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|
| Number |
21-080 |
| Issued by |
 Europe |
| Issue date |
2021-06-01 |
| EASA approval number |
|
| Contributor |
EASA Environment & Propulsion Systems Department |
| ATA Chapter |
72 |
Approval Holder
/ Type Designation |
-
GE AVIATION CZECH
-
M601
-
M601D
-
M601D-1
-
M601D-11
-
M601D-11NZ
-
M601D-2
-
M601E
-
M601E-11
-
M601E-11A
-
M601E-11AS
-
M601E-11S
-
M601E-21
-
M601F
-
M601F-11
-
M601F-22
-
M601F-32
-
M601FS
-
M601T
-
M601Z
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes AD 2021-0052 dated 24 February 2021.
|
| Publication(s) and related information |
GEAC ASB-M601D-72-10-00-0072, ASB-M601E-72-10-00-0103, ASB-M601F-72-10-00-0056 and ASB-M601Z-72-10-00-0056 (single document) original issue dated 13 February 2021, or Revision 01 dated 18 March 2021, and Revision 02 dated 31 May 2021.
The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD. |
| Remarks |
1. This Proposed AD will be closed for consultation on 29 June 2021.
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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