| Number |
2019-0307R1 |
| Issued by |
 Europe |
| Issue date |
2023-03-28 |
| Effective date |
2023-04-11 |
| EASA approval number |
|
| ATA Chapter |
32 |
Approval Holder
/ Type Designation |
-
GENERAL ATOMICS AeroTec Systems GmbH
|
| Revision |
This AD revises EASA AD 2019-0307 dated 18 December 2019.
|
| Correction |
Not applicable
|
| Supersedure |
The original issue of this AD supersedes EASA Emergency AD 2006-0352-E dated 24 November 2006.
|
| Publication(s) and related information |
RUAG ASB Dornier 228-265 original issue dated 17 November 2006, and Revision 1 dated 02 September 2019, and Revision 2 dated 10 December 2019.
RUAG Dornier 228 TM-TLMCM-228-090305-ALL Revision 8 dated 01 August 2018.
RUAG Dornier 228 TM-TLMCM-228-00002-150610 Revision 4 dated 01 August 2018.
The use of later approved revisions of the above-mentioned documents (that may be published by General Atomics, the current design approval holder) is acceptable for compliance with the requirements of this AD. |
| PAD number |
19-182 |
| 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 September 2019 as PAD 19-182 for consultation until 25 October 2019. The Comment Response Document can be found in the EASA Safety Publications Tool, in the compressed (zipped) file attached to the record for this AD.
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.
|
