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
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Table 2 DGAC ADs
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Note 1: EASA and DGAC ADs may be accessed via the internet at the following URLs: http://ad.easa.europa.eu/ http://regles.gsac.fr/GSAC/ad_cns.nsf/vwAppliquablesParReference?OpenView | ||||||||||
Compliance: | For Requirements 1 and 2 - Within 30 days after the effective date of this Directive or prior to the issue of a certificate of airworthiness, which ever occurs later. | |||||||||
This Airworthiness Directive becomes effective on 22 August 2008. | ||||||||||
Background: | The EASA and DGAC ADs listed in Table 1 and Table 2 of this Directive require one time actions for which the compliance date and/or period has passed. CASA has determined that these ADs may be applicable to recently registered Australian aircraft. This Directive is issued to ensure all State of Design ADs are complied with. | |||||||||
CASA appreciates that, due to date of aircraft manufacture or aircraft configuration and modification status, not all the ADs listed in Table 1 and Table 2 will be applicable to all Eurocopter EC 225 helicopters. |