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2016-0229 : Wing – Damage Limitations Changes in Structural Repair Manual – Inspection / Repair

Number 2016-0229
Issued by Europe  Europe
Issue date 2016-11-15
Effective date 2016-11-29
EASA approval number
ATA Chapter 57
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
    • A300-600ST (Beluga)
      • A300F4-608ST
    • A310
      • A310-203
      • A310-203C
      • A310-204
      • A310-221
      • 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 A300-57-0256 original issue dated 03 August 2015. Airbus SB A310-57-2102 original issue dated 03 August 2015. Airbus SB A300-57-6114 original issue dated 03 August 2015. Airbus SB A300-57-9027 original issue dated 03 August 2015. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
PAD number 16-117
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 02 August 2016 as PAD 16-117 for consultation until 30 August 2016. The Comment Response Document can be found at https://ad.easa.europa.eu. 3. Enquiries regarding this AD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.