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ADs [at] easa.europa [dot] eu
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| Number |
26-091 |
| Issued by |
Europe |
| Issue date |
2026-07-30 |
| EASA approval number |
|
| ATA Chapter |
72 |
Approval Holder / Type Designation |
-
CFM INTERNATIONAL
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CFM56-7B
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CFM56-7B20
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CFM56-7B20/2
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CFM56-7B20/3
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CFM56-7B20E
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CFM56-7B22
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CFM56-7B22/2
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CFM56-7B22/3
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CFM56-7B22/3B1
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CFM56-7B22/B1
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CFM56-7B22E
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CFM56-7B22E/B1
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CFM56-7B24
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CFM56-7B24/2
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CFM56-7B24/3
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CFM56-7B24/3B1
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CFM56-7B24/B1
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CFM56-7B24E
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CFM56-7B24E/B1
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CFM56-7B26
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CFM56-7B26/2
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CFM56-7B26/3
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CFM56-7B26/3B1
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CFM56-7B26/3B2
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CFM56-7B26/3B2F
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CFM56-7B26/3F
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CFM56-7B26/B1
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CFM56-7B26/B2
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CFM56-7B26E
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CFM56-7B26E/B1
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CFM56-7B26E/B2
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CFM56-7B26E/B2F
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CFM56-7B26E/F
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CFM56-7B27
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CFM56-7B27/2
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CFM56-7B27/3
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CFM56-7B27/3B1
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CFM56-7B27/3B1F
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CFM56-7B27/3B3
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CFM56-7B27/3F
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CFM56-7B27/B1
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CFM56-7B27/B3
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CFM56-7B27A
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CFM56-7B27A/3
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CFM56-7B27AE
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CFM56-7B27E
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CFM56-7B27E/B1
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CFM56-7B27E/B1F
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CFM56-7B27E/B3
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CFM56-7B27E/F
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2019-0018 dated 30 January 2019.
|
| Publication(s) and related information |
CFM International S.A. CFM56-7B SB 72-1019 original issue dated 24 March 2017, or Revision 01 dated 13 June 2017.
CFM International S.A. CFM56-7B SB 72-1024 original issue dated 26 July 2017.
CFM International S.A. CFM56-7B SB 72-1033 original issue dated 20 April 2018, or Revision 01 dated 09 May 2018, or Revision 02 dated 27 July 2018, or Revision 03 dated 06 November 2018, or Revision 04 dated 12 September 2019, or Revision 05 dated 28 July 2026.
CFM International S.A. ESM Revision 54 Incremental Change, or Revision 55 or later Revisions, or Revision 67 dated 15 July 2026.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| Remarks |
1.
This Proposed AD will be closed for consultation on 27 August 2026.
2. Enquiries regarding this PAD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.
3. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this PAD, and which may occur, or have occurred on a product, part or appliance not affected by this PAD, 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 PAD 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.
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