| Number |
US-2008-26-02 |
| Issued by |
 United States of America |
| Issue date |
2009-01-20 |
| Effective date |
2009-01-26 |
| EASA approval number |
|
| ATA Chapter |
|
Approval Holder
/ Type Designation |
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes FAA AD 2006-06-51 dated April 17, 2006, previously Emergency AD 2006-06-51, issued on March 17, 2006.
|
| Publication(s) and related information |
GE CT7-8 Shop Manual, GEK 10517; and GE Aircraft Engines CT7-8 SB No. 72-0017, Revision 02, dated May 14, 2008 and earlier revisions pertain to the subject of this AD. Contact General Electric Aircraft Engines CT7 Series Turboshaft Engines, 1000 Western Ave., Lynn, MA 01910; telephone (781) 594-6726; fax (781) 594-1583, for a copy of this service information. |
| Remarks |
Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail:
ADs [at] easa.europa [dot] eu
|
