Safety Publications Tool

2012-0175R2 : Flight Controls – Trimmable Horizontal Stabilizer Actuator Ballscrew Lower Splines – Inspection / Replacement

Number 2012-0175R2
Issued by Europe  Europe
Issue date 2016-02-02
Effective date 2016-02-04
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
    • A321
      • A321-111
      • A321-112
      • A321-131
      • A321-211
      • A321-212
      • A321-213
      • A321-231
      • A321-232
Revision This AD revises EASA AD 2012-0175R1 dated 07 January 2014.
Correction Not applicable
Supersedure None
Publication(s) and related information Airbus SB A320-27-1214 original issue dated 23 February 2012. Airbus SB A320-27-1222 original issue dated 17 July 2015. Goodrich SB 47145-27-16 original issue dated 07 November 2011. UTAS SB 47145-27-18 original issue dated 31 March 2015. UTAS SB 47145-27-20 original issue dated 16 July 2015. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
PAD number 12-057
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 04 June 2012 as PAD 12-057 for consultation until 18 June 2012. 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.