Safety Publications Tool
Starting from 26 February 2024, for an AD published with no prior consultation as PAD (except for an Emergency AD), if any comments are received during the period of 28 days following the publication of that AD, EASA will publish a Comment Response Document (CRD) collecting EASA answers to those comments.
Please refer to the “Remarks” section of such ADs for instructions about how to send comments.
2022-0230 : Flight Controls – Aileron and Airbrake Control Rod Connecting Devices – Replacement
EASA approval number
EASA General Aviation Department
/ Type Designation
CALSBACH, INGENIEURBUERO UG
EASA STC 10070970
DG AVIATION GmbH
Publication(s) and related information
Ingenieurburo Calsbach UG SB STC 10070970-1 original issue dated 09 August 2022. 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. Based on the required actions and the compliance time, EASA have decided to issue a Final AD with Request for Comments, postponing the public consultation process until after publication. 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_2022_0230.pdf (192 kb)
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