| Number |
2021-0178R2 |
| Issued by |
 Europe |
| Issue date |
2023-01-30 |
| Effective date |
2023-01-30 |
| EASA approval number |
|
| ATA Chapter |
55 |
Approval Holder
/ Type Designation |
|
| Revision |
This AD revises EASA AD 2021-0178R1 dated 08 June 2022.
|
| Correction |
Not applicable
|
| Supersedure |
The original issue of this AD superseded EASA AD 2019-0148R1 dated 27 April 2021.
|
| Publication(s) and related information |
AH EC175 Emergency ASB 05A030 original issue dated 20 June 2019, or Revision 1 dated 10 May 2021, or Revision 2 dated 24 January 2022.
AH ASB EC175-55A009 original issue dated 11 May 2021, or Revision 1 dated 30 September 2021, or Revision 2 dated 17 October 2022, or Revision 3 dated 10 January 2023.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
21-088 |
| 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 2021 as PAD 21-088 for consultation until 14 July 2021. 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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