| Number |
2024-0222 |
| Issued by |
 Europe |
| Issue date |
2025-01-06 |
| Effective date |
2024-12-06 |
| EASA approval number |
|
| ATA Chapter |
25 |
Approval Holder
/ Type Designation |
-
AEROLITE AG
-
EASA STC 10016765
-
EASA STC 10016793
-
EASA STC 10017157
-
EASA STC 10030992
-
EASA STC 10039944
-
EASA STC 10075050
-
FOCA STC 25-20-95
-
LBA STC RC 1240
-
STC EASA.IM.R.S.01096
-
STC EASA.IM.R.S.01143
-
STC EASA.R.S.01265
-
AIRBUS HELICOPTERS DEUTSCHLAND
|
| Revision |
Not applicable
|
| Correction |
This AD is republished to correct typographical errors in the 'Ref. Publications' section.
|
| Supersedure |
None
|
| Publication(s) and related information |
Aerolite AG ASB 17-012 original issue dated 24 August 2017, Revision A dated 15 May 2023, Revision B dated 11 August 2023, Revision C dated 09 May 2024, or Revision D dated 18 November 2024.
Aerolite AG ASB 17-013 original issue dated 09 January 2018, Revision A dated 15 May 2023, Revision B dated 11 August 2023, or Revision C dated 18 November 2024.
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, this AD was posted on 22 November 2024 as Final AD with Request for Comments, postponing the public consultation process until 03 January 2025. The Comment Response Document can be found in the EASA Safety Publications Tool, in the 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.
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