| Number |
2023-0082 |
| Issued by |
 Europe |
| Issue date |
2023-04-18 |
| Effective date |
2023-05-02 |
| EASA approval number |
|
| ATA Chapter |
57 |
Approval Holder
/ Type Designation |
-
AIRBUS DEFENCE & SPACE S.A.
-
CN-235
-
CN-235
-
CN-235-100
-
CN-235-200
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes Direccion General de Aviacion Civil (DGAC) Spain AD No. 01/92, dated 14 January 1992.
|
| Publication(s) and related information |
CASA MI COM235-58 dated 21 November 1991.
Airbus DS SB-235-57-15 original issue dated 04 April 1995, or Revision 1 dated 16 March 1998, or Revision 2 dated 21 December 2000.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD. |
| PAD number |
23-032 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. This AD was posted on 14 March 2023 as PAD 23-032 for consultation until 11 April 2023. 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.
|
