| Number |
2023-0080 |
| Issued by |
 Europe |
| Issue date |
2023-04-17 |
| Effective date |
2023-05-01 |
| EASA approval number |
|
| ATA Chapter |
32 |
Approval Holder
/ Type Designation |
-
DAHER AEROSPACE
-
M.S. 880
-
M.S. 880 B
-
M.S. 880 B-D
-
M.S. 881
-
M.S. 883
-
M.S. 884
-
M.S. 885
-
M.S. 886
-
M.S. 887
-
M.S. 890
-
M.S. 890 A
-
M.S. 890 B
-
M.S. 892 A.150
-
M.S. 892 B.150
-
M.S. 892 E-D.150
-
M.S. 892 E.150
-
M.S. 893 A
-
M.S. 893 B
-
M.S. 893 E
-
M.S. 893 E-D
-
M.S. 894 A
-
M.S. 894 E
-
Rallye 100
-
Rallye 100 S
-
Rallye 100 S-D
-
Rallye 100 ST
-
Rallye 100 ST-D
-
Rallye 110 ST
-
Rallye 150
-
Rallye 150 ST
-
Rallye 150 ST-D
-
Rallye 150 SV
-
Rallye 150 SVS
-
Rallye 150 T
-
Rallye 150 T-D
-
Rallye 180
-
Rallye 180 T
-
Rallye 180 T-D
-
Rallye 180 TS
-
Rallye 235
-
Rallye 235 A
-
Rallye 235 E
-
Rallye 235 E-D
-
Rallye 235 F
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2015-0203 dated 07 October 2015.
|
| Publication(s) and related information |
SOCATA SB 150-32 Revision 2 dated January 1994, or Revision 3 dated September 2015, or DAHER SB 150-32 Revision 4 dated January 2023.
The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD. |
| PAD number |
23-034 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. This AD was posted on 16 March 2023 as PAD 23-034 for consultation until 13 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.
|
