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ADs [at] easa.europa [dot] eu
|
| Number |
21-091 |
| Issued by |
 Europe |
| Issue date |
2021-06-24 |
| EASA approval number |
|
| Contributor |
EASA General Aviation & VTOL Department |
| ATA Chapter |
|
Approval Holder
/ Type Designation |
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2013-0287 dated 05 December 2013.
|
| Publication(s) and related information |
AH ASB AS350-01.00.67 original issue dated 04 December 2013, or Revision 1 dated 30 January 2014, or Revision 2 dated 17 February 2014.
AH ASB EC130-04A004 original issue dated 04 December 2013, or Revision 1 dated 30 January 2014 or Revision 2 dated 17 February 2014.
SAFRAN SB 292 73 2852 version A (original issue) dated 06 December 2013, version B dated 12 February 2014 or version C dated 06 June 2016.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD. |
| Remarks |
1. This Proposed AD will be closed for consultation on 22 July 2021.
2. Enquiries regarding this PAD should be referred to the EASA Safety Information Section,
Certification Directorate. E-mail: ADs[at]easa.europa.eu.
3. Information about any failures, malfunctions, defects or other occurrences, which may be
similar to the unsafe condition addressed by this PAD, and which may occur, or have occurred
on a product, part or appliance not affected by this PAD, 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 PAD 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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