| Number |
2019-0087-E |
| Issued by |
 Europe |
| Issue date |
2019-04-24 |
| Effective date |
2019-04-26 |
| EASA approval number |
|
| Contributor |
EASA eVTOL & New Concepts Section |
| ATA Chapter |
67 |
Approval Holder
/ Type Designation |
-
AIRBUS HELICOPTERS DEUTSCHLAND
-
EC135/635
-
EC135 P1
-
EC135 P2
-
EC135 P2+
-
EC135 P3
-
EC135 T1
-
EC135 T2
-
EC135 T2+
-
EC135 T3
-
EC635 P2+
-
EC635 P3
-
EC635 T1
-
EC635 T2+
-
EC635 T3
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
AH ASB EC135-67A-039 original issue dated 08 April 2019, or Revision 01 dated 23 April 2019.
AH ASB EC135H-67A-011 original issue dated 08 April 2019, or Revision 01 dated 23 April 2019.
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 Programming and Continued
Airworthiness 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.
|
