Number |
2020-0261R1 |
Issued by |
Europe |
Issue date |
2022-06-30 |
Effective date |
2022-07-07 |
EASA approval number |
|
Contributor |
EASA Environment and Propulsion Systems Department |
ATA Chapter |
72 |
Approval Holder / Type Designation |
-
CFM INTERNATIONAL
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CFM56-3
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CFM56-3
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CFM56-3B
-
CFM56-3C
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CFM56-7B
-
CFM56-7B20
-
CFM56-7B20/2
-
CFM56-7B20/3
-
CFM56-7B22
-
CFM56-7B22/2
-
CFM56-7B22/3
-
CFM56-7B22/3B1
-
CFM56-7B22/B1
-
CFM56-7B24
-
CFM56-7B24/2
-
CFM56-7B24/3
-
CFM56-7B24/3B1
-
CFM56-7B24/B1
-
CFM56-7B26
-
CFM56-7B26/2
-
CFM56-7B26/3
-
CFM56-7B26/3B1
-
CFM56-7B26/3B2
-
CFM56-7B26/3B2F
-
CFM56-7B26/3F
-
CFM56-7B26/B1
-
CFM56-7B26/B2
-
CFM56-7B27
-
CFM56-7B27/2
-
CFM56-7B27/3
-
CFM56-7B27/3B1
-
CFM56-7B27/3B1F
-
CFM56-7B27/3B3
-
CFM56-7B27/3F
-
CFM56-7B27/B1
-
CFM56-7B27/B3
|
Revision |
This AD revises EASA AD 2020-0261 dated 27 November 2020.
|
Correction |
Not applicable
|
Supersedure |
This original issue of this AD superseded EASA AD 2012-0209 dated 08 October 2012.
|
Publication(s) and related information |
CFMI CFM56-7B S/B 72-0564 Revision 2 dated 16 November 2010, Revision 3 dated 25 May 2011, Revision 4 dated 30 September 2013, Revision 5 dated 14 January 2014, Revision 6 dated 20 January 2017, Revision 7 dated 07 November 2018, Revision 8 dated 06 May 2020 and Revision 9 dated 03 December 2021.
CFMI CFM56-3 S/B 72-1129 original issue dated 09 March 2011, Revision 1 dated 22 June 2012, Revision 2 dated 16 November 2012, Revision 3 dated 15 January 2014, Revision 4 dated 19 February 2016, Revision 5 dated 20 January 2017, Revision 6 dated 07 November 2018 and Revision 7 dated 06 May 2020.
CFMI CFM56-7B S/B 72-0879 Revision 1 dated 12 April 2012, Revision 2 dated 15 July 2013, Revision 3 dated 15 January 2014, Revision 4 dated 07 September 2015, Revision 5 dated 20 January 2017, Revision 6 dated 01 March 2018 and Revision 7 dated 10 February 2021.
CFMI CFM56-7B S/B 72-1071 original issue dated 03 December 2021.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
PAD number |
20-100R1 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. The original issue of this AD was posted on 29 June 2020 as PAD 20-100 for consultation until 27 July 2020, and republished as PAD 20-100R1 on 19 October 2020 for additional consultation until 02 November 2020. The Comment Response Documents can be found in the EASA Safety Publications Tool, in the compressed (zipped) file attached to the record for this AD.
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.
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