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2013-0136R1 : Nacelles/Pylons – Pylon Side Panels at Rib 8 – Inspection

Number 2013-0136R1
Issued by Europe  Europe
Issue date 2013-07-30
Effective date 2013-08-13
EASA approval number
ATA Chapter 54
Approval Holder
/ Type Designation
  • AIRBUS S.A.S.
    • A300
      • A300B4-103
      • A300B4-120
      • A300B4-203
      • A300B4-2C
      • A300F4-203
    • A300-600
      • A300B4-601
      • A300B4-603
      • A300B4-605R
      • A300B4-620
      • A300B4-622
      • A300B4-622R
      • A300C4-620
    • A310
      • A310-203
      • A310-203C
      • A310-204
      • A310-221
      • A310-222
      • A310-304
      • A310-308
      • A310-322
      • A310-324
      • A310-325
Revision This AD revise EASA AD 2013-0136 dated 01 October 2008.
Correction Not applicable
Supersedure This AD supersedes EASA AD 2008-0181 dated 01 October 2008.
Publication(s) and related information Airbus SB A300-54-0075 Revision 03 dated 25 March 2013. Airbus SB A310-54-2018 Revision 03 dated 25 March 2013. Airbus SB A300-54-6015 Revision 03 dated 25 March 2013. Airbus SB A300-54-0081 original issue dated 23 May 1995. Airbus SB A310-54-2024 original issue dated 23 May 1995. Airbus SB A300-54-6021 original issue dated 11 August 1993, or Revision 01 dated 16 November 2007, or Revision 02 dated 21 May 2008. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
PAD number 13-063R1
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 30 April 2013 as PAD 13-063 and republished as PAD 13-063R1 for additional consultation until 28 May 2013. No comments were received during consultation period. 3. Enquiries regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA. E-mail: ADs[at]easa.europa.eu.