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ADs [at] easa.europa [dot] eu
|
| Number |
23-030 |
| Issued by |
 Europe |
| Issue date |
2023-03-07 |
| EASA approval number |
|
| Contributor |
EASA Large Aeroplanes Department |
| ATA Chapter |
24 |
Approval Holder
/ Type Designation |
-
ATR
-
ATR42
-
ATR72
-
101
-
102
-
201
-
202
-
211
-
212
-
212A
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
ATR AOM 2021/05 issue 1 dated 19 April 2021, issue 2 dated 03 May 2021, issue 3 dated 11 May 2021, issue 4 dated 16 March 2022 and issue 5 dated 30 November 2022.
ATR OEB 56, issue 3, "Potential temporary loss of all Cockpit Display Systems" dated 24 November 2022.
ATR SB ATR42-24-0062 and SB ATR72-24-1032, both dated 01 March 2023.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| Remarks |
1. This Proposed AD will be closed for consultation on 21 March 2023.
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.
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