| Number |
US-2006-12-07 |
| Issued by |
 United States of America |
| Issue date |
2006-06-06 |
| Effective date |
2006-07-11 |
| EASA approval number |
|
| ATA Chapter |
72 |
Approval Holder
/ Type Designation |
-
LYCOMING ENGINES
-
AEIO-320
-
AEIO-320-D1B
-
AEIO-320-D2B
-
AEIO-320-E1A
-
AEIO-320-E1B
-
AEIO-320-E2A
-
AEIO-320-E2B
-
AEIO-360
-
AEIO-360-B1B
-
AEIO-360-B1D
-
AEIO-360-B1F
-
AEIO-360-B1F6
-
AEIO-360-B1G6
-
AEIO-360-B1H
-
AEIO-360-B2F
-
AEIO-360-B2F6
-
AEIO-360-B4A
-
AEIO-360-H1A
-
AEIO-360-H1B
-
AEIO-540
-
AEIO-540-D4A5
-
AEIO-540-D4B5
-
AEIO-540-D4C5
-
AEIO-540-D4D5
-
AIO-320
-
AIO-320-A1A
-
AIO-320-A1B
-
AIO-320-A2A
-
AIO-320-A2B
-
AIO-320-B1B
-
AIO-320-C1B
-
HIO-360
-
HIO-360-B1A
-
HIO-360-B1B
-
HIO-360-G1A
-
HO-360
-
HO-360-A1A
-
HO-360-B1A
-
HO-360-B1B
-
HO-360-C1A
-
IO-320
-
IO-320-A1A
-
IO-320-A2A
-
IO-320-B1A
-
IO-320-B1B
-
IO-320-B1C
-
IO-320-B1D
-
IO-320-B1E
-
IO-320-B2A
-
IO-320-C1A
-
IO-320-C1B
-
IO-320-D1A
-
IO-320-D1B
-
IO-320-D1C
-
IO-320-E1A
-
IO-320-E1B
-
IO-320-E2A
-
IO-320-E2B
-
IO-320-F1A
-
IO-360
-
IO-360-B1A
-
IO-360-B1B
-
IO-360-B1C
-
IO-360-B1D
-
IO-360-B1E
-
IO-360-B1F
-
IO-360-B1F6
-
IO-360-B1G6
-
IO-360-B2E
-
IO-360-B2F
-
IO-360-B2F6
-
IO-360-B4A
-
IO-360-E1A
-
IO-360-F1A
-
IO-360-L2A
-
IO-360-M1A
-
IO-360-M1B
-
IO-540
-
IO-540-AB1A5
-
IO-540-C1B5
-
IO-540-C1C5
-
IO-540-C2C
-
IO-540-C4B5
-
IO-540-C4B5D
-
IO-540-C4C5
-
IO-540-C4D5
-
IO-540-C4D5D
-
IO-540-D4A5
-
IO-540-D4B5
-
IO-540-D4C5
-
IO-540-J4A5
-
IO-540-N1A5
-
IO-540-R1A5
-
IO-540-T4A5D
-
IO-540-T4B5
-
IO-540-T4B5D
-
IO-540-T4C5D
-
IO-540-V4A5
-
IO-540-V4A5D
-
IO-540-W1A5
-
IO-540-W1A5D
-
IO-540-W3A5D
-
LIO-320
-
LO-360
-
LTIO-540
-
LTO-360
-
O-320
-
O-320-A1A
-
O-320-A1B
-
O-320-A2A
-
O-320-A2B
-
O-320-A2C
-
O-320-A2D
-
O-320-A3A
-
O-320-A3B
-
O-320-A3C
-
O-320-B1A
-
O-320-B1B
-
O-320-B2A
-
O-320-B2B
-
O-320-B2C
-
O-320-B2D
-
O-320-B2E
-
O-320-B3A
-
O-320-B3B
-
O-320-B3C
-
O-320-C1A
-
O-320-C1B
-
O-320-C2A
-
O-320-C2B
-
O-320-C2C
-
O-320-C3A
-
O-320-C3B
-
O-320-C3C
-
O-320-D1A
-
O-320-D1B
-
O-320-D1C
-
O-320-D1D
-
O-320-D1F
-
O-320-D2A
-
O-320-D2B
-
O-320-D2C
-
O-320-D2F
-
O-320-D2G
-
O-320-D2H
-
O-320-D2J
-
O-320-D3G
-
O-320-E1A
-
O-320-E1B
-
O-320-E1C
-
O-320-E1F
-
O-320-E1J
-
O-320-E2A
-
O-320-E2B
-
O-320-E2C
-
O-320-E2D
-
O-320-E2F
-
O-320-E2G
-
O-320-E2H
-
O-320-E3D
-
O-320-E3H
-
O-360
-
O-360-A1A
-
O-360-A1AD
-
O-360-A1C
-
O-360-A1D
-
O-360-A1F
-
O-360-A1F6
-
O-360-A1F6D
-
O-360-A1G
-
O-360-A1G6
-
O-360-A1G6D
-
O-360-A1H
-
O-360-A1H6
-
O-360-A1LD
-
O-360-A1P
-
O-360-A2A
-
O-360-A2D
-
O-360-A2E
-
O-360-A2F
-
O-360-A2G
-
O-360-A2H
-
O-360-A3A
-
O-360-A3AD
-
O-360-A3D
-
O-360-A4A
-
O-360-A4AD
-
O-360-A4D
-
O-360-A4G
-
O-360-A4J
-
O-360-A4K
-
O-360-A4M
-
O-360-A4N
-
O-360-A4P
-
O-360-A5AD
-
O-360-B1A
-
O-360-B1B
-
O-360-B2A
-
O-360-B2B
-
O-360-B2C
-
O-360-C1A
-
O-360-C1C
-
O-360-C1E
-
O-360-C1F
-
O-360-C1G
-
O-360-C2A
-
O-360-C2B
-
O-360-C2C
-
O-360-C2D
-
O-360-C2E
-
O-360-C4F
-
O-360-C4P
-
O-360-D1A
-
O-360-D2A
-
O-360-D2B
-
O-360-F1A6
-
O-360-G1A6
-
O-360-J2A
-
O-540
-
O-540-A1A
-
O-540-A1A5
-
O-540-A1B5
-
O-540-A1C5
-
O-540-A1D
-
O-540-A1D5
-
O-540-A2B
-
O-540-A3D5
-
O-540-A4A5
-
O-540-A4B5
-
O-540-A4C5
-
O-540-A4D5
-
O-540-B1A5
-
O-540-B1B5
-
O-540-B1D5
-
O-540-B2A5
-
O-540-B2B5
-
O-540-B2C5
-
O-540-B4A5
-
O-540-B4B5
-
O-540-D1A5
-
O-540-E4A5
-
O-540-E4B5
-
O-540-E4C5
-
O-540-F1A5
-
O-540-F1B5
-
O-540-G1A5
-
O-540-G2A5
-
O-540-H1A5
-
O-540-H1A5D
-
O-540-H1B5D
-
O-540-H2A5
-
O-540-H2A5D
-
O-540-H2B5D
-
O-540-J1A5D
-
O-540-J1B5D
-
O-540-J1C5D
-
O-540-J1D5D
-
O-540-J2A5D
-
O-540-J2B5D
-
O-540-J2C5D
-
O-540-J2D5D
-
O-540-J3A5
-
O-540-J3A5D
-
O-540-J3C5D
-
O-540-L3C5D
-
TIO-540
-
TIO-540-AA1AD
-
TIO-540-AB1AD
-
TIO-540-AB1BD
-
TIO-540-AF1A
-
TIO-540-AG1A
-
TIO-540-AK1A
-
TIO-540-C1A
-
TIO-540-E1A
-
TIO-540-G1A
-
TIO-540-H1A
-
TIO-540-K1AD
-
TO-360
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes FAA AD 2005-26-10, dated December 27, 2005.
|
| Publication(s) and related information |
ECi SB No. 05-08, Revision 2, dated February 28, 2006. For a copy of this service information, contact Engine Components Inc. (ECi), 9503 Middlex, San Antonio, TX 78217, telephone +1 (210) 820-8101, Fax: +1 (210) 820-8102, or go to http://www.eci.aero/pages/tech_svcpubs.aspx.
|
| Remarks |
Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail:
ADs [at] easa.europa [dot] eu
|
