AD/A119/11 Pilot and Co-Pilot Doors Emergency Release System (Cth)

Case
No judgment structure available for this case.

AIRWORTHINESS DIRECTIVE

For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (AD) under subregulation 39.001(1) of CASR 1998.  The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.

Agusta A119 Series Helicopters

AD/A119/11 Pilot and Co-Pilot Doors
Emergency Release System
2/2008 TX

Applicability:

Model A119 helicopters, all serial numbers.

Requirement:

Inspect and modify in accordance with Agusta Alert Technical Bulletin 119-25.

Note:  EASA Emergency AD 2007-0295-E refers.

Compliance:

Within 5 flight hours after 4 December 2007, but not later than 31 December 2007, whichever occurs first.

This Airworthiness Directive becomes effective on 4 December 2007.

Background:

During a ground test of the emergency door release system, the Pilot doors failed to disengage.  Investigation determined that the reason for the malfunction was interference between the lower hinge and the fuselage structure.  This condition, if not corrected, creates the risk of non-disengagement of the Pilot-and/or Co-pilot doors during an emergency, inhibiting the evacuation during an emergency, with possible injuries to the occupants.


David Villiers
Delegate of the Civil Aviation Safety Authority

3 December 2007

Actions
Download as PDF Download as Word Document


Cases Citing This Decision

0

Cases Cited

0

Statutory Material Cited

0