| Number |
2024-0181R1 |
| Issued by |
 Europe |
| Issue date |
2024-09-24 |
| Effective date |
2024-10-03 |
| EASA approval number |
|
| Contributor |
EASA General Aviation Department |
| ATA Chapter |
27 |
Approval Holder
/ Type Designation |
|
| Revision |
This AD revises EASA AD 2024-0181 dated 19 September 2024.
|
| Correction |
Not applicable
|
| Supersedure |
The original issue of this AD superseded EASA AD 2023-0219-E dated 19 December 2023.
|
| Publication(s) and related information |
Pilatus PC-24 SB 27-010 original issue dated 04 July 2024.
The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD.
|
| PAD number |
24-102 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. The original issue of this AD was posted on 15 August 2024 as PAD 24-102 for consultation until 12 September 2024. 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.
|
