AD/A109/19 Amdt 2 - Tail Rotor Hub

Airworthiness Directive - AD/A109/19 Amdt 2 - Tail Rotor Hub Airworthiness Directive - AD/A109/19 Amdt 2 - Tail Rotor Hub CASA Airworthiness Directive Jurisdiction:Commonwealth of Australia;CorporateName:Civil Aviation Safety Authority; Issue 9/1995,Rotorcraft,Agusta A109 Series Helicopters,Tail Rotor Hub,19 Amdt 2 DellaCa, Donna 2 0 2022-10-20T23:55:00Z 2022-10-20T23:55:00Z 1 152 867 Office of Parliamentary Counsel 7 2 1017 16.0000 2006-09-21T00:00:00Z Toolkit http://www.activepdf.com 2022-10-20T00:00:00Z COMMONWEALTH OF AUSTRALIA   (Civil Aviation Regulations 1998) , PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES   Agusta A109 Series Helicopters   AD/A109/19 Amdt 2 Tail Rotor Hub   9/95   Applicability:   All A109C helicopters equipped with Fork Assy P/N 109-8131-05-109 and -113 installed on Tail rotor Assy P/N 1009-8131-02-115.   Requirement:   1. Inspect in accordance with Bollettino Technico Telegrafico No. 109-8 Rev. A, and   2. Modify in accordance with Bollettino Technico No. 109- 100.   Note: RAI AD 95-101 refers.   Compliance:   1. In accordance with the Requirement Document until modified, and   2. Prior to 31 March 1997.   For Requirement 1 the effective date was 25 January 1992. This amendment is effective 17 August 1995. Background:     The initial issue of this Directive was to address cracking of the flange of the tail rotor grip. Amendment 1 extended the inspection to the -113 part number grip.   Amendment 2 provides terminating action through modification.