| Publication(s) and related information |
AH ASB AS350-05-00-0005 original issue (Issue 001) dated 17 June 2026, or Issue 002 dated 20 July 2026.
AH ASB AS355-05-00-0006 original issue (Issue 001) dated 17 June 2026, or Issue 002 dated 20 July 2026.
AH ASB EC130-05-00-0003 original issue (Issue 001) dated 17 June 2026, or Issue 002 dated 20 July 2026.
The use of later approved revisions of the above-mentioned documents 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.
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. All interested persons may send their comments, referencing the AD Number, to the E-mail address specified in below Remark 3, prior to 21 August 2026. Only if any comment is received during the consultation period, a Comment Response Document will be published in the EASA Safety Publications Tool, in a compressed (zipped) file, attached to the record for this AD.
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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