Safety Publications Tool
2022-0197 : Fuel – Fuel Pump – Inspection / Modification
EASA approval number
EASA Large Aeroplanes Department
/ Type Designation
This AD supersedes EASA AD 2020-0283 dated 17 December 2020, including its correction dated 24 December 2020.
Publication(s) and related information
Airbus AOT A28L006-17 original issue dated 03 November 2017, or Revision 01 dated 16 November 2017, or Revision 02 dated 08 February 2018, or Revision 03 dated 28 May 2019, or Revision 04 dated 04 September 2019, or Revision 05 dated 02 March 2020, or Revision 06 dated 17 November 2020. Airbus SB A330-28-3132 original issue dated 06 March 2019, or Revision 01 dated 05 December 2019, or Revision 02 dated 09 July 2020, or Revision 03 dated 03 March 2021, or Revision 04 dated 13 May 2022. Airbus SB A340-28-4142 original issue dated 06 March 2019, or Revision 01 dated 28 April 2020, or Revision 02 dated 03 March 2021, or Revision 03 dated 13 May 2022. Airbus SB A340-28-5062 original issue dated 06 March 2019, or Revision 01 dated 28 April 2020, or Revision 02 dated 03 March 2021, or Revision 03 dated 13 May 2022. Eaton Aerospace Ltd SB 8810-28-06 Revision 2 dated 01 March 2019. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 09 August 2022 as PAD 22-107 for consultation until 06 September 2022. The Comment Response Documents 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. 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.
EASA_AD_2022_0197.pdf (228 kb)
EASA_PAD_22_107.zip (650 kb)
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