AD/EC 225/2 - State of Design Airworthiness Directives (Cth)

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.

Eurocopter EC 225 Series Helicopters AD/EC 225/2 State of Design Airworthiness Directives 11/2008 DM

Applicability: Eurocopter EC 225 helicopters. Requirement: 1. Determine the applicability of the EASA or Direction Générale de l'Aviation Civile of France (DGAC) Airworthiness Directives (AD) listed in Table 1 and Table 2. 2. If it is determined that an EASA or DGAC AD listed in Table 1 and Table 2 is applicable and has not been previously accomplished, perform the actions required by that AD.

Table 1 EASA ADs EASA AD Number Effective Date Title 2006-0146 12 June 2006 Engine Indicating - Torquemeter Printed Circuit Boards 2006-0244 1 September 2006 Rotor Flight Controls - Collective Lever Control 2006-0299 15 October 2006 Crash Position Indicator Interface Unit 2006-0300 15 October 2006 Crash Position Indicator ELT Water-activated Switch 2006-0340R1 23 November 2006 Equipment and Furnishings - Seal of the Jettisonable Window Panel 2007-0115 11 May 2007 Ice and Rain Protection - Main Rotor Blade De-Icing System Harness Connectors 2007-0134 28 May 2007 Main Rotor Drive - Engine-to-Main Gearbox Coupling Shaft Flange Threaded Attachment Bolt Assembly 2008-0075 6 May 2008 Seat Harness Belt Buckle Blanking Plugs