Document ID: chunk:federal_register_of_legislation:F2011L01814:body:0:p2
Version: federal_register_of_legislation:F2011L01814
Segment Type: other
Provision Reference: 
Character Range: 5386–8337

Bleed Air Shut-off Valve Circuit Breakers
 92-028-2  20 January 1993    Return Filter Bypass Valve Assemblies
 92-016    24 January 1992    Flight Control Computer
 92-015-2  26 June 1992       APU Fuel Supply Line
 91-116    18 October 1991    Service/Emergency Door C-Latch Nylon Bushes
 91-106    13 September 1991  Flight Mode  Panel
 91-105    6 September 1991   Engine Fire Detection Wire
 91-071-2  6 April 1992       Passenger Address System

                Netherlands AD                                                                                                                                                                                                                                                                                                              Issue Date                                      Title
 91-013      8 January 1991                                                                                                                                                                                                                                                                                                              Primary Flight Control Servo Mounts and Motors
 90-122      26 October 1990                                                                                                                                                                                                                                                                                                             Main Wheel Assembly
             Note 1:  Netherlands ADs may be accessed via the internet at the following URL:

             http://ad.easa.europa.eu/
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 - within 60 days after the effective date of this Directive.
             This Amendment becomes effective on 9 September 2011.
Background:  The Netherlands ADs listed in Table 1 of this Directive require once-only 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, some of the ADs listed in Table 1 will not be applicable to some aeroplanes.

             Amendment 1 of this Airworthiness Directive has been issued to remove reference to Netherlands AD 94-146 from Table 1.  The release of EASA AD No. 2011-0158 (26 August 2011) supersedes Netherlands AD 94-146, thus removing the requirement to comply with AD 94-146 via this Directive.

Mike Higgins
Delegate of the Civil Aviation Safety Authority

31 August 2011