| Number |
US-2010-10-17 |
| Issued by |
 United States of America |
| Issue date |
2010-11-24 |
| Effective date |
2010-07-22 |
| EASA approval number |
|
| ATA Chapter |
|
Approval Holder
/ Type Designation |
-
MITSUBISHI HEAVY INDUSTRIES LTD.
-
MU-2B (USA production)
-
MU-2B-25
-
MU-2B-26
-
MU-2B-26A
-
MU-2B-36A
-
MU-2B-40
-
MU-2B-60
|
| Revision |
Not applicable
|
| Correction |
This FAA AD corrects the reissue date of the MU-2B-60 airplane flight manual (AFM) in table 3 of the Compliance section (e)(1)(i), in that it is ''September 24, 1985,'' instead of ''September 24, 1986.'' In all other respects, this FAA AD remains the same. This correction is effective November 23, 2010. The effective date for AD 2010-10-17 remains July 22, 2010.
|
| Supersedure |
This AD supersedes FAA AD 97-25-02, FAA AD 2000-02-25, FAA AD 2006-15-07, and FAA AD 2006-17-01.
|
| Publication(s) and related information |
Mitsubishi Heavy Industries, Ltd. MU-2 Service Bulletin (SB) 095/77-002, dated July 15, 1998; and the AFMs specified in Table 6 – Material Incorporated by Reference - of this AD. For service information identified in this AD, contact Mitsubishi Heavy Industries America, Inc., 4951 Airport Parkway, Suite 800, Addison, Texas 75001; telephone: (972) 934-5480; fax: (972) 934-5488; Internet: http://www.mu-2aircraft.com or http://www.turbineair.com. |
| Remarks |
This AD applies to the US-manufactured MU-2B aeroplanes (FAA TCDS A10SW, serial numbers with suffix S.A.) ONLY; for the Japan-manufactured MU-2B aeroplanes, the Japan Civil Aviation Bureau (JCAB) is the State of Design authority, and is expected to take similar AD action. Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA; E-mail: ADs [at] easa.europa [dot] eu
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