Document ID: chunk:federal_register_of_legislation:F2006B01803:body:0
Version: federal_register_of_legislation:F2006B01803
Segment Type: other
Provision Reference: 
Character Range: 0–1095

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.