| Number |
US-2001-24-12 |
| Issued by |
 United States of America |
| Issue date |
2001-12-26 |
| Effective date |
2001-12-19 |
| EASA approval number |
|
| ATA Chapter |
72 |
Approval Holder
/ Type Designation |
-
ROLLS-ROYCE CORPORATION (USA)
-
250 Series II
-
250-C20
-
250-C20B
-
250-C20F
-
250-C20J
-
250-C20R
-
250-C20R/1
-
250-C20R/2
-
250-C20S
-
250-C20W
-
250-B15/-B17
-
250-B17
-
250-B17C
-
250-B17D
-
250-B17E
-
250-B17F
-
250-B17F/1
-
250-B17F/2
|
| Revision |
Not applicable
|
| Correction |
This AD was republished to add the AD number (2001-20-51) being superseded, which was inadvertently omitted in the original AD.
|
| Supersedure |
This AD supersedes FAA Emergency AD 2001-20-51, dated October 3, 2001.
|
| Publication(s) and related information |
For a copy of service information related to this AD, if any, contact Rolls-Royce Corporation, P.O. Box 420, Indianapolis, IN 46206-0420; telephone +1 (317) 230-6400; fax 1 (317) 230-4243. |
| Remarks |
Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail:
ADs [at] easa.europa [dot] eu
|
