Number |
2022-0034 |
Issued by |
Europe |
Issue date |
2022-03-04 |
Effective date |
2022-03-18 |
EASA approval number |
|
Contributor |
EASA Environment & Propulsion Systems Department |
ATA Chapter |
72 |
Approval Holder / Type Designation |
-
GE AVIATION CZECH
-
H75, H80, H85
-
H75-100
-
H75-200
-
H80
-
H80-100
-
H80-200
-
H85-100
-
H85-200
-
M601
-
M601D
-
M601D-1
-
M601D-11
-
M601D-11NZ
-
M601D-2
-
M601E
-
M601E-11
-
M601E-11A
-
M601E-11AS
-
M601E-11S
-
M601E-21
-
M601F
-
M601FS
-
M601Z
|
Revision |
Not applicable
|
Correction |
Not applicable
|
Supersedure |
None
|
Publication(s) and related information |
GEAC ASB ASB-H75-72-40-00-0056, ASB-H80-72-40-00-0099, ASB-M601F-72-40-00-0064, ASB-M601E-72-40-00-0113, ASB-M601D-72-40-00-0081, ASB-M601Z-72-40-00-0063 and ASB-H85-72-40-00-0045 (issued as single document) original issue dated 21 December 2021, and Revision 01 dated 16 February 2022.
The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD. |
PAD number |
22-010 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted 31 January 2022 as PAD 22-010 for consultation until 28 February 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.
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