| Number |
2024-0064R1 |
| Issued by |
 Europe |
| Issue date |
2024-03-18 |
| Effective date |
2024-03-21 |
| EASA approval number |
|
| ATA Chapter |
55 |
Approval Holder
/ Type Designation |
|
| Revision |
This AD revises EASA AD 2024-0064 dated 14 March 2024.
|
| Correction |
Not applicable
|
| Supersedure |
The original issue of this AD superseded EASA AD 2021-0178R2 dated 30 January 2023 and EASA AD 2022-0099 dated 01 June 2022.
|
| Publication(s) and related information |
AH EC175 Emergency ASB 05A020 original issue dated 27 March 2018, or Revision 1 dated 03 June 2019, or Revision 2 dated 25 July 2019, or Revision 3 dated 10 May 2021, or Revision 4 dated 20 December 2021, or Revision 5 dated 28 February 2022, or Revision 6 dated 30 May 2022.
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, or Revision 4 dated 11 May 2023.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD. |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. Based on the required actions and the compliance time, EASA have decided to issue a Final AD with Request for Comments, postponing the public consultation process until after publication.
All interested persons may send their comments, referencing the AD Number, to the E-mail
address specified in below Remark 3, prior to 11 April 2024. Only if any comment is received
during the consultation period, a Comment Response Document will be published in the EASA
Safety Publications Tool, in a compressed ('zipped') file, attached to the record for this AD.
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.
|
