Safety Publications Tool

2012-0132R1 : Fuselage – Forward Fuselage Frame (FR) 24 Circumferential Junction – Inspection / Repair

Number 2012-0132R1
Issued by Europe  Europe
Issue date 2013-03-01
Effective date 2013-03-01
EASA approval number
ATA Chapter 53
Approval Holder
/ Type Designation
  • AIRBUS S.A.S.
    • A318
      • A318-112
    • A319
      • A319-111
      • A319-112
      • A319-115
      • A319-132
      • A319-133
Revision This AD revises EASA AD 2012-0132 dated 18 July 2012.
Correction Not applicable
Supersedure None.
Publication(s) and related information Airbus SB A320-53-1242 original issue, dated 22 May 2012. Airbus SB A320-00-1219 original issue dated 09 November 2010, Revision 01 dated 08 December 2010, Revision 02 dated 06 September 2011 or Revision 03 dated 28 March 2012. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
PAD number 12-059
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 05 June 2012 as PAD 12-059 for consultation until 03 July 2012. The Comment Response Document can be found at https://ad.easa.europa.eu. 3. Enquiries regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA. E-mail ADs[at]easa.europa.eu.