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2013-0129 : Airborne Auxiliary Power – Auxiliary Power Unit Exhaust Tailpipe – Modification

Number 2013-0129
Issued by Europe  Europe
Issue date 2013-06-21
Effective date 2013-07-05
EASA approval number
ATA Chapter 49
Approval Holder
/ Type Designation
  • AIRBUS S.A.S.
    • A318
      • A318-111
      • A318-112
      • A318-121
      • A318-122
    • A319
      • A319-111
      • A319-112
      • A319-113
      • A319-114
      • A319-115
      • A319-131
      • A319-132
      • A319-133
    • A320
      • A320-211
      • A320-212
      • A320-214
      • A320-215
      • A320-216
      • A320-231
      • A320-232
      • A320-233
    • A321
      • A321-111
      • A321-112
      • A321-131
      • A321-211
      • A321-212
      • A321-213
      • A321-231
      • A321-232
Revision Not applicable
Correction Not applicable
Supersedure This AD supersedes EASA AD 2012-0214 dated 18 October 2012.
Publication(s) and related information Airbus SB A320-49-1057 Original issue dated 02 June 1999, or Revision 01 dated 28 March 2003. The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD. APIC SB 4500001-49-72 Revision 01 dated 20 November 1998. APIC SB 4500001-49-13 Original Issue dated 24 March 1995, or Revision 01 dated 21 June 1996, or Revision 02 dated 20 November 1998. APIC SB 4500001-49-100 original issue dated 12 May 1999, or Revision 01 dated 24 November 1999.
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. Based on the required actions and the compliance time, EASA have decided to issue a Final AD with Request for Comments, postponing the public consultation process until after publication. 3. Enquiries regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA. E-mail: ADs[at]easa.europa[dot]eu.

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