This N-number isn't registered right now. Below is its last known registration, canceled Jan 11, 2018.
Safety record in brief:1 NTSB accident (Jun 2003)6 ADs may apply63 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 in-flight encounter with turbulence during normal descent resulting in a serious injury to a passenger. A finding in the investigation was the seatbelt sign had been on for approximately 2 minutes at the time of the turbulence encounter.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for MIA03LA127)
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-145LR) |
| 2024-26-07 | Fuselage | Mar 11, 2025 | Airframe (EMB-145LR) |
| 2021-07-14 | Main landing gear | Apr 20, 2021 | Airframe (EMB-145LR) |
| 2004-22-03 | Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135 and -145 Series Airplanes | Dec 3, 2004 | Airframe (EMB-145LR)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-145LR)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-145LR)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.
THE MAIN ENTRY DOOR WAS UNABLE TO BE OPERATED WITH THE HYDRAULIC SYSTEM. MAINTENANCE FOUND AND CLEANED DEBRIS FROM THE MAIN ENTRY DOOR SWITCHES AND ALL OPS CHECKS WERE GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number.THE LIGHT BALLAST OVER THE LAVATORY TOILET WAS FOUND TO BE SMOKING. MAINTENANCE DEACTIVATED THE BALLAST AND DEFERRED IT. MAINTENANCE LATER DETERMINED THE FAULT TO BE DUE TO A FAULTY HARNESS. THE BALLAST REMAINS ON DEFERRAL.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING INSPECTION, CORROSION WAS FOUND ON THE DOUBLER AT LT OMEGA FRAME 20. THE DOUBLER, FILLER, AND 2 OF EACH SHIMS WERE R & R IAW SRM 53-00-10.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING INSPECTION, CORROSION WAS FOUND AT THE TEE FITTING AT FRAME 65. THE TEE FITTING WAS R & R IAW SRM 51-40-02.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING INSPECTION, THE RUDDER TOP HINGE FITTING BUSHING BORE'S WERE FOUND TO BE OUT OF LIMITS. THE TOP HINGE FITTING WAS REPLACED IAW SRM 55-40-02.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING INSPECTION, THE RUDDER BOTTOM HINGE FITTING BUSHING BORES WERE FOUND TO BE OUT OF LIMITS. THE BOTTOM HINGE FITTING WAS REPLACED IAW SRM 55-40-02.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING INSPECTION, THE CENTER OMEGA BEAM WAS FOUND TO HAVE CRACKS AT THE FWD AND AFT NUTPLATES AT FRAMES 59, 60, 61. NEW OMEGA BEAM INSTALLED
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING INSPECTION, THE RT OMEGA BEAM WAS FOUND TO HAVE A CRACK AT THE AFT NUTPLATE BETWEEN FRAMES 60 AND 61. THE BEAM WAS REPAIRED IAW ETD2014-145-05099.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING INSPECTION, CORROSION WAS FOUND IN THE GUSSET CENTER OMEGA AT FRAMES 20, 21, 22, 23. THE CENTER OMEGA BEAM WAS R & R IAW SRM 51-40-02.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING INSPECTION, CORROSION WAS FOUND AT THE LOWER HOLE AT THE UPRIGHT STANTION AT FRAME 20 AND THE LT OMEGA BEAM. THE STANTION WAS R & R IAW SRM 51-40-02.
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 63 reports.