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2008-0173R1 : Electrical Power / Airborne Auxiliary Power – Auxiliary Power Unit (APU) Generator – Inspection / Modification

Number 2008-0173R1
Issued by Europe  Europe
Issue date 2010-10-22
Effective date 2010-11-05
EASA approval number
ATA Chapter 24/49
Approval Holder
/ Type Designation
  • AIRBUS S.A.S.
    • A330
      • A330-201
      • A330-202
      • A330-203
      • A330-223
      • A330-243
      • A330-301
      • A330-302
      • A330-303
      • A330-321
      • A330-322
      • A330-323
      • A330-341
      • A330-342
      • A330-343
    • A340
      • A340-211
      • A340-212
      • A340-213
      • A340-311
      • A340-312
      • A340-313
      • A340-541
      • A340-542
      • A340-642
      • A340-643
Revision This AD revises EASA AD 2008-0173 dated 15 September 2008, which superseded EASA AD 2008-0017R1 dated 17 June 2008.
Correction Not applicable
Supersedure None
Publication(s) and related information Airbus AOT A330-24A3044 Revision 03 Airbus AOT A340-24A4057 Revision 03 Airbus AOT A340-24A5021 Revision 02 Airbus SB A330-24-3045 at original issue Airbus SB A340-24-4058 at original issue Airbus SB A340-24-5022 at original issue. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. The original issue of this AD was posted on 19 August 2008 as PAD 08-095 for consultation until 02 September 2008. The Comment Response Document can be found at https://ad.easa.europa.eu. 3. Enquiries regarding this AD should be referred to the Airworthiness Directives, Safety Management & Research Section, Certification Directorate, EASA; E-mail: ADs[at]easa.europa[dot]eu .