| Number |
2022-0191R1 |
| Issued by |
 Europe |
| Issue date |
2025-12-09 |
| Effective date |
2025-12-16 |
| EASA approval number |
|
| ATA Chapter |
65 |
Approval Holder
/ Type Designation |
|
| Revision |
This AD revises EASA AD 2022-0191 dated 15 September 2022.
|
| Correction |
Not applicable
|
| Supersedure |
The original issue of this AD superseded EASA AD 2020-0171 dated 28 July 2020.
|
| Publication(s) and related information |
AH SA 330 Emergency ASB 05.96 Revision 1 dated 24 July 2020, or Revision 2 dated 25 July 2022.
AH SB SA 330-65.127 original issue dated 25 June 2018.
AH ASB SA 330-65.137 original issue dated 25 July 2022, or Revision 1 dated 09 December 2025.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD. |
| PAD number |
22-110 |
| Remarks |
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 16 August 2022 as PAD 22-110 for consultation until 13 September
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.
|
