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2016-0132 : [Correction] Auto Flight / Instruments – Stop Rudder Input Warning – Installation / Activation

Number 2016-0132
Issued by Europe  Europe
Issue date 2016-07-20
Effective date 2016-07-19
EASA approval number
ATA Chapter 22, 31
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 This AD is republished to remove a typographical error in Appendix 1.
Supersedure This AD supersedes EASA AD 2014-0217R1 dated 26 February 2015.
Publication(s) and related information Airbus SB A320-22-1375 original issue, dated 15 January 2014. Airbus SB A320-22-1427 original issue, dated 25 January 2013. Airbus SB A320-22-1447 original issue, dated 18 October 2013. Airbus SB A320-22-1461 original issue, dated 31 October 2013. Airbus SB A320-22-1480 original issue, dated 09 July 2014, or Revision 01, dated 06 February 2015, or Revision 02, dated 30 March 2015, or Revision 03, dated 13 October 2015. Airbus SB A320-22-1454 original issue, dated 12 February 2014. Airbus SB A320-22-1502 original issue, dated 14 November 2014. Airbus SB A320-22-1516 original issue, dated 17 July 2015. Airbus SB A320-22-1539 original issue, dated 08 December 2015, or Revision 01, dated 24 February 2016. Airbus SB A320-22-1553 original issue, dated 21 March 2016. Airbus SB A320-22-1554 original issue, dated 19 April 2016. Airbus SB A320-31-1414 original issue, dated 19 December 2012. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
PAD number 16-066
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 10 May 2016 as PAD 16-066 for consultation until 07 June 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.