Number |
2023-0148 |
Issued by |
Europe |
Issue date |
2023-07-19 |
Effective date |
2023-08-02 |
EASA approval number |
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ATA Chapter |
11, 63 |
Approval Holder / Type Designation |
|
Revision |
Not applicable
|
Correction |
Not applicable
|
Supersedure |
This AD supersedes EASA Emergency AD 2019-0152-E dated 28 June 2019.
|
Publication(s) and related information |
AH EC225 Emergency ASB 04A016 Revision 1 dated 28 June 2019, or Revision 2 dated 23 July 2019, or Revision 3 dated 05 August 2019, or Revision 4 dated 19 June 2023.
The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD. |
PAD number |
23-078 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 20 June 2023 as PAD 23-078 for consultation until 18 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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