Document ID: chunk:federal_register_of_legislation:F2010L02435:body:0:p1
Version: federal_register_of_legislation:F2010L02435
Segment Type: other
Provision Reference: 
Character Range: 0–5452

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/B767/256 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.

Boeing 767 Series Aeroplanes
AD/B767/256 Amdt 1  State of Design Airworthiness Directives  18/2010

Applicability:                                                           Boeing 767 aircraft.
Requirement:                                                                1. Determine the applicability of the United States Federal Aviation Administration (FAA) Airworthiness Directives (ADs) listed in Table 1.

                                                                            2.         If it is determined that an FAA AD listed in Table 1 is applicable and has not been previously accomplished, perform the actions required by that AD or later FAA-approved revision.

                                                                         Service Bulletins approved by the FAA as Alternative Methods of Compliance (AMOC) to the FAA ADs listed in the Table 1 are considered acceptable for compliance with the equivalent requirements of this Directive.
                                                                            Table 1
   FAA AD                                                                   Effective Date                                                                                                                                                                                                       Title
2005-05-20                                                               17 April 2006                                                                                                                                                                                                        Flight deck door electronic equipment
2004-16-11                                                               13 September 2004                                                                                                                                                                                                    Hanger arm of RAT hydraulic pump
2000-11-08                                                               6 July 2000                                                                                                                                                                                                          Fuel nozzles
93-05-13                                                                 18 March 1993                                                                                                                                                                                                        Power feeder connectors
92-16-10                                                                 28 September 1992                                                                                                                                                                                                    Slat hydraulic pressure tubes
90-17-08                                                                 17 September 1990                                                                                                                                                                                                    Anti-ice system
88-19-05                                                                 26 September 1988                                                                                                                                                                                                    Firewall seal
Note 1:  FAA ADs may be accessed via the internet at the following URL:

http://rgl.faa.gov

Compliance:  If a certificate of airworthiness has not been issued for the aircraft - before issue of the certificate of airworthiness.

             If a certificate of airworthiness has been issued for the aircraft - before further flight after 19 October 2010.

             This Amendment becomes effective on 10 September 2010.

             Note 2:  This amendment relieves the operator of certain requirements and so the compliance dates have been maintained as per the original issue.
Background:  The FAA ADs listed in Table 1 of this Directive require once-only actions for which the compliance date has passed.  CASA has determined that these ADs may be applicable to some Australian aircraft.  This Directive is issued to ensure compliance with all State of Design ADs.

             CASA appreciates that, due to date of aircraft manufacture or aircraft configuration and modification status, some of the ADs listed in Table 1 will not be applicable to any aircraft presently registered in Australia.

             This Amendment removes two FAA ADs from the Requirements section