| Number |
US-2005-01-04 |
| Issued by |
United States of America |
| Issue date |
2005-02-10 |
| Effective date |
2005-02-22 |
| EASA approval number |
|
| ATA Chapter |
28 |
Approval Holder / Type Designation |
-
TEXTRON AVIATION INC.
-
100 (King Air)
-
200 (Super King Air)
-
200
-
200C
-
200CT
-
200T
-
A200
-
A200C
-
A200CT
-
B200
-
B200C
-
B200T
-
300 (Super King Air)
-
65 (Queen Air)
-
90 (King Air)
-
99 (Airliner)
|
| Revision |
Not applicable
|
| Correction |
This AD, originally dated January 6, 2005, was re-published on January 20, 2005, to correct the model C90B (which does not exist) in the Applicability to model C90A. This AD has been re-published again to incorporate the original AD and the Correction into one document to help eliminate any confusion.
|
| Supersedure |
This AD supersedes FAA AD 98-15-13, dated July 16, 1998.
|
| Publication(s) and related information |
Raytheon Aircraft Mandatory SB 2718, Revision 1, dated June 1997; or Revision 2, dated April 2000. For a copy of this service information, contact Raytheon Aircraft Company, P.O. Box 85, Wichita, Kansas 67201-0085; telephone: (800) 625-7043. |
| Remarks |
Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA; E-mail:
ADs [at] easa.europa [dot] eu
|