Number |
2025-0174R1 |
Issued by |
Europe |
Issue date |
2025-09-22 |
Effective date |
2025-09-29 |
EASA approval number |
|
ATA Chapter |
53 |
Approval Holder / Type Designation |
-
AIRBUS HELICOPTERS DEUTSCHLAND
-
EC135/635
-
EC135 P1
-
EC135 P2
-
EC135 P2+
-
EC135 P3
-
EC135 T1
-
EC135 T2
-
EC135 T2+
-
EC135 T3
-
EC635 P2+
-
EC635 T1
-
EC635 T2+
|
Revision |
This AD revises AD 2025-0174 dated 05 August 2025.
|
Correction |
Not applicable
|
Supersedure |
The original issue of this AD superseded EASA Emergency AD 2013-0289-E dated 06 December 2013.
|
Publication(s) and related information |
AH ASB EC135-53A-029 revision 1 dated 31 July 2025.
AH SB EC135-53-030 original issue dated 26 March 2014, or revision 01 dated 12 May 2014.
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 02 September 2025. 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.
|