Number |
2021-0062 |
Issued by |
Europe |
Issue date |
2021-03-05 |
Effective date |
2021-03-19 |
EASA approval number |
|
Contributor |
EASA Environment and Propulsion Systems Department |
ATA Chapter |
72 |
Approval Holder / Type Designation |
-
CFM INTERNATIONAL
-
CFM56-5B
-
CFM56-5B1
-
CFM56-5B1/P
-
CFM56-5B2
-
CFM56-5B2/P
-
CFM56-5B3/P
-
CFM56-5B3/P1
-
CFM56-5B4
-
CFM56-5B4/P
-
CFM56-5B4/P1
-
CFM56-5B5
-
CFM56-5B5/P
-
CFM56-5B6
-
CFM56-5B6/P
-
CFM56-5B7
-
CFM56-5B7/P
-
CFM56-5B8/P
-
CFM56-5B9/P
|
Revision |
Not applicable
|
Correction |
Not applicable
|
Supersedure |
This AD supersedes EASA AD 2016-0039 dated 29 February 2016.
|
Publication(s) and related information |
CFMI CFM56-5B SB 72-0308 Revision 5 dated 12 October 2007.
CFMI CFM56-5B SB 72-0309 Revision 5 dated 12 October 2007.
CFMI CFM56-5B SB 72-0850 dated 19 December 2012 and Revision 1 dated 16 August 2018.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD. |
PAD number |
20-178 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. This AD was posted on 06 November 2020 as PAD 20-178 for consultation until 04 December 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.
|