Number |
2022-0167 |
Issued by |
Europe |
Issue date |
2022-08-11 |
Effective date |
2022-08-25 |
EASA approval number |
|
Contributor |
EASA General Aviation Department |
ATA Chapter |
27 |
Approval Holder / Type Designation |
-
TECNAM, Costruzioni Aeronautiche
|
Revision |
Not applicable
|
Correction |
Not applicable
|
Supersedure |
This AD supersedes EASA AD 2022-0132 dated 04 July 2022.
|
Publication(s) and related information |
TECNAM SB 574-CS Ed. 1 original issue (Rev 0), or Rev 1 dated 31 May 2022, or Rev 2 dated 04 July 2022, or Rev 3 dated 01 August 2022.
The use of later approved revisions of the above-mentioned document 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.
|