AD/A109/22 - Sliding Doors Emergency Exit Panel

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

Legislation au F2006B01807 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/A109/22 Sliding Doors Emergency Exit Panel 8/94

DM

 

Applicability: A109A and A109AII.

 

Requirement: Action in accordance with Agusta Bollettino Tecnico 109-95.

 

Note: RAI AD 94-71 refers.

 

Compliance: Part I: Within 25 hours time in service after 26 May 1994.

 

Part II: At each 100 hour inspection after compliance with Part I. Part III: Prior to 30 June 1994.

Background: This Directive is issued following the loss of an emergency exit in flight. This was due to incomplete engagement of the locking pins and improper safety wire installation.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.