Number |
2025-0171R1 |
Issued by |
Europe |
Issue date |
2025-08-15 |
Effective date |
2025-08-20 |
EASA approval number |
|
ATA Chapter |
72 |
Approval Holder / Type Designation |
-
CFM INTERNATIONAL
-
LEAP-1A/-1C
-
LEAP-1A23
-
LEAP-1A24
-
LEAP-1A24E1
-
LEAP-1A26
-
LEAP-1A26CJ
-
LEAP-1A26E1
-
LEAP-1A29
-
LEAP-1A29CJ
-
LEAP-1A30
-
LEAP-1A32
-
LEAP-1A33
-
LEAP-1A33B2
-
LEAP-1A35A
|
Revision |
This AD revises EASA AD 2025-0171 dated 04 August 2025.
|
Correction |
Not applicable
|
Supersedure |
None
|
Publication(s) and related information |
CFM SB LEAP-1A-72-00-0485-01A-930A-D Issue 001 dated 2 July 2022, Issue 002 dated 16 April 2025 and Issue 003 dated 30 July 2025.
CFM SB LEAP-1A-72-00-0461-01A-930A-D Issue 001 dated 10 December 2021, Issue 002 dated 21 December 2021 and Issue 003 dated 13 July 2022.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
PAD number |
25-106 |
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 17 July 2025 as PAD 25-106 for consultation until 31 July 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.
|