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  Safety Publications Tool

2016-0212 : Fuselage – Central Vertical Strut at Frame 65 – Modification

Number 2016-0212
Issued by Europe  Europe
Issue date 2016-10-25
Effective date 2016-11-08
EASA approval number
ATA Chapter 53
Approval Holder
/ Type Designation
  • AIRBUS S.A.S.
    • A318
      • A318-111
      • A318-112
      • A318-121
      • A318-122
    • A319
      • A319-111
      • A319-112
      • A319-113
      • A319-114
      • A319-115
      • A319-131
      • A319-132
      • A319-133
    • A320
      • A320-211
      • A320-212
      • A320-214
      • A320-215
      • A320-216
      • A320-231
      • A320-232
      • A320-233
    • A321
      • A321-111
      • A321-112
      • A321-131
      • A321-211
      • A321-212
      • A321-213
      • A321-231
      • A321-232
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information Airbus SB A320-53-1262 Revision 01 dated 29 July 2016. Airbus SB A320-53-1333 original issue dated 29 July 2016. Airbus SB A320-53-1334 original issue dated 29 July 2016. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
PAD number 15-156R1
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 18 December 2015 as PAD 15-156 for consultation until 15 January 2016, and republished on 29 September 2016 as PAD 15-156R1 for additional consultation until 13 October 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.