| Number |
2024-0225 |
| Issued by |
 Europe |
| Issue date |
2024-11-26 |
| Effective date |
2024-12-10 |
| 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
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2023-0108 dated 26 May 2023.
|
| Publication(s) and related information |
CFM SB LEAP-1A-72-00-0470-01A-930A-D Issue 003 dated 03 March 2023.
CFM SB LEAP-1A-72-00-0493-01A-930A-D Issue 002 dated 17 November 2022.
CFM SB LEAP-1A-72-00-0496-01A-930A-D original issue (Issue 001) dated 07 March 2023.
CFM SB LEAP-1A-72-00-0507-01A-930A-D original issue (Issue 001) dated 24 January 2024.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
24-118 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 16 October 2024 as PAD 24-118 for consultation until 13 November 2024. 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.
|
