| Number |
2023-0184 |
| Issued by |
 Europe |
| Issue date |
2023-10-19 |
| Effective date |
2023-11-02 |
| EASA approval number |
|
| ATA Chapter |
05 |
Approval Holder
/ Type Designation |
-
PILATUS AIRCRAFT LTD
-
PC-12
-
PC-12
-
PC-12/45
-
PC-12/47
-
PC-12/47E
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2008-0163 dated 27 August 2008 and EASA AD 2022-0103 dated 09 June 2022.
|
| Publication(s) and related information |
Pilatus PC-12, PC-12/45 and PC-12/47 AMM Chapter 04-00-00 (DMC-12-A-04-00-00-00A-000A-A issue 19), Document Number 02049 Issue 01 Revision 46 dated 02 October 2023.
Pilatus PC-12/47E AMM Chapter 04-00-00 (DMC-12-B-04-00-00-00A-000A-A issue 22), Document Number 02300 Issue 01 Revision 31 dated 02 October 2023.
Pilatus PC-12/47E AMM Chapter 04-00-00 (DMC-12-C-04-00-00-00A-000A-A issue 7), Document Number 02436 Issue 01 Revision 09 dated 02 October 2023.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD. |
| PAD number |
23-103 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 19 September 2023 as PAD 23-103 for consultation until 17 October 2023. No comments were received during the consultation process.
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.
|
