This N-number isn't registered right now. Below is its last known registration, canceled Mar 30, 2018.
Safety record in brief:2 NTSB incidents (minor damage at worst, latest Aug 2011)4 ADs may apply47 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 improper air traffic control takeoff clearance issued by the local controller because of his lack of monitoring and lack of awareness of the conflicting arrival airplane.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for OPS11IA819)
The airport authorities' improper decision to deactivate the jet bridge braking system which created an unsafe condition by the gate agents not being able to stop the bridge from impacting the airplane during a wind gust.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CEN11IA270)
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.
DURING INSPECTION, BOTH OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING CRUISE, HEARD A LOUD POP IN COCKPIT AND CAPTAIN'S WINDSCREEN SHATTERED. DESCENDED AND DECLARED AN EMERGENCY. DIVERTED AND LANDED WITHOUT INCIDENT. REPLACED WINDSHIELD. OPS AND LEAK CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING INSPECTION, THE OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MX REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.
From FAA Service Difficulty Reports; matched by N-number and serial number.CREW REPORTED THAT THEY RECEIVED RUDDER SYSTEM 1 AND 2 INOPERATIVE MESSAGES ON CLIMBOUT. THE ASSOCIATED MESSAGES OF YAW DAMPER FAIL AND AUTO-PILOT FAIL WERE ALSO PRESENT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RUDDER SYSTEM 1 AND 2 PRESSURE SWITCHES.…
From FAA Service Difficulty Reports; matched by N-number and serial number.CREW REPORTED THAT THEY RECEIVED RUDDER SYSTEM 1 AND 2 INOPERATIVE MESSAGES ON CLIMBOUT. THE ASSOCIATED MESSAGES OF YAW DAMPER FAIL AND AUTO-PILOT FAIL WERE ALSO PRESENT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RUDDER SYSTEM 1 AND 2 PRESSURE SWITCHES.…
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING INSPECTION, CORROSION WAS FOUND ON THE EDGE OF STRINGER 21R AT FRAME 11 THROUGH 12. THE STRINGER WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING INSPECTION, THE LEFT SIDE COCKPIT BULK HEAD BAYONET RECEPTACLE UPPER REPAIR WAS FOUND TO BE DAMAGED. THE UPPER PLATES WERE REPLACED IN ACCORDANCE WITH SRM 51-40-00.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING INSPECTION, THE LEFT SIDE COCKPIT BULK HEAD BAYONET RECEPTACLE LOWER REPAIR WAS FOUND TO BE DAMAGED. THE LOWER PLATE WERE REPLACED IN ACCORDANCE WITH SRM 51-40-00.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT OUTBOARD SEAT TRACK AT FRAME 23 THROUGHT FRAME 28. THE SEAT TRACK WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING INSPECTION, THE COCKPIT UNDERFLOOR AILERON QUADRANT RIGHT SUPPORT BRACKET WAS FOUND TO BE CORRODED. THE SUPPORT BRACKET WAS REPLACED 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 47 reports.