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ADs [at] easa.europa [dot] eu
|
| Number |
25-169 |
| Issued by |
 Europe |
| Issue date |
2025-11-03 |
| EASA approval number |
|
| ATA Chapter |
05 |
Approval Holder
/ Type Designation |
-
PILATUS AIRCRAFT LTD
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PC-6
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PC-6
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PC-6-H1
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PC-6-H2
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PC-6/350
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PC-6/350-H1
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PC-6/350-H2
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PC-6/A
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PC-6/A-H1
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PC-6/A-H2
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PC-6/A1-H2
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PC-6/A2-H2
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PC-6/B-H2
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PC-6/B1-H2
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PC-6/B2-H2
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PC-6/B2-H4
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PC-6/C-H2
-
PC-6/C1-H2
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2020-0278 dated 14 December 2020.
|
| Publication(s) and related information |
Pilatus PC-6 ALS Document Number 02334, issue 13 dated 31 October 2025.
Pilatus PC-6 AMM, Chapter 04-00-00, Document Number 01975, issue 39 dated 31 October 2025.
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 01 December 2025.
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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