Safety record in brief:1 NTSB accident (substantial damage, Sep 2014)6 ADs may apply176 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 tractor driver's failure to give way to the taxiing airplane.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for DCA14CA170)
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-145XR) |
| 2024-26-07 | Fuselage | Mar 11, 2025 | Airframe (EMB-145XR) |
| 2021-07-14 | Main landing gear | Apr 20, 2021 | Airframe (EMB-145XR) |
| 2004-22-03 | Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135 and -145 Series Airplanes | Dec 3, 2004 | Airframe (EMB-145XR)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-145XR)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-145XR)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.
AISLE EMERGENCY LIGHT LAMP AT ROW 18 BURNED OUT. REMOVED AND REPLACED ROW 18 AISLE EMERGENCY LIGHT LAMP. OPS CHECK SAT.
From FAA Service Difficulty Reports; matched by N-number and serial number.FUMES SMELLED ON TO ON OCF FROM SURFACE TO 2000 FT SIMILAR TO GASOLINE NOT JET A. INSPECTED E1/E2 INLETS. T/S USING FIM. FOUND BURNT OIL ODOR WOULD OCCUR WHEN RUNNING PACKS OFF OF APU. INSPECTED APU FOR SIGNS OF OVERSERVICING. FOUND APU OIL OVER SERVICED ABOVE FULL LINE. CORRECTED APU OIL LEVEL.…
From FAA Service Difficulty Reports; matched by N-number and serial number.FUMES IN COCKPIT AND CABIN ON LIFT OFF. T/S, PERFORMED ENGINES RUNS. PERFORMED PACKS OPERATION. NO ABNORMAL SMELLS OBSERVED, NO DEFECTS NOTED. FURTHER T/S INSPECTED W/S TEMP CONTROL. FOUND NO DEFECTS. INSEPCTED W/S TERM. NO DEFECTS. INSPECTED COMP. WASH PORT CAP. NO SIGNS OF OIL. RAN ENGINES ON…
From FAA Service Difficulty Reports; matched by N-number and serial number.SCREWS HOLES ELONGATED ON BOTH STARKE SPLICE SKIN. STARKE SPLICE SKIN (2X) FABRICATED.
From FAA Service Difficulty Reports; matched by N-number and serial number.CF4, EXTERNAL POTABLE WATER DRAIN DOUBLER BTW FR 57-58 AND STR 19R-20R FOUND CORRODED. CF4 EXTERNAL POTABLE WATER DRAIN DOUBLER BTW FR 57-58 AND STR 19R-20R REMOVED FOR ACCESS, CORROSION BLENDED WITHIN LIMIT. AFTER INVESTIGATION, INTERNAL SKIN BTW FR 57-59 AND BTW STR 19R-29 FOUND CORROSION OUT OF…
From FAA Service Difficulty Reports; matched by N-number and serial number.LH FR 72 BTW STR 16L-17L SHEAR CLIP FOUND CRACKED. AT FR72 BTW STR 16L-17L SHEAR CLIP REMOVED FOR REPLACEMENT. AT FR72 BTW STR 16L-17L INSTALLED.
From FAA Service Difficulty Reports; matched by N-number and serial number.REAR FUSELAGE I AVIONIC COMPARTMENT, AT FR 75 AND STR 14R SUPPORT ON ELECTRIC RACK CRACKED. REAR FUSE I AVIONIC COMPARTMENT AT FR 75 AND STR 14R SUPPORT ON ELECTRIC RACK REMOVED AND REPLACED
From FAA Service Difficulty Reports; matched by N-number and serial number.RH WING TO BODY FAIRING, ANGLE #3 FOUND CRACKED. RH WING TO BODY FAIRING, ANGLE #3 REPLACED.
From FAA Service Difficulty Reports; matched by N-number and serial number.CF3, SHEAR CLIP AT FR 52 BTW STR 21L-21R FOUND CORRODED. CF3, SHEAR CLIP ON FR52 BTW STR 21L-21R BOTH SHEAR CLIPS BLENDED AND FOUND OUT OF LIMIT. CF3, SHEAR CLIPS ON FR52 BTW STR 21-21R REMOVED AND INSTALLED.
From FAA Service Difficulty Reports; matched by N-number and serial number.CF1, RH OMEGA BEAM FOUND CORRODED AT FR20 AND AT FR23. AFTER INVESTIGATION, NO CORROSION FOUND AT FR20, ONLY CORROSION FOUND AT FR23. AT CF1 FR23 RH OMEGA BEAM BLENDED OUT OF LIMITS. AT CF1 FR23 CUTOUT MADE ON RH OMEGA BEAM. REPAIR PART FABRICATED. AT CF1 FR23 REPAIR PART INSTALLED ON RH OMEGA BEAM
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 176 reports.