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2017-0098R1 : Fuselage – Potable Water and Waste Water Service Panels – Reinforcement

Number 2017-0098R1
Issued by Europe  Europe
Issue date 2025-04-07
Effective date 2025-04-14
EASA approval number
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 EASA AD 2017-0098 dated 07 June 2017.
Correction Not applicable
Supersedure The original issue of this AD superseded EASA AD 2014-0081 dated 31 March 2014.
Publication(s) and related information Airbus SB A320-53-1267 original issue dated 24 June 2013, or Rev. 01 dated 02 October 2013, or Rev. 02 dated 19 May 2014, or Rev. 03 dated 26 November 2015, or Rev. 04 dated 01 February 2016 or Rev. 05 dated 29 November 2016, or Rev. 06 dated 17 May 2019. Airbus SB A320-53-1272 original issue dated 10 January 2013, or Rev. 01 dated 06 August 2013, or Rev. 02 dated 19 May 2014, or Rev. 03 dated 26 November 2015, or Rev. 04 dated 29 November 2016, or Rev. 05 dated 17 May 2019.
PAD number 17-035
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 20 March 2017 as PAD 17-035 for consultation until 17 April 2017. The Comment Response Document can be found at https://ad.easa.europa.eu 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. This may include reporting on the same or similar components, other than those covered by the design to which this AD applies, if the same unsafe condition can exist or may develop on an aircraft with those components installed. Such components may be installed under an FAA Parts Manufacturer Approval (PMA), Supplemental Type Certificate (STC) or other modification.