Document ID: chunk:federal_register_of_legislation:F2006B02224:body:0:p2
Version: federal_register_of_legislation:F2006B02224
Segment Type: other
Provision Reference: 
Character Range: 2896–3461

low cycle fatigue of the 2nd stage HPT wheel in the aft bore face that can lead to wheel failure, power loss, and possible damage to the aeroplane.

            This Directive was previously issued as AD/AE3007/1 however that Directive number was previously issued to another Directive. This Directive has been re-issued with a new number with no changes to the content.

 Bernard Malcolm Hole
 Delegate of the Civil Aviation Safety Authority 30 July 2004

 The above AD is notified in the Commonwealth of Australia Gazette on 8 September 2004.