| Number |
2023-0072 |
| Issued by |
 Europe |
| Issue date |
2023-04-05 |
| Effective date |
2023-04-19 |
| EASA approval number |
|
| ATA Chapter |
|
Approval Holder
/ Type Designation |
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
WSK "PZL-SWIDNIK" S.A. PZL SW-4 ASB ASB-60-23-116 original issue dated 04 April 2023.
WSK "PZL-SWIDNIK" S.A. PZL SW-4 Basic RFM, ref. AE-60.01.04.1 RFM, Reissue 1, PART 1, Revision 6 dated 31 January 2023.
WSK "PZL-SWIDNIK" S.A. PZL SW-4 RFMS No. AE-60.01.04.1 RFMS - 0.00, Reissue 1, Revision 3 dated 31 January 2023.
WSK "PZL-SWIDNIK" S.A. PZL SW-4 RFMS No. AE-60.01.04.1 RFMS - 37.00, Reissue 1, Revision 1 dated 31 January 2023.
WSK "PZL-SWIDNIK" S.A. PZL SW-4 RFMS No. AE-60.01.04.1 RFMS - 40.00, Reissue 1, original issue (Revision 0) dated 31 January 2023.
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.
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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