Number |
2023-0048-E |
Issued by |
Europe |
Issue date |
2023-03-07 |
Effective date |
2023-03-09 |
EASA approval number |
|
Contributor |
EASA General Aviation Department |
ATA Chapter |
57, 11 |
Approval Holder / Type Designation |
-
CEAPR
-
DR 400
-
DR 400/100
-
DR 400/120
-
DR 400/120 A
-
DR 400/120 D
-
DR 400/125
-
DR 400/125 i
-
DR 400/140
-
DR 400/140 B
-
DR 400/160
-
DR 400/160 D
-
DR 400/180
-
DR 400/180 R
-
DR 400/180 S
-
DR 400/2+2
-
DR 400/200 I
-
DR 400/200 R
-
DR 400/500
-
DR 400/NGL
-
DR 400/RP
|
Revision |
Not applicable
|
Correction |
Not applicable
|
Supersedure |
This AD supersedes EASA Emergency AD 2022-0267-E dated 27 December 2022.
|
Publication(s) and related information |
CEAPR SB 221201 original issue (Edition 1) dated 23 December 2022, or Revision 1 dated 28 December 2022, or Revision 2 dated 06 March 2023.
APEX AIRCRAFT / CEAPR mod No. 020903 (approved 20 January 2003) and associated modification instruction No. 1001047 original issue (Issue H) dated 19 May 2003.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. The results of the safety assessment have indicated the need for immediate publication and notification, without the full consultation process.
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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