Number |
2013-0104R3 |
Issued by |
Europe |
Issue date |
2024-02-20 |
Effective date |
2024-02-27 |
EASA approval number |
|
Contributor |
EASA General Aviation Department |
ATA Chapter |
27 |
Approval Holder / Type Designation |
|
Revision |
This AD revises EASA AD 2013-0104R2 dated 27 October 2022.
|
Correction |
Not applicable
|
Supersedure |
None
|
Publication(s) and related information |
DAHER SB 70-118-27 original issue dated May 2004, Revision 1 dated August 2012, Revision 2 dated September 2022, or Revision 3 dated December 2023.
The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD. |
PAD number |
13-052 |
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 09 April 2013 as PAD 13-052 for consultation until 07 May 2013. 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.
|