AD/A109/28 - Tail Rotor Blade Grip Assemblies

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B01813 In force Legislative Instrument

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Agusta A109 Series Helicopters

 

AD/A109/28 Tail Rotor Blade Grip Assemblies 7/97

DM

Applicability: All A109C up to Serial Number 7670, excluding 7630, 7633, 7645, 7651, 7653, 7657,

7661, 7663, 7665, 7667, and 7669.

 

Requirement: Action in accordance with Agusta Bollettino Tecnico No. 109-100, Rev A.

 

Note: RAI AD 97-084 refers.

 

Compliance: Before 30 June 1997.

 

This Airworthiness Directive becomes effective on 14 May 1997.

 

Background: Cracking has been discovered in the grip assemblies P/N 109-8131-05-109 and -113.

This Directive is issued to replace the grip assemblies with an improved item and rework of the blades to accept larger diameter bolts.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.