This N-number isn't registered right now. Below is its last known registration, canceled Dec 29, 2015.
Safety record in brief:1 NTSB incident (Jun 2011)6 ADs may apply107 service difficulty reports
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Individual owners are shown by city and state only.
the Gulfport control tower local controller cleared two aircraft for takeoff from runways with intersecting departure flight paths without ensuring the first aircraft had passed the flight path intersection prior to clearing the second aircraft for takeoff.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for OPS11IA673)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2025-08-07 | Flight Controls | Jun 26, 2025 | Airframe (EMB-145EP) |
| 2024-26-07 | Fuselage | Mar 11, 2025 | Airframe (EMB-145EP) |
| 2021-07-14 | Main landing gear | Apr 20, 2021 | Airframe (EMB-145EP) |
| 2004-22-03 | Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135 and -145 Series Airplanes | Dec 3, 2004 | Airframe (EMB-145EP)Serial numbers per EMBRAER Service Bulletin 145-57-0034, Change 01, dated January 9, 2002 |
| 2002-14-23 | Empresa Brasileira de Aeronautica S.A. | Aug 2, 2002 | Airframe (EMB-145EP)Serial numbers per EMBRAER Service Bulletin 145-27-0088, dated February 1, 2002. Only with: Equipped with horizontal stabilizer actuator (HSA) assemblies having part numbers and serial numbers listed in EMBRAER Service Bulletin 145-27-0088. |
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2000-09-09 | EMBRAER Model EMB-145 Series Airplanes | Jun 16, 2000 | Airframe (EMB-145EP)Certain serial numbers: EMB-145 145004–145047; EMB-145 145049–145051. Only with: Equipped with IC-600 #1 P/N 7017000-82402; excluding airplanes modified per EMBRAER SB 145-22-0001, SB 145-22-0004 Rev 01, or SB 145-31-0007 Rev 02. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
DURING 1A CHECK THE RT FUSELAGE SKIN WAS FOUND TO BE CRACKED AROUND A RIVET AT FR79 ABOVE STR 6R. MX REMOVED THE DAMAGE AND PERFORMED A BUSHING REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE ON 07/15/13.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING 1A INSPECTION THE RT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET AT FR77 STRINGER 04R. MX REMOVED THE DAMAGE AND PERFORMED A BUSHING REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE ON 07/15/2013.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING 1A INSPECTION THE RT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET AT FR78 BETWEEN STRINGERS 5 & 6R. MX REMOVED THE DAMAGE AND PERFORMED A BUSHING REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING 1A CHECK THE RT FUSELAGE SKIN WAS FOUND TO BE CRACKED AROUND A RIVET AT FR79 BELOW STR 6R. MX REMOVED THE DAMAGE AND PERFORMED A BUSHING REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING 1A CHECK THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED AROUND A RIVET AT FR77 BELOW STR 04L. MX REMOVED THE DAMAGE AND PERFORMED A BUSHING REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE ON 07/15/13.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING 1A CHECK THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED AROUND A RIVET AT FR 77 ABOVE S6L. MX REMOVED THE DAMAGE AND PERFORMED A BUSHING REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING 1A CHECK THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED AROUND A RIVET AT FR78 BELOW S4L. MX REMOVED THE DAMAGE AND PERFORMED A BUSHING REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING 1A CHECK THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED AROUND A RIVET AT FR79 ABOVE STR 06L. MX REMOVED THE DAMAGE AND PERFORMED A BUSHING REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number.THE CREW REPORTED A BURNING ODOR IN THE CABIN NOTICED BY THE F/A. MX INSPECTED THE ACFT AND WAS UNABLE TO DUPLICATE ANY BURNING ODOR OR SMELL, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number.THE CREW REPORTED THAT THE EMERGENCY LIGHT ABOVE ROW 1A WAS INOPERATIVE. MX R & R THE AFFECTED LIGHT ASSY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 107 reports.