| Number |
2017-0075R1 |
| Issued by |
 Europe |
| Issue date |
2017-05-05 |
| Effective date |
2017-05-16 |
| EASA approval number |
|
| Contributor |
EASA Propulsion Section |
| ATA Chapter |
71 |
Approval Holder
/ Type Designation |
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
|
| Revision |
This AD revises EASA AD 2017-0075 dated 02 May 2017.
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Rolls-Royce plc NMSB RB.211-71-AJ576 original issue dated 17 March 2017.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD. |
| PAD number |
17-040 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. The original issue of this AD was posted on 24 March 2017 as PAD 17-040 for consultation until 21 April 2017. The Comment Response Document can be found in the EASA Safety Publications Tool, in the compressed (zipped) file attached to the record for this AD.
3. Enquiries regarding this AD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.
|
