AD/A109/23 - Tail Boom and Vertical Fin Modification

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

Legislation au F2006B01808 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/A109/23 Tail Boom and Vertical Fin Modification 8/94

Applicability: All models A109A, A109AII and A109C with serial numbers up to and including 7670, except for serial numbers 7630, 7633, 7645, 7651, 7654, 7663, and 7665 to

7669.

 

Requirement: Action in accordance with Agusta Bollettino Technico 109-96.

 

Note: RAI AD 94-098 refers.

 

Compliance: Part I - Within 100 hours time in service after 21 July 1994 or prior to 30 June 1995, whichever occurs first.

 

Part II - At each 300 hour inspection after accomplishment of Part I.

 

Background:  Some cracking of structural parts has been found in the vertical fin attachment area of the tail boom. This Directive provides for ready access to the area, and the inspection requirements.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.