| Number |
2025-0003 |
| Issued by |
 Europe |
| Issue date |
2025-01-07 |
| Effective date |
2025-01-21 |
| EASA approval number |
|
| Contributor |
EASA Environment & Propulsion Systems Department |
| 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
-
LEAP-1C28
-
LEAP-1C30
-
LEAP-1C30B1
-
LEAP-1B
-
LEAP-1B21
-
LEAP-1B23
-
LEAP-1B25
-
LEAP-1B27
-
LEAP-1B28
-
LEAP-1B28B1
-
LEAP-1B28B2
-
LEAP-1B28B2C
-
LEAP-1B28B3
-
LEAP-1B28BBJ1
-
LEAP-1B28BBJ2
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
CFM SB LEAP-1A-72-00-0519-01A-930A-D original issue (Issue 001) dated 18 September 2024.
CFM SB LEAP-1B-72-00-0419-01A-930A-D original issue (Issue 001) dated 18 September 2024.
CFM SB LEAP-1C-72-00-0100-01A-930A-D original issue (Issue 001) dated 18 September 2024.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
24-143 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 22 November 2024 as PAD 24-143 for consultation until 03 January 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.
|
