| Number |
2024-0226 |
| 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-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 |
This AD supersedes EASA AD 2023-0109 dated 26 May 2023.
|
| Publication(s) and related information |
CFM SB LEAP-1B-72-00-0392-01A-930A-D Issue 002 dated 05 September 2023.
CFM SB LEAP-1B-72-00-0402-01A-930A-D original issue (Issue 001) dated 23 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 |
24-119 |
| 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 24-119 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.
|
