanks) for certain A321-211 and A321-231 aeroplanes.

           The original issue of this Airworthiness Directive became effective on 23 March 2000.

           Amendment 1 became effective on 19 April 2001.

           Amendment 2 became effective on 21 March 2002.

 James Coyne
 Delegate of the Civil Aviation Safety Authority 31 May 2002

 The above AD is notified in the Commonwealth of Australia Gazette on 19 June 2002.