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2018-0007R1 : Flight Controls – Elevator Aileron Computers – Replacement / Software Update

Number 2018-0007R1
Issued by Europe  Europe
Issue date 2018-01-19
Effective date 2018-01-24
EASA approval number
ATA Chapter 27
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
      • A320-251N
      • A320-271N
    • A321
      • A321-111
      • A321-112
      • A321-131
      • A321-211
      • A321-212
      • A321-213
      • A321-231
      • A321-232
Revision This AD revises EASA AD 2018-0007 dated 10 January 2018.
Correction Not applicable
Supersedure The original issue of this AD superseded EASA AD 2015-0088R1 dated 02 June 2015.
Publication(s) and related information Airbus SB A320-27-1243 original issue dated 17 March 2015, or Revision 01 dated 14 December 2015. Airbus SB A320-27-1244 original issue dated 05 March 2015. Airbus SB A320-27-1251 original issue dated 26 May 2016, or Revision 01 dated 01 January 2017. Airbus SB A320-27-1255 original issue dated 26 May 2016, or Revision 01 dated 01 January 2017. Airbus SB A320-27-1263 original issue dated 28 April 2017. Airbus SB A320-27-1264 original issue dated 28 April 2017. Airbus SB A320-27-1267 original issue dated 27 September 2017. Airbus SB A320-27-1268 original issue dated 27 September 2017. Airbus SB A320-27-1269 original issue dated 27 September 2017. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
PAD number 17-158
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 21 November 2017 as PAD 17-158 for consultation until 19 December 2017. 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.