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2019-0197R1 : Fuel – Fuel Level Sensor Support Bracket – Replacement

Number 2019-0197R1
Issued by Europe  Europe
Issue date 2020-10-14
Effective date 2020-10-21
EASA approval number
Contributor EASA Large Aeroplanes Department
ATA Chapter 57
Approval Holder
/ Type Designation
  • AIRBUS
    • A318
      • A318-112
    • 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
      • A320-251N
      • A320-271N
Revision This AD revises EASA AD 2019-0197 dated 11 July 2019.
Correction Not applicable
Supersedure None
Publication(s) and related information Airbus SB A320-28-1216 Revision 01 dated 19 June 2018. Airbus SB A320-28-1238 Revision 01 dated 15 September 2017. Airbus SB A320-28-1239 Revision 01 dated 15 September 2017. The use of later approved revisions of the above-referenced documents is acceptable for compliance with the requirements of this AD.
PAD number 19-108
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 17 June 2019 as PAD 19-108 for consultation until 15 July 2019. 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 Programming and Continued Airworthiness 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.