Safety Publications Tool

2020-0104R1 : Oxygen – Oxygen Supply Solenoid Valve – Inspection / Replacement

Number 2020-0104R1
Issued by Europe  Europe
Issue date 2021-01-28
Effective date 2021-02-04
EASA approval number
Contributor EASA Large Aeroplanes Department
ATA Chapter 35
Approval Holder
/ Type Designation
  • AIRBUS
    • A318
      • A318-111
      • A318-112
      • A318-121
      • A318-122
    • 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 2020-0104 dated 07 May 2020.
Correction Not applicable
Supersedure None
Publication(s) and related information Airbus SB A320-35-1096 original issue dated 18 September 2019. The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD. Zodiac Aerospace Services SB DVE90-35-348 Revision 1 dated 04 October 2019 and Revision 02 dated 08 January 2020.
PAD number 20-009
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 January 2020 as PAD 20-009 for consultation until 14 February 2020. 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.