Safety Publications Tool

2026-0209 : Wings – Main Landing Gear Attachment / Rib 5 Forward Lug – Inspection(s)

Number 2026-0209
Issued by Europe  Europe
Issue date 2026-11-03
Effective date 2026-11-17
EASA approval number
ATA Chapter 57
Approval Holder
/ Type Designation
  • AIRBUS S.A.S.
    • A300-600
      • A300B4-603
      • A300B4-605R
      • A300B4-622
      • A300B4-622R
      • A300C4-605R variant F
      • A300F4-605R
      • A300F4-622R
    • A300-600ST (Beluga)
      • A300F4-608ST
    • A310
      • A310-203
      • A310-222
      • A310-304
      • A310-308
      • A310-322
      • A310-324
      • A310-325
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information Airbus SB A300-57-6126 original issue dated 10 July 2026. Airbus SB A310-57-2109 original issue dated 16 July 2026. Airbus SB A300-57-9038 original issue dated 16 July 2026. Airbus SB A300-57-6106 Rev 1 (original issue) dated 22 May 2007, or Rev 2 dated 18 June 2010, or Rev 3 dated 26 January 2012, or Rev 4 dated 24 July 2014. Airbus SB A310-57-2090 Rev 1 (original issue) dated 22 May 2007, or Rev 2 dated 18 June 2010, or Rev 3 dated 23 January 2012, or Rev 4 dated 24 July 2014. Airbus SB A310-57-2101 original issue dated 13 January 2012, or Rev 1 dated 21 September 2017. Airbus SB A300-57-6112 original issue dated 13 January 2012. Airbus SB A300-57-9024 original issue dated 13 January 2012. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
PAD number 26-109
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. The original issue of this AD was posted on 18 September 2026 as PAD 26-109 for consultation until 16 October 2026. The Comment Response Document can be found in the EASA Safety Publications Tool, in the compressed (zipped) file attached to the record for this AD. 3. Enquiries regarding this AD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu. 4. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on a product, part or appliance not affected by this AD, can be reported to the EU aviation safety reporting system. This may include reporting on the same or similar components, other than those covered by the design to which this AD applies, if the same unsafe condition can exist or may develop on an aircraft with those components installed. Such components may be installed under an FAA Parts Manufacturer Approval (PMA), Supplemental Type Certificate (STC) or other modification.