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2013-0203 : Fuselage – Frame 47 Splice Plate Butt Joint Crossing Area – Inspection / Repair

Number 2013-0203
Issued by Europe  Europe
Issue date 2013-09-06
Effective date 2013-09-20
EASA approval number
ATA Chapter 53
Approval Holder
/ Type Designation
  • AIRBUS S.A.S.
    • A320
      • A320-211
      • A320-212
      • A320-214
      • A320-215
      • A320-216
      • A320-231
      • A320-232
      • A320-233
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information Airbus SB A320-53-1260 original issue, dated 19 December 2012. Airbus SB A320-53-1271 original issue, dated 18 December 2012. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
PAD number 13-091
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 02 July 2013 as PAD 13-091 for consultation until 30 July 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.