Safety Publications Tool

2012-0198R1 : Fuel System – Centre Tank Fuel Pump Control Circuit – Modification

Number 2012-0198R1
Issued by Europe  Europe
Issue date 2014-10-10
Effective date 2014-10-10
EASA approval number
ATA Chapter 28
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
Revision This AD revises EASA AD 2012-0198 dated 26 September 2012, which superseded EASA AD 2012-0133 dated 18 July 2012.
Correction Not applicable
Supersedure None
Publication(s) and related information Airbus SB A320-28-1188 original issue dated 23 March 2012, or Revision 01 dated 31 January 2013, or Revision 02 dated 27 November 2013, or Revision 03 dated 26 June 2014. The use of later approved revisions of this document is acceptable for compliance with the requirements of the AD.
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. Based on the required actions and the compliance time, EASA have decided to issue a Final AD with Request for Comments, postponing the public consultation process until after publication. 3. Enquiries regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA. E-mail ADs[at]easa.europa[dot]eu.