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2013-0216 : Nacelles / Pylons – Pylon Lower Spar between Ribs 9 and 10 - Inspection

Number 2013-0216
Issued by Europe  Europe
Issue date 2013-09-17
Effective date 2013-10-01
EASA approval number
ATA Chapter 54
Approval Holder
/ Type Designation
  • AIRBUS S.A.S.
    • A300
      • A300B4-102
      • A300B4-103
      • A300B4-120
      • A300B4-203
      • A300B4-220
      • A300B4-2C
      • A300C4-203
      • A300F4-203
    • A300-600
      • A300B4-620
      • A300B4-622
      • A300B4-622R
      • A300C4-620
    • A310
      • A310-221
      • A310-222
      • A310-322
      • A310-324
      • A310-325
Revision Not applicable
Correction Not applicable
Supersedure This AD supersedes EASA AD 2013-0014 dated 16 January 2013.
Publication(s) and related information AIRBUS SB A300-54-0071 Revision 04 dated 11 April 2013. AIRBUS SB A310-54-2016 Revision 05 dated 05 October 2012. AIRBUS SB A300-54-6011 Revision 03 dated 23 June 2011. AIRBUS SB A300-54-0079 Revision 01 dated 09 July 2002. AIRBUS SB A310-54-2022 Revision 02 dated 09 July 2002. AIRBUS SB A300-54-6019 Revision 02 dated 07 April 2003. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
PAD number 13-119
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 15 August 2013 as PAD 13-119 for consultation until 12 September 2013. No comments were received during the consultation period. 3. Enquiries regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA. E-mail: ADs[at]easa.europa[dot]eu.