Safety Publications Tool

2021-0150 : SUPERSEDED BY EASA AD 2022-0028

Number 2021-0150
Issued by Europe  Europe
Issue date 2021-06-25
Effective date 2021-06-28
EASA approval number
ATA Chapter 34
Approval Holder
/ Type Designation
  • AIRBUS S.A.S.
    • A319
      • A319-151N
      • A319-153N
      • A319-171N
    • A320
      • A320-251N
      • A320-252N
      • A320-253N
      • A320-271N
      • A320-272N
      • A320-273N
    • A321
      • A321-251N
      • A321-251NX
      • A321-252N
      • A321-252NX
      • A321-253N
      • A321-253NX
      • A321-271N
      • A321-271NX
      • A321-272N
      • A321-272NX
Revision Not applicable
Correction This AD is republished to correct an error in the Ref. Publications.
Supersedure None
Publication(s) and related information Airbus A319/A320/A321 AFM TR 787 Issue 1, EASA approval date 17 June 2021. Airbus A318/A319/A320/A321 MMEL item 34-23-02B update, ident MI-34-23-00008619.0009001, dated 18 June 2021. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. Based on the required actions and the compliance time, EASA have decided to issue a Final AD with Request for Comments, postponing the public consultation process until after publication. 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.