| Number |
2022-0234 |
| Issued by |
 Europe |
| Issue date |
2022-12-01 |
| Effective date |
2022-12-15 |
| EASA approval number |
|
| Contributor |
EASA Environment & Propulsion Systems Department |
| ATA Chapter |
76 |
Approval Holder
/ Type Designation |
-
GE AVIATION CZECH
-
H75, H80, H85
-
M601
-
M601E-11AS
-
M601E-11S
-
M601FS
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
GEAC ASB SB-M601F-76-00-00-0071, SB-M601E-76-00-00-0121, SB-H85-76-00-00-0052,
SB-H75-76-00-00-0063 and SB-H80-76-00-00-0108 (issued as a single document) original issue dated 11 August 2022.
The use of later approved revisions of the above-mentioned document is acceptable for compliance
with the requirements of this AD. |
| PAD number |
22-144 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. This AD was posted on 25 October 2022 as PAD 22-144 for consultation until 22 November
2022. No comments were received during the consultation period.
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.
|
