| Publication(s) and related information |
Airbus DS CN-235 Variation 05 of ALL DT-86-3001 Issue R dated 16 December 2024.
Airbus DS CN-235-300MP Variation 05 of ALL DT-06-3009 Issue A dated 16 December 2024.
The use of later approved revisions of the above-mentioned documents, or of an ALL revision which includes the technical content of the Variation(s), as applicable, is acceptable for compliance with the requirements of this AD. |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. This AD was posted on 19 February 2025 as PAD 25-034 for consultation until 19 March 2025.
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.
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