AD/A109/27 - Tail Rotor Blades P/N 109-8132-01-107

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

Legislation au F2006B01812 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/A109/27 Tail Rotor Blades P/N 109-8132-01-107 7/97

DM

Applicability: Model A109C with tail rotor blades Part Number 109-8132-01-107 with Serial Numbers prefixed A5- installed.

 

Requirement: Action in accordance with Agusta Bullettino Technico 109-105.

 

Note: RAI AD 97-090 refers.

 

Compliance: Within 25 hours time in Service after 12 May 1997.

 

This Airworthiness Directive becomes effective on 12 May 1997.

 

Background: This Directive is raised to inspect the bonding of the tail rotor blades tip fairing for voids and disbonding. Loss of a tip fairing will cause severe vibration, and may cause severe structural damage that may result in loss of control.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.