Safety Publications Tool
leading to the decision not to take AD action similar to Federal Aviation Administration (FAA) AD 2019-24-01
leading to the decision not to take AD action similar to Federal Aviation Administration (FAA) AD 2020-01-15
2020-0201R1 : Engine Fuel & Control – Fuel Control Unit – Replacement
EASA approval number
EASA Environment and Propulsion Systems Department
/ Type Designation
GE AVIATION CZECH
H75, H80, H85
This AD revises EASA Emergency AD 2020-0201-E dated 21 September 2020.
Publication(s) and related information
GE Aviation Czech ASB-H75-73-00-00-0038, ASB-H80-73-00-00-0074, ASB-H85-73-00-00-0032, ASB-M601D-73-00-00-0066, ASB-M601E-73-00-00-0097, ASB-M601F-73-00-00-0050 and ASB-M601T-73-00-00-0040 (single document) original issue dated 18 September 2020, and Revision 1 dated 24 September 2020. 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. The results of the safety assessment have indicated the need for immediate publication and notification, without the full consultation process. 3. Enquiries regarding this AD should be referred to the EASA Programming and Continued Airworthiness 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_2020_0201.zip (2 mb)
EASA_AD_2020_0201_R1.pdf (587 kb)
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