Document ID: chunk:federal_register_of_legislation:F2010L02437:body:0:p1
Version: federal_register_of_legislation:F2010L02437
Segment Type: other
Provision Reference: 
Character Range: 0–7925

AIRWORTHINESS DIRECTIVE
For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (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.

British Aerospace BAe 146 Series Aeroplanes
AD/BAe 146/141  State of Design Airworthiness Directives  18/2010

Applicability:  British Aerospace BAe 146 and Avro 146-RJ aircraft - all series.
Requirement:       1. Determine the applicability of the UK CAA Airworthiness Directives (AD) listed in Table 1.

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

                    Service Bulletins approved by EASA as Alternative Methods of Compliance (AMOC) to the ADs listed in Table 1 are considered acceptable for compliance with the equivalent requirements of this Airworthiness Directive.
                   Table 1
   CAA AD          Service Bulletin                                                                                                                                                                                                            Title
004-03-2001     57-064                                                                                                                                                                                                                      Replace bolts on wing rear spar
004-10-2000     57-62                                                                                                                                                                                                                       Inspect spars for corrosion and cracking
002-11-99       57-A58                                                                                                                                                                                                                      Inspect for micro-biological contamination
006-04-98       57-55                                                                                                                                                                                                                       Inspect wing stringers for machining error
007-09-97       24-120                                                                                                                                                                                                                      Inspect ERMA terminals in equipment bays
010-07-97       55-16                                                                                                                                                                                                                       Inspect elevator hinge bracket rib 1
002-03-97       SB not specified                                                                                                                                                                                                            Ex US Air and ex PSA aircraft
006-05-95       35-35-56091A                                                                                                                                                                                                                Stainless steel pipe in oxygen system
008-09-94       36-23                                                                                                                                                                                                                       Inspection of housings in bleed air system
015-05-93       29-31-01339A                                                                                                                                                                                                                Fire resistance coupling in engine bay

                CAA AD                                                                                                                                               Service Bulletin     Title
             009-04-92                                                                                                                                            27-135               Pitch servomotor mounting bracket
             006-12-91                                                                                                                                            25-299-60358D        Revised interior décor specification
             004-10-90                                                                                                                                            53-98                Pitting corrosion of fuselage skins
             011-09-90                                                                                                                                            27-114-01028B        Stall identification and warning system
             048-09-89                                                                                                                                            32-A101              Hydraulic lines to wheel brake units
             009-08-89                                                                                                                                            25-A157              Insulation bags in passenger compartment
             005-10-88                                                                                                                                            27-87                Aileron disconnect unit
             003-04-88                                                                                                                                            27-74                Aileron and elevator trim screwjacks
             009-11-86                                                                                                                                            52-55-00830A         Remove locking arm from doors
             002-08-86                                                                                                                                            24-30-00757A         DC electrical power distribution
             013-04-86                                                                                                                                            27-A54               Flap control system
             011-04-86                                                                                                                                            25-13-70039A         Modification of evacuation slide
             003-02-86                                                                                                                                            21-24-00543A         Air conditioning
             Note 1:  UK CAA 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 - before further flight after 60 days from the effective date of this Directive.
             This Airworthiness Directive becomes effective on