| Number |
2013-0031 |
| Issued by |
 Europe |
| Issue date |
2013-02-18 |
| Effective date |
2013-03-04 |
| 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 2012-0099 dated 08 June 2012.
|
| Publication(s) and related information |
Pilatus PC-12 Structural, Component and Miscellaneous – Airworthiness
Limitations, Chapter 4 of AMM report 02049 issue 26 dated 15 December 2012,
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 9 dated 15 December 2012,
for PC-12/47E aeroplane.
The use of later approved revisions of these documents is acceptable for
compliance with the requirements of this AD. |
| PAD number |
13-007 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve
Alternative Methods of Compliance for this AD.
2. This AD was posted on 15 January 2013 as PAD 13-007 for consultation
until 12 February 2013. 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.
|
