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2014-0018R1 : [Correction] Hydraulic Power – Hydraulic Accumulator – Inspection / Replacement / Placard Installation

Number 2014-0018R1
Issued by Europe  Europe
Issue date 2014-01-23
Effective date 2014-01-30
EASA approval number
ATA Chapter 29
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 This AD revises EASA AD 2014-0018 dated 16 January 2014.
Correction This AD is republished to correct and clarify paragraph (3).
Supersedure The original issue of this AD superseded EASA AD 2011-0006 dated 17 January 2011.
Publication(s) and related information Airbus SB A300-29-0126 Revision 01 dated 12 October 2010. Airbus SB A300-29-0127 Revision 01 dated 08 July 2013. Airbus SB A310-29-2099 original issue dated 12 August 2010. Airbus SB A310-29-2100 Revision 01 dated 03 July 2013. Airbus SB A300-29-6063 original issue dated 12 August 2010. Airbus SB A300-29-6064 Revision 01 dated 08 July 2013. Airbus SB A300-29-9012 original issue dated 12 August 2010. Airbus SB A300-29-9013 Revision 01 dated 08 July 2013. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
PAD number 13-118R1
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 15 August 2013 as PAD 13-118 for consultation until 12 September 2013 and republished on 23 September as PAD 13-118R1 for consultation until 07 October 2013. The Comment Response Documents can be found at https://ad.easa.europa.eu. 3. Enquiries regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA. E-mail: ADs[at]easa.europa.eu.