Safety Publications Tool
2023-0013 : Flight Controls – Rudder Steering Bracket – Inspections / Modification
EASA approval number
EASA General Aviation Department
/ Type Designation
DIAMOND AIRCRAFT INDUSTRIES
DA 42 M
DA 42 M-NG
DA 42 NG
This AD supersedes EASA AD 2019-0302 dated 13 December 2019.
Publication(s) and related information
Diamond Aircraft Industries MSB 42-143 and MSB 42NG-086 (published as a single document), dated 23 December 2021, which includes WI-MSB 42-143 and WI-MSB 42NG-086 original issue dated 23 December 2021; or MSB 42-143/1 and MSB 42NG-086/1 (published as a single document), dated 25 January 2022, which includes WI-MSB 42-143 and WI-MSB 42NG-086 Revision 1 dated 25 January 2022, or Revision 2 dated 10 March 2022, or Revision 3 dated 15 November 2022. Diamond Aircraft Industries MSB 42-146 and MSB 42NG-087 (published as a single document), original issue dated 15 November 2022. Diamond Aircraft Industries Recommended Service Bulletin (RSB) 42-139 or RSB 42NG-081 (published as a single document), original issue dated 21 October 2019. Diamond Aircraft Industries AMM-TR-MAM-42-1213 original issue dated 28 September 2021. 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 19 December 2022 as PAD 22-177 for consultation until 16 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_0013.pdf (207 kb)
EASA_PAD_22_177.zip (389 kb)
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