| Number |
US-2002-26-01 |
| Issued by |
 United States of America |
| Issue date |
2002-12-27 |
| Effective date |
2003-01-31 |
| EASA approval number |
|
| ATA Chapter |
72 |
Approval Holder
/ Type Designation |
-
LYCOMING ENGINES
-
AEIO-320
-
AEIO-360
-
AEIO-540
-
AIO-320
-
AIO-360
-
HIO-360
-
IGO-480
-
IGO-540
-
IO-320
-
IO-360
-
IO-540
-
IO-720
-
IVO-360
-
IVO-540
-
LIO-320
-
LIO-360
-
LTIO-540
-
TIO-360
-
TIO-540
-
TIVO-540
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes FAA AD 93-02-05, effective date 14 June 1993 (all fuel-injected engines, except Model TIO-540-S1AD engines) and FAA AD 93-05-22, effective date 11 May 1993 (TIO-540-S1AD engines only).
|
| Publication(s) and related information |
Textron Lycoming MSB No. 342D, dated July 10, 2001. Copies may be obtained from Textron Lycoming, 652 Oliver Street, Williamsport, PA 17701, telephone (570) 323-6181. |
| Remarks |
Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail:
ADs [at] easa.europa [dot] eu
|
