| Number |
2023-0147R1 |
| Issued by |
 Europe |
| Issue date |
2025-03-12 |
| Effective date |
2025-03-19 |
| EASA approval number |
|
| ATA Chapter |
05, 53 |
Approval Holder
/ Type Designation |
|
| Revision |
This AD revises EASA AD 2023-0147 dated 19 July 2023.
|
| Correction |
Not applicable
|
| Supersedure |
The original issue of this AD superseded EASA AD 2022-0021 dated 01 February 2022.
|
| Publication(s) and related information |
AH AS332 Emergency ASB 01.00.86 original issue dated 27 July 2017, or Revision 1 dated 25 August 2017, or Revision 2 dated 02 March 2020, or Revision 3 dated 19 August 2021, or Revision 4 dated 06 January 2022.
AH EC225 Emergency ASB 04A013 original issue dated 27 July 2017, or Revision 1 dated 25 August 2017, or Revision 2 dated 02 March 2020, or Revision 3 dated 19 August 2021, or Revision 4 dated 06 January 2022.
AH SB AS332-53.02.03 original issue dated 19 August 2021, or AH ASB AS332-53.02.03 Revision 1 dated 06 January 2022, or Revision 2 dated 15 June 2023.
AH SB EC225-53-065 original issue dated 19 August 2021, or AH ASB EC225-53A065 Revision 1 dated 06 January 2022, or Revision 2 dated 05 May 2022, or Revision 3 dated 15 June 2023, or Revision 4 dated 26 May 2024, or Revision 5 dated 05 December 2024.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
23-077 |
| 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 June 2023 as PAD 23-077 for consultation until 14 July 2023. 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.
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