Document ID: chunk:federal_register_of_legislation:F2007L04610:body:0:p2
Version: federal_register_of_legislation:F2007L04610
Segment Type: other
Provision Reference: 
Character Range: 3468–5081

29 June 2006       F-2003-202          Aileron Bellcrank
                DCA/R2000/38      29 June 2006       No Equivalent       Cabin Compartment Barrier - Inspection and Modification
                DCA/R2000/39      31 August 2006     No Equivalent       Fuel Shut - Off Mechanism

                Note 2:  NZ CAA ADs may be accessed via the internet at the following URL: http://www.caa.govt.nz/Airworthiness_Directives/Airworthiness_Directives_Home.htm
Compliance:     For Requirements 1 and 2 - Within 30 days after the effective date of this AD or prior to the issue of a Certificate of Airworthiness, whichever occurs first.
                This Airworthiness Directive becomes effective on 5 December 2007.
Background:     Alpha Aviation Design Ltd of Hamilton New Zealand is now the Type Certificate holder for the aircraft models listed in the applicability section of this AD.

                CASA has reviewed the ADs issued by the CAA (NZ) and has determined that the ADs listed in Table 1 may be applicable to Australian aircraft.  The ADs listed in Table 1 of this AD require either one time actions for which the compliance date and/or period has passed or multiple inspection/actions until a terminating action has been applied and the compliance date and/or period for the terminating action has passed.
                CASA appreciates that, due to date of aircraft manufacture or aircraft configuration and modification status, not all the ADs listed in Table 1 of this AD will be applicable to all Models.

David Punshon
Delegate of the Civil Aviation Safety Authority

29 November 2007