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| Number |
26-001R1 |
| Issued by |
 Europe |
| Issue date |
2026-02-04 |
| EASA approval number |
|
| ATA Chapter |
72 |
Approval Holder
/ Type Designation |
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CFM INTERNATIONAL
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CFM56-5B
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CFM56-5B1
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CFM56-5B1/2P
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CFM56-5B1/3
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CFM56-5B1/P
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CFM56-5B2
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CFM56-5B2/2P
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CFM56-5B2/3
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CFM56-5B2/P
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CFM56-5B3/2P
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CFM56-5B3/2P1
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CFM56-5B3/3
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CFM56-5B3/3B1
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CFM56-5B3/P
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CFM56-5B3/P1
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CFM56-5B4
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CFM56-5B4/2P
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CFM56-5B4/2P1
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CFM56-5B4/3
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CFM56-5B4/3B1
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CFM56-5B4/P
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CFM56-5B4/P1
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CFM56-5B5
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CFM56-5B5/3
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CFM56-5B5/P
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CFM56-5B6
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CFM56-5B6/2P
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CFM56-5B6/3
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CFM56-5B6/P
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CFM56-5B7
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CFM56-5B7/3
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CFM56-5B7/P
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CFM56-5B8/3
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CFM56-5B8/P
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CFM56-5B9/2P
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CFM56-5B9/3
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CFM56-5B9/P
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CFM56-5C
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CFM56-5C2
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CFM56-5C2/4
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CFM56-5C2/F
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CFM56-5C2/F4
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CFM56-5C2/G
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CFM56-5C2/G4
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CFM56-5C2/P
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CFM56-5C3/F
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CFM56-5C3/F4
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CFM56-5C3/G
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CFM56-5C3/G4
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CFM56-5C3/P
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CFM56-5C4
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CFM56-5C4/1
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CFM56-5C4/1P
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CFM56-5C4/P
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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 |
This PAD is revised to remove reference to the one-time inspection, which was proposed to be required in the original issue of this PAD, to mandate the use of the latest revisions of certain SBs and to provide credit for inspections done before the effective date of this AD.
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
CFM56-7B S/B 72-1093 initial issue dated 28 January 2025, Revision 01 dated 10 July 2025, or Revision 02 dated 19 January 2026.
CFM56-5C S/B 72-0811 initial issue dated 28 January 2025, Revision 01 dated 10 July 2025 or Revision 02 dated 19 January 2026.
CFM56-5B S/B 72-1125 initial issue dated 28 January 2025, Revision 01 dated 10 July 2025, or Revision 02 dated 19 January 2026.
CFM56-5C S/B 72-0813 initial issue dated 15 July 2025.
CFM56-5B S/B 72-1129 initial issue dated 10 July 2025 or Revision 01 dated 21 January 2026.
CFM56-7B S/B 72-1096 initial issue dated 10 July 2025 or Revision 01 dated 21 January 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 18 February 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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