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2012-0229 : Fuselage – Frame Base Fitting between Frames 41 and 46 Area 2 – Inspection

Number 2012-0229
Issued by Europe  Europe
Issue date 2012-10-31
Effective date 2012-11-14
EASA approval number
ATA Chapter 53
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
      • A300B4-601
      • A300B4-603
      • A300B4-605R
      • A300B4-620
      • A300B4-622
      • A300B4-622R
      • A300C4-605R variant F
      • A300C4-620
      • A300F4-605R
      • A300F4-622R
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information Airbus Alert Operators Transmission (AOT) A53W001-12 dated 04 July 2012. Airbus Service Bulletins: A300-53-0337 Revision 01 dated 17 March 2003 or earlier revision. A300-53-6111 Revision 04 dated 25 August 2011 or earlier revisions.
PAD number 12-082
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 20 July 2012 as PAD 12-082 for consultation until 17 August 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[dot]eu.