| Number |
US-2010-13-07 |
| Issued by |
 United States of America |
| Issue date |
2010-07-29 |
| Effective date |
2010-07-28 |
| EASA approval number |
|
| Contributor |
EASA General Aviation |
| ATA Chapter |
78 |
Approval Holder
/ Type Designation |
-
PIPER AIRCRAFT INC.
-
PA-32 (Saratoga)
-
PA-32R-301T (Saratoga II TC)
-
PA-46 (Malibu)
|
| Revision |
Not applicable
|
| Correction |
This AD was republished to help eliminate any confusion that the original AD 2010-13-07 may have created. That AD incorrectly stated, in the Summary and Discussion sections, that it requires replacing any spot-welded, V-band exhaust coupling with a riveted, V-band exhaust coupling instead of stating the specific P/N to be replaced. Also, in the Cost of Compliance section, the AD incorrectly stated that Model PA-32R-301T airplanes, instead of Model PA-46-350P airplanes, are equipped with two of the affected V-band clamps.
|
| Supersedure |
None
|
| Publication(s) and related information |
Lycoming Service Instruction No. 1238B, dated January 6, 2010, or the procedures specified in paragraph (e)(1) of this AD. For service information identified in this AD, contact Lycoming, 652 Oliver Street, Williamsport, PA 17701; telephone: (570) 323-6181; fax: (570) 327-7101; Internet: http://www.lycoming.com. |
| Remarks |
Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail:
ADs [at] easa.europa [dot] eu
|
