Safety Publications Tool
2021-0154 : Engine – Propeller Shaft – Replacement [Life Limit]
EASA approval number
EASA Environment & Propulsion Systems Department
/ Type Designation
GE AVIATION CZECH
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.
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 01 June 2021 as PAD 21-080 for consultation until 29 June 2021. 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_2021_0154.pdf (205 kb)
EASA_PAD_21_080.zip (385 kb)
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