| Number |
US-2003-17-04 |
| Issued by |
 United States of America |
| Issue date |
2003-08-20 |
| Effective date |
2003-10-03 |
| EASA approval number |
|
| ATA Chapter |
56 |
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 |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Mitsubishi MU-2 SB No. 087/56-001B (revision B) dated May 4, 1998. For a copy of this service information, contact Mitsubishi Heavy Industries America, Inc., 4951 Airport Parkway, suite 800, Addison, Texas 75001; telephone: (972) 934-5480; facsimile: (972) 934-5488. |
| 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 have issued AD TCD-4311-95, also adopted by EASA. Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA; E-mail: ADs [at] easa.europa [dot] eu
|
