| Number |
2022-0007 |
| Issued by |
 Europe |
| Issue date |
2022-01-19 |
| Effective date |
2022-02-02 |
| EASA approval number |
|
| ATA Chapter |
05 |
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 |
None
|
| Publication(s) and related information |
CFM LEAP-1A ESM SM.20, Chapter 05, currently at Revision 019, data modules as listed in Appendix 1 of this AD.
CFM SB LEAP-1A-72-00-0413-01A-930A-D, Issue 004 dated 11 December 2021.
CFM SB LEAP-1A-72-00-0463-01A-930A-C, Issue 001 dated 17 November 2021
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD. |
| PAD number |
21-177 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. This AD was posted on 02 December 2021 as PAD 21-177 for consultation until 07 January
2022. 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.
|
