Safety Publications Tool
2022-0096R1 : Aircraft Flight Manual / Section Limitations – Amendment / Auto Flight – New Flight Guidance Standard – Modification
EASA approval number
EASA Large Aeroplanes Department
/ Type Designation
This AD revises EASA AD 2022-0096 dated 31 May 2022.
This original issue of this AD supersedes EASA AD 2020-0118 dated 22 May 2020.
Publication(s) and related information
Airbus A319 AFM TR 784 issue 1, EASA approval date 30 April 2020. Airbus A319/A320/A321 AFM TR 785 issue 1, EASA approval date 30 April 2020. Airbus SB A320-22-1819 original issue dated 07 March 2022. Airbus SB A320-22-1820 original issue dated 23 May 2022. Airbus SB A320-22-1821 original issue dated 26 November 2021, or Revision 01 dated 24 March 2022. Airbus SB A320-22-1822 original issue dated 14 February 2022. Airbus SB A320-22-1823 original issue dated 30 March 2022. Airbus SB A320-22-1824 original issue dated 18 March 2022. Airbus SB A320-22-1827 original issue dated 07 February 2022. Airbus SB A320-22-1828 original issue dated 22 December 2021. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
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 28 April 2022 as PAD 22-049 for consultation until 26 May 2022. No comments were received during the consultation period. 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.
EASA_AD_2022-0096R1.pdf (233 kb)
EASA_PAD_22_049.zip (1 mb)
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