Safety Publications Tool
2021-0195 : Rotorcraft Flight Manual – Engine Digital Electronic Control Unit Emergency Procedure – Amendment
EASA approval number
EASA VTOL Department
/ Type Designation
AS 350 / EC 130
AS 350 B3
EC 130 T2
This AD supersedes EASA AD 2013-0287 dated 05 December 2013.
Publication(s) and related information
AH ASB AS350-01.00.67 original issue dated 04 December 2013, or Revision 1 dated 30 January 2014, or Revision 2 dated 17 February 2014. AH ASB EC130-04A004 original issue dated 04 December 2013, or Revision 1 dated 30 January 2014 or Revision 2 dated 17 February 2014. SAFRAN SB 292 73 2852 version A (original issue) dated 06 December 2013, version B dated 12 February 2014 or version C dated 06 June 2016. 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 24 June 2021 as PAD 21-091 for consultation until 22 July 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_0195.pdf (206 kb)
EASA_PAD_21_091.zip (388 kb)
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