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F-2004-189R1 : Fuselage - Keel Beam Main Landing Gear Door Actuator Fitting - Inspection/Modification

Number F-2004-189R1
Issued by Europe  Europe
Issue date 2005-01-05
Effective date 2005-01-15
EASA approval number 2004-12555
ATA Chapter 53
Approval Holder
/ Type Designation
  • AIRBUS S.A.S.
    • 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 DGAC AD F-2004-189. Revision 1 aims at clarifying paragraphs A.1.2.1 et B.1 as well as modifying the list of aircraft involved in paragraph B.1.
Correction N/A
Supersedure This AD supersedes DGAC AD F-2004-189, EASA approval number 2004-11504, which superseded DGAC AD 2000-521-160, (also) cancelled by its Revision 1.
Publication(s) and related information AIRBUS SB A320-53A1135 Revision 3, SB A320-53-1140 Revision 2, SB A320-53-1148, SB A320-53-1149, SB A320-53-1160, SB A320-53-1158, or later approved revisions of these documents.
Remarks Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail: ADs [at] easa.europa [dot] eu