Safety Publications Tool
22-127 : Electric and Electronic Common Installation – Cockpit Panel Bracket – Inspection
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EASA approval number
EASA Large Aeroplanes Department
/ Type Designation
This AD supersedes EASA AD 2018-0131 dated 19 June 2018.
Publication(s) and related information
Airbus SB A320-92-1087 original issue dated 28 March 2011, or Revision 01 dated 17 May 2011, or Revision 02 dated 25 November 2014, or Revision 03 dated 31 July 2017, or Revision 04 dated 16 May 2022. Airbus SB A320-92-1119 original issue dated 28 July 2017, or Revision 01 dated 05 August 2019, or Revision 02 dated 16 May 2022. 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 20 October 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_127.pdf (199 kb)
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