| Number |
2007-0241R4 |
| Issued by |
 Europe |
| Issue date |
2010-08-31 |
| Effective date |
2010-09-14 |
| EASA approval number |
|
| ATA Chapter |
57 |
Approval Holder
/ Type Designation |
|
| Revision |
This Airworthiness Directive (AD) revises EASA AD 2007-0241R3 dated 06 May 2009.
|
| Correction |
Not applicable
|
| Supersedure |
The original issue oif this AD superseded FOCA (Switzerland) AD TM-L Nr. 80.627-6 / Index 72-2 dated 06 December 1972, FOCA AD HB-2006-400 dated 21 September 2006, and EASA AD 2007-0114 dated 02 May 2007.
|
| Publication(s) and related information |
Pilatus Aircraft Ltd. PC-6 SB No. 57-005 dated 30 August 2007, Revision 1
dated 19 November 2007 and Revision 2 dated 19 May 2008.
Pilatus PC-6 AMM Chapter 04-00-00, Document Number 01975, Revision 12
dated 14 May 2010.
The use of later approved revisions of these 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 initial issue of this AD was published as an Emergency AD on 05 September 2007.
3. Enquiries regarding this AD should be referred to the Airworthiness Directives, Safety Management & Research Section, Certification Directorate, EASA; E-mail ADs[@]easa.europa.eu.
|
