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ADs [at] easa.europa [dot] eu
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| Number |
26-052 |
| Issued by |
 Europe |
| Issue date |
2026-04-20 |
| EASA approval number |
|
| ATA Chapter |
80 |
Approval Holder
/ Type Designation |
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2006-0337 dated 07 November 2006.
|
| Publication(s) and related information |
AH ASB EC130-04A002 Revision 0 dated 10 August 2006, Revision 1 dated 14 September 2006 or Revision 2 dated 15 April 2026.
AH ASB AS350-01.00.57 Revision 0 dated 10 August 2006, Revision 1 dated 14 September 2006 or Revision 2 dated 15 April 2026.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| Remarks |
1.
This Proposed AD will be closed for consultation on 04 May 2026.
2.
Enquiries regarding this PAD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.
3.
Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this PAD, and which may occur, or have occurred on a product, part or appliance not affected by this PAD, 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 PAD 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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