Commonwealth legislation

AD/A109/22 - Sliding Doors Emergency Exit Panel

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

4/10 complexity

This Airworthiness Directive requires operators of Agusta A109A and A109AII helicopters to inspect and, if necessary, modify sliding-door emergency exit panels following Agusta Bollettino Tecnico 109-95. It was issued after an in‑flight loss of an emergency exit caused by incomplete locking‑pin engagement and incorrect safety‑wire installation. Compliance is mandatory within set timeframes (Part I: within 25 hours after 26 May 1994; Part II: at each 100‑hour inspection after Part I; Part III: prior to 30 June 1994). Operators and maintenance organisations must carry out the work.

JSON API

Deep dive

Want the full deep dive?

Zoe can write the in-depth analysis on top of the summary above: how it works, who it affects and what each part actually does.

Current sections

Direct links to the current provisions in AD/A109/22 - Sliding Doors Emergency Exit Panel.

AD/A109/22 - Sliding Doors Emergency Exit Panel

meta-content-style-type: text/css meta-content-type: application/xhtml+xml; charset=utf-8 meta-description: CASA Airworthiness Directive meta-generator: Aspose.Words for .NET 22.10.0 meta-keywords: Issue 8/1994,Rotorcraft,Agusta A109 Series Helicopters,Sliding Doors Emergency Exit Panel,22 title: Airworthiness Directive - AD/A109/22 - Sliding Doors Emergency Exit Panel

?xml version="1.0" encoding="utf-8" standalone="no"?>

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source Agusta A109 Series Helicopters

AD/A109/22 Sliding Doors Emergency Exit Panel 8/94

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.

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.