Safety Publications Tool
22-002 : Aircraft Flight Manual / Section Normal Procedures – Amendment / Navigation – Master Minimum Equipment List – Integrated Standby Instrument System – Amendment / Flight Controls – Elevator Aileron Computer System - Modification
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EASA approval number
EASA Large Aeroplanes Department
/ Type Designation
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.
1. This Proposed AD will be closed for consultation on 09 February 2022. 2. Enquiries regarding this PAD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu. 3. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this PAD, and which may occur, or have occurred on a product, part or appliance not affected by this PAD, 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 PAD 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_PAD_22_002.pdf (210 kb)
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