This N-number isn't registered right now. Below is its last known registration, canceled Apr 3, 2020.
Safety record in brief:1 NTSB accident (substantial damage, May 2014)4 ADs may apply26 service difficulty reports
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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.
An in-flight collision with a bird during the descent to land, which resulted in substantial damage to the airplane.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CEN14LA262)
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 |
|---|---|---|---|
| 2024-26-07 | Fuselage | Mar 11, 2025 | Airframe (EMB-135KL) |
| 2021-07-14 | Main landing gear | Apr 20, 2021 | Airframe (EMB-135KL) |
| 2004-22-03 | Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135 and -145 Series Airplanes | Dec 3, 2004 | Airframe (EMB-135KL)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-135KL)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. |
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.
CREW REPORTED THAT AFTER TAKEOFF, THEY RECEIVED AN ENG 1 FIRE DETECTION FAIL MSG. THE CREW DIVERTED THE ACFT & LANDED WITHOUT FURTHER INCIDENT. REPLACED THE ENG 1 PYLON FIRE LOOP. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING FLIGHT THERE WAS AN OIL BURNING ODOR IN THE COCKPIT WHILE USING BLEED SYSTEM 1 AND BOTH PACK SYSTEMS TURNED ON. THE ODOR WAS ONLY PRESENT IN THE COCKPIT AND CLEARED ON THE GROUND WHILE USING THE APU AS A BLEED SOURCE. LANDED WITHOUT INCIDENT. MX REPLACED THE NR 1 ENGINE. OPS CHECKED GOOD…
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING ALL PHASES OF FLIGHT, A SLIGHT OIL BURNING ODOR WAS PRESENT. MX RAN BOTH ENGINES WITH THE ENGINE BLEED AND PACK SYS TURNED ON. NO ODORS OR DEFECTS WERE NOTED AND ACFT RETURNED TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING INSPECTION, THE OVERHEAD COCKPIT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MX REPLACED THE COCKPIT EMERGENCY LIGHT BULB. OPS CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING INSPECTION, A TOOLING MARK ON THE INTERIOR BELLY SKIN WAS FOUND ADJACENT TO STRINGER 21L AND BETWEEN FRAMES 10 AND 11. THE SKIN WAS REPAIRED IN ACCORDANCE WITH ETD 2013-145-008436.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING INSPECTION, A MISDRILLED RIVET HOLE ON THE RIGHT CONTROL CABLE QUADRANT SUPPORT. THE SUPPORT BRACKETS AND QUADRANT SUPPORT WERE REPLACED IN ACCORDANCE WITH SRM 51-40-02 AND 51-20-03.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING INSPECTION, AN ELONGATED RIVET HOLE WAS FOUND ON FRAME 12 BETWEEN STRINGERS 21R AND 20R. THE FRAME WAS REPAIRED IN ACCORDANCE WITH ETD 2013-145-008257.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING INSPECTION, CORROSION AND CRACKS WERE FOUND ON THE FLOORBOARD SUPPORT FLANGE OF THE LEFT OMEGA BEAM BETWEEN FRAME 24 AND FRAME 25. THE OMEGA BEAM WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-10.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING INSPECTION, CORROSION WAS FOUND ON STRINGER 21R BETWEEN FRAMES 13 AND 9. THE STRINGER WAS REPLACED IAW SRM 51-40-02.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING INSPECTION, CORROSION WAS FOUND IN THE RIGHT AILERON QUADRANT SUPPORT WEB AT FRAME 12 AND 13 AND STRINGERS 20R AND 21R. THE RIGHT QUADRANT SUPPORT WAS REPAIRED IN ACCORDANCE WITH SRM 51-40-02.
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 26 reports.