| Number |
2019-0070 |
| Issued by |
 Europe |
| Issue date |
2019-03-28 |
| Effective date |
2019-04-11 |
| EASA approval number |
|
| ATA Chapter |
55 |
Approval Holder
/ Type Designation |
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes DGAC France AD F-2003-366 R1 (EASA approval 2004-11116) dated 24 November 2004.
|
| Publication(s) and related information |
EADS SOCATA SB 70-104-55 original issue dated June 2003, or Revision 1 dated August 2004, or
Revision 2 dated January 2007, or Revision 3 dated December 2007, or DAHER Aerospace SB
70-104-55 Revision 4 dated December 2018.
DAHER Aerospace SB 70-255-55 original issue dated December 2018.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD. |
| PAD number |
19-027 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. This AD was posted on 18 February 2019 as PAD 19-027 for consultation until 18 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.
|
