Safety Publications Tool
2022-0100 : Fuselage – Belly Fairing Torsion Box – Modification
EASA approval number
EASA Large Aeroplanes Department
/ Type Designation
This AD supersedes EASA AD 2019-0222 dated 06 September 2019.
Publication(s) and related information
Airbus SB A380-53-8153 original issue dated 24 April 2019, or Revision 01 dated 11 February 2022. The use of later approved revisions of the above-mentioned document 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. This AD was posted on 04 May 2022 as PAD 22-051 for consultation until 01 June 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_0100.pdf (195 kb)
EASA_PAD_22_051.zip (365 kb)
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