Document ID: chunk:federal_register_of_legislation:F2006B01846:body:0:p2
Version: federal_register_of_legislation:F2006B01846
Segment Type: other
Provision Reference: 
Character Range: 2727–3338

grip modification is also specified for helicopters with the P/N 109-8131-02-149 tail rotor hub and blade assembly fitted. A placard is also fitted to reduce Vne by 30 KIAS until the requirements of Part IV of Agusta Alert Service Bulletin 119-6, Revision A are complied with, upon which the placard may be removed.

           The original issue of this Airworthiness Directive became effective on 3 July 2002.

 David Alan Villiers
 Delegate of the Civil Aviation Safety Authority 17 July 2002

 The above AD is notified in the Commonwealth of Australia Gazette on 18 July 2002.