| Number |
2018-0014-CN |
| Issued by |
 Europe |
| Issue date |
2018-01-24 |
| Effective date |
2018-01-24 |
| EASA approval number |
|
| ATA Chapter |
72 |
Approval Holder
/ Type Designation |
-
SAFRAN HELICOPTER ENGINES
-
ARTOUSTE II
-
ARTOUSTE II C5
-
ARTOUSTE II C6
-
ARTOUSTE III
-
ARTOUSTE III B
-
ARTOUSTE III B1
-
ASTAZOU XIV
-
TURMO IV C
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This Notice cancels DGAC France AD 2002-597 and AD 2002-598, both dated 27 November 2002, AD F-2005-060 (EASA approval 2005-3067) dated 13 April 2005 and AD F-2005-064 (EASA approval 2005-3626) dated 27 April 2005.
|
| Publication(s) and related information |
The related Safran Helicopter Engines or Turbomeca SB, as applicable to engine type and model, is specified in each relevant EASA TCDS (hyperlinks provided above): ARTOUSTE II: EASA.E.137, ARTOUSTE III: EASA.E.091, ASTAZOU XIV: EASA.E.075, and TURMO IV: EASA.E.074. |
| PAD number |
17-171-CN |
| Remarks |
1. This AD-CN was posted on 13 December 2017 as PAD 17-171-CN for consultation until 10 January 2018. No comments were received during the consultation period.
2. Enquiries regarding this AD-CN should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.
|
