Document ID: chunk:federal_register_of_legislation:F2006B01807:body:0
Version: federal_register_of_legislation:F2006B01807
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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.