| Number |
2019-0074R1 |
| Issued by |
 Europe |
| Issue date |
2022-03-08 |
| Effective date |
2022-03-15 |
| EASA approval number |
|
| ATA Chapter |
62 |
Approval Holder
/ Type Designation |
|
| Revision |
This AD revises EASA AD 2019-0074 dated 28 March 2019.
|
| Correction |
Not applicable
|
| Supersedure |
This original issue of this AD supersedes EASA AD 2017-0191R2 dated 15 December 2017.
|
| Publication(s) and related information |
AH EC225 Emergency ASB 05A051 original issue dated 22 September 2017, or Revision 1 dated 16 November 2017, or Revision 2 dated 26 February 2019, or Revision 3 dated 07 December 2021, or Revision 4 dated 28 February 2022.
The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD. |
| PAD number |
19-032 |
| 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 27 February 2019 as PAD 19-032 for consultation until 27 March 2019. 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.
|
