Safety Publications Tool
2023-0020 : Time Limits / Maintenance Checks – Airworthiness Limitations Section – Amendment
EASA approval number
EASA Environment & Propulsion Systems Department
/ Type Designation
GE AVIATION CZECH
This AD supersedes EASA AD 2021-0060 dated 03 March 2021 and EASA AD 2021-0154 dated 01 July 2021.
Publication(s) and related information
GEAC M601D-1, M601D-2, M601D-11, M601D-11NZ and M601Z EMM No. 0982309 Revision 21 dated 18 November 2022. GEAC M601E and M601E-21 EMM No. 0982055 Revision 21 dated 18 November 2022. GEAC M601E-11, M601E-11S, M601E-11AS, M601F and M601FS EMM No. 0982302 Revision 20 dated 18 November 2022. GEAC M601D EMM No. 0982051 Revision 17 dated 18 November 2022. GEAC ASB-H75-72-10-00-0062, ASB-H80-72-10-00-0107, ASB-H85-72-10-00-0051, ASB-M601F-72-10-00-0070, ASB-M601E-72-10-00-0120, ASB-M601D-72-10-00-0087 and ASB-M601Z-72-10-00-0069, published as a single document, original issue dated 15 December 2022 and Revision 01 dated 20 January 2023. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 16 December 2022 as PAD 22-173 for consultation until 13 January 2023. 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.
EASA_AD_2023_0020.pdf (209 kb)
EASA_PAD_22_173.zip (394 kb)
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