| Number |
2021-0086 |
| Issued by |
 Europe |
| Issue date |
2021-03-24 |
| Effective date |
2021-04-07 |
| EASA approval number |
|
| Contributor |
EASA General Aviation & VTOL Department |
| ATA Chapter |
67 |
Approval Holder
/ Type Designation |
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2014-0080 dated 27 March 2014.
|
| Publication(s) and related information |
AH ASB AS332-05.00.98 original issue dated 26 March 2014, or Revision 1 dated 10 February 2021.
AH SB AS332-67.00.52 original issue dated 02 March 2020.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
21-026 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 22 February 2021 as PAD 21-026 for consultation until 22 March 2021. 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.
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