EASA Orders Checks Of Thales AoA Probe

jueves, 11 de febrero de 2010

http://www.aviationweek.com/aw/generic/story_channel.jsp?channel=comm&id=news/awx/2010/02/10/awx_02_10_2010_p0-203459.xml

The inspections are necessary to identify and replace parts suspected of causing inaccurate AoA indications. The requirement comes from a Feb. 9 airworthiness directive issued by the European Aviation Safety Agency (EASA) after final assembly line testing revealed that AoA data from two different aircraft were incorrect. Flight data analysis confirmed the inaccuracies.




2010-0016R1 : Navigation – Thales Avionics Angle of Attack (AoA) Probe – Inspection / Replacement

Number 2010-0016R1
Issued by Europe  Europe
Issue date 2010-02-09
Effective date 2010-02-10
EASA approval number
Contributor EASA Large Aeroplanes Section
ATA Chapter 34
Approval Holder
/ Type Designation
  • AIRBUS
    • A330
      • 201
      • 202
      • 203
      • 223
      • 243
      • 301
      • 302
      • 303
      • 321
      • 322
      • 323
      • 341
      • 342
      • 343
    • A340
      • 211
      • 212
      • 213
      • 311
      • 312
      • 313
      • 541
      • 542
      • 642
      • 643
Revision This AD revises EASA AD 2010-0016 dated 27 January 2010. This AD revision is issued to specify that the identification of the affected AoA probes is also possible in accordance with aeroplane maintenance records data analysis.
Correction Not applicable
Supersedure None
Related information Airbus Service Bulletin A330-34-3232 at original issue; Airbus Service Bulletin A340-34-4239 at original issue; Airbus Service Bulletin A340-34-5072 at original issue. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. Thales Service Bulletin C16291A-34-007 Revision 01 dated 03 December 2009.
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. The required actions and the risk allowance have granted the issuance of a Final AD with Request for Comments, postponing the public consultation process after publication. 3. Enquiries regarding this AD should be referred to the Airworthiness Directives, Safety Management & Research Section, Certification Directorate, EASA. E-mail: ADs@easa.europa.eu . 4. For any questions concerning the technical content of the requirements in this AD, please contact: AIRBUS – Airworthiness Office – EAL; E-mail: airworthiness.A330-A340@airbus.com .


http://ad.easa.europa.eu/blob/easa_ad_2010_0016_R1.pdf/AD_2010-0016R1_1



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