Safety Publications Tool

2022-0028 : Aircraft Flight Manual / Section Normal Procedures – Amendment / Navigation – Master Minimum Equipment List – Integrated Standby Instrument System – Amendment / Flight Controls – Elevator Aileron Computer System - Modification

Number 2022-0028
Issued by Europe  Europe
Issue date 2022-02-22
Effective date 2022-03-08
EASA approval number
ATA Chapter 27, 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 Not applicable
Supersedure This AD supersedes EASA AD 2021-0150 dated 21 June 2021, including its correction dated 25 June 2021.
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. Airbus SB A320-27-1288 original issue dated 15 October 2021. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
PAD number 22-002
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 12 January 2022 as PAD 22-002 for consultation until 09 February 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.