| Number |
2014-0170 |
| Issued by |
 Europe |
| Issue date |
2014-07-17 |
| Effective date |
2014-07-31 |
| EASA approval number |
|
| ATA Chapter |
05 |
Approval Holder
/ Type Designation |
-
PILATUS AIRCRAFT LTD
-
PC-12
-
PC-12
-
PC-12/45
-
PC-12/47
-
PC-12/47E
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2013-0031 dated 18 February 2013.
|
| Publication(s) and related information |
Pilatus PC-12 Structural, Component and Miscellaneous – Airworthiness Limitations, Chapter 4 of AMM report 02049 issue 28 dated 31 May 2014, for PC-12, PC-12/45, PC-12/47 aeroplanes.
Pilatus PC-12 Structural, Component and Miscellaneous – Airworthiness Limitations, Chapter 4 of AMM report 02300 issue 11 dated 31 May 2014, for PC-12/47E aeroplanes.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
14-102 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 23 June 2014 as PAD 14-102 for consultation until 07 July 2014. No comments were received during the consultation period.
3. Enquiries regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA. E-mail: ADs[at]easa.europa[dot]eu.
|
