Safety Publications Tool
2021-0088R1 : Engine Fuel & Control – Digital Engine Control Unit – Software Update
EASA approval number
EASA Environment & Propulsion Systems Department
/ Type Designation
SAFRAN HELICOPTER ENGINES
This AD revises EASA AD 2021-0088 dated 24 March 2021.
The original issue of this AD superseded DGAC France AD F-2004-017 R1 dated 03 March 2004, EASA approval 2004-1618.
Publication(s) and related information
Turbomeca SB 319 73 2080 Revision 1 dated 13 February 2004. Turbomeca SB 319 73 2081 Revision 1 dated 13 February 2004. Turbomeca SB 319 73 2082 Version D dated 06 June 2011. Turbomeca SB 319 73 2090 original issue dated 13 February 2004. 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 23 February 2021 as PAD 21-030 for consultation until 23 March 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_0088R1.zip (1 mb)
EASA_AD_2021_0088__R1.pdf (200 kb)
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