Safety Publications Tool

2019-0017 : Flight Controls / Stabilizers – Rudder Servo Control – Inspection

Number 2019-0017
Issued by Europe  Europe
Issue date 2019-01-29
Effective date 2019-02-12
EASA approval number
ATA Chapter 27, 55
Approval Holder
/ Type Designation
  • AIRBUS S.A.S.
    • A300
      • A300B4-102
      • A300B4-103
      • A300B4-120
      • A300B4-203
      • A300B4-220
      • A300B4-2C
      • A300C4-203
      • A300F4-203
    • A300-600
      • A300B4-601
      • A300B4-603
      • A300B4-605R
      • A300B4-620
      • A300B4-622
      • A300B4-622R
      • A300C4-605R variant F
      • A300C4-620
      • A300F4-605R
      • A300F4-622R
    • A300-600ST (Beluga)
      • A300F4-608ST
    • A310
      • A310-203
      • A310-203C
      • A310-204
      • A310-221
      • A310-222
      • A310-304
      • A310-308
      • A310-322
      • A310-324
      • A310-325
Revision Not applicable
Correction Not applicable
Supersedure This AD supersedes DGAC France AD F-2004-063 dated 12 May 2004, and AD F-2004-092 (EASA approval 2004-6368) dated 23 June 2004.
Publication(s) and related information Airbus SB A300-27-0188 Revision 05 dated 16 April 2004, or Revision 06 dated 23 January 2006, or Revision 07 dated 06 May 2010. Airbus SB A310-27-2082 Revision 05 dated 16 April 2004, or Revision 06 dated 23 December 2004, or Revision 07 dated 23 January 2006, or Revision 08 dated 06 May 2010. Airbus SB A300-27-6036 Revision 08 dated 16 April 2004, or Revision 09 dated 23 January 2006, or Revision 10 dated 01 August 2007, or Revision 11 dated 01 October 2007, or Revision 12 dated 06 May 2010. Airbus SB A300-27-9009 original issue dated 16 April 2004, or Revision 01 dated 23 January 2006, or Revision 02 dated 11 June 2010. Airbus SB A300-55-0044 Revision 04 dated 14 December 2017. Airbus SB A300-55-6023 Revision 08 dated 14 December 2017. Airbus SB A310-55-2026 Revision 04 dated 14 December 2017. Airbus SB A300-55-9007 Revision 01 dated 04 January 2018. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
PAD number 18-165
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 03 December 2018 as PAD 18-165 for consultation until 31 December 2018. 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. 4. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on a product, part or appliance not affected by this AD, can be reported to the EU aviation safety reporting system.