| Number |
2023-0191 |
| Issued by |
 Europe |
| Issue date |
2023-11-02 |
| Effective date |
2023-11-16 |
| EASA approval number |
|
| ATA Chapter |
31 |
Approval Holder
/ Type Designation |
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2023-0134 dated 05 July 2023.
|
| Publication(s) and related information |
ATR AOM 2020/13 Issue 1 dated 28 September 2020, Issue 2 dated 14 October 2020, Issue 3 dated 09 November 2020, or Issue 4 dated 28 January 2021.
ATR SB ATR42-27-0113 original issue dated 09 December 2020, or Revision 01 dated 10 March
2021.
ATR SB ATR42-31-0121 original issue dated 12 May 2023, or Revision 01 dated 24 July 2023, or Revision 02 dated 13 September 2023.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD. |
| PAD number |
23-115 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. This AD was posted on 18 October 2023 as PAD 23-115 for consultation until 01 November
2023. No comments were received during the consultation process.
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.
|
