| Publication(s) and related information |
PAI P.180 SB 80-0492 original Issue dated 30 November 2022, Revision 1 dated 20 December 2022, Revision 2 dated 15 May 2023, or Revision 3 dated 12 June 2023.
PAI SRM 180-MAN-0250-01106 Revision D0 dated 18 November 2023.
PAI TR no. 030 to SRM 180-MAN-0250-01106 Revision D0 dated 06 April 2023.
PAI TR no. 031 to SRM 180-MAN-0250-01106 Revision D0 dated 29 May 2023.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD. |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. Based on the required actions and the compliance time, EASA have decided to issue a Final AD with Request for Comments, postponing the public consultation process until after publication.
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.
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