Document ID: chunk:federal_register_of_legislation:F2009L01968:body:0:p1
Version: federal_register_of_legislation:F2009L01968
Segment Type: other
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Character Range: 0–7326

AIRWORTHINESS DIRECTIVE
On the effective date specified below, and for the reasons set out in the background section, the CASA delegate whose signature appears below revokes Airworthiness Directive (AD) AD/FMS/3 and issues the following 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.

Flight Management Systems
AD/FMS/3 Amdt 1  Honeywell NZ-2000 and IC-800  6/2009
                 Navigation Computers

Applicability:  Honeywell NZ-2000 navigation computers and Honeywell IC-800 or IC-800E integrated avionics computers.
                Note 1:  These computers are known to be installed on, but not limited to, the following Transport Category aeroplanes:
                Manufacturer                                                                                                                                                                                                                                                                                                                                                                                        Model

                Bombardier, Inc                                                                                                                                                                                                                                                                                                                                                                                     CL-600-2B16 (CL-601-3A, CL-601-3R and CL-604)
                                                                                                                                                                                                                                                                                                                                                                                                                    Mystère-Falcon 900
                Dassault Aviation                                                                                                                                                                                                                                                                                                                                                                                   G-1159A, G-IV and GV
                Gulfstream Aerospace Corporation                                                                                                                                                                                                                                                                                                                                                                    382G series
                Lockheed                                                                                                                                                                                                                                                                                                                                                                                            BAe.125 Series 800A (including C-29A and U-125)
                Hawker Beechcraft (formerly Raytheon Aircraft Company)
Requirement:       1. If not previously accomplished in accordance with the original issue of this Directive, determine if the installed NZ-2000 navigation computers and IC-800 or IC-800E integrated avionics computers serving flight management systems (FMS) have computer part numbers and software modification levels identified in Honeywell Technical Newsletter (TN) A23-6111-008, Revision 001, dated
                   22 February 2007.
                Note 2:  For purposes of this Directive, aeroplanes with FMS computers having a part number and software modification level identified in the newsletter are "affected aeroplanes.''
                   2. For any affected aeroplane, revise the Limitations Section of the applicable Aircraft Flight Manual (AFM) to incorporate the information included in Appendix A of TN A23-6111-008, Revision 001.  This may be accomplished by inserting a copy of Appendix A of the newsletter into the AFM.
                   3. Upgrade the applicable software as specified in Table 1.

             After upgrading the applicable software in accordance with Requirement 3, Requirements 1 and 2 are no longer necessary and the Requirement 2 AFM revision may be removed.
             Table 1
             Upgrade new software in -                                                                                                                                                                                                                                               In accordance with the Accomplishment Instructions of -                                       For -
             The IC-800 or IC-800E integrated avionic computer (IAC), as applicable                                                                                                                                                                                                  Honeywell Alert Service Bulletin (ASB) 7017300-22-A6112, Revision 001, dated 7 February 2008  The IAC identified in ASB 7017300-22-A6112, Revision 001
             The NZ-2000 navigation computer (NAV computer)                                                                                                                                                                                                                          Honeywell ASB 7018879-34-A6060, Revision 001, dated                                           The NAV computer identified in ASB 7018879-34-A6060, Revision 001
                                                                                                                                                                                                                                                                                     21 January 2008
                                                                                                                                                                                                                                                                                     Honeywell ASB 7018879-34-A6062, dated 12 June 2007                                            The NAV computer identified in ASB 7018879-34-A6062
                                                                                                                                                                                                                                                                                     Honeywell ASB 7018879-34-A6063, dated 6 July 2007                                             The