# N14514: 2000 Embraer EMB-135LR, registration cancelled 2018-10-30 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 30, 2018 - Exported to: Angola - Status when cancelled: Valid registration - Airframe: [Embraer EMB-135LR](https://openairdocs.org/model/embraer-emb-135lr) (registry code 3260305) - Engine: [Allison AE-3007A](https://openairdocs.org/engine/allison-ae-3007a) (registry code 03030) - Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (OpenAirDocs) - Serial number: 145303 - Year built: 2000 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: August 30, 2000 - Certificate issued: June 15, 2018 - Last registry action: June 15, 2018 - Mode S code: A0B7DB - Owner when cancelled: [Tvpx Aircraft Solutions Inc Trustee](https://openairdocs.org/faa-owner/TVPX%20AIRCRAFT%20SOLUTIONS%20INC%20TRUSTEE) - Location: [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake) - Owner type: Corporation - Owner's area on the map: 40.8386° N, 111.9179° W: Placed by OpenAirDocs at the center of ZIP code 84054, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N14514 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14514 - Page: https://openairdocs.org/deregistered/N14514-2018-10-30 From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Embraer EMB-135LR: https://openairdocs.org/model/embraer-emb-135lr.md ## Service difficulty reports (65, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASOA20140701087](https://openairdocs.org/sdr/ASOA20140701087), Jul 1, 2014: BULB. FAILED. THE F/A REPORTED THE LIGHT AT SEAT 2A WAS FLICKERING AND HAD AN ELECTRICAL BURNING ODOR. MAINTENANCE R & R THE BULB, OPERATED CABIN LIGHTS WITH NO DEFECTS OR OD - [SDR ASOA20140506067](https://openairdocs.org/sdr/ASOA20140506067), May 4, 2014: SKIN. CRACKED. DURING 4A INSPECTION, THE LEFT AFT FUSELAGE SKIN WAS FOUND TO HAVE A 2 MM CRACK EMINATING FROM A RIVET ON FRAME 75, STRINGER 2L. MAINTENANCE REMOVED THE DAMAGE - [SDR ASOA20140108006](https://openairdocs.org/sdr/ASOA20140108006), Jan 8, 2014: INVERTER. INOPERATIVE. DURING ROUTINE CHECK THE FWD EMERGENCY EXIT SIGN IN THE OVERWING AISLE CEILING PANEL WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 6 EMERGENCY LIGHT INV - [SDR ASOA20131212282](https://openairdocs.org/sdr/ASOA20131212282), Dec 12, 2013: LIGHT. INOPERATIVE. AFT OVERHEAD EMERGENCY LIGHT INOPERATIVE. R & R OVERHEAD EMERGENCY LIGHT IAW 33-50-13. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20130423139](https://openairdocs.org/sdr/ASOA20130423139), Apr 20, 2013: INVERTER. INOPERATIVE. DURING ROUTINE CHECK THE GALLEY EMERGENCY LIGHTS FAILED OPS TESTING. MX R & R THE NR 3 INVERTER IAW AMM 33-50-11. THE EMERGENCY LIGHTS OPS CHECKED GOOD. THE ACF - [SDR ASOA20130322039H](https://openairdocs.org/sdr/ASOA20130322039H), Mar 22, 2013: CONNECTOR. DISCONNECTED. DURING MX INSPECTION, THE EMERGENCY LIGHT EXIT LOCATING SIGN IN THE GALLEY AISLE CEILING PANEL WAS FOUND TO BE INOPERATIVE. MX INSPECTED THE SIGN, RECONNECTED T - [SDR C2XA08IA185](https://openairdocs.org/sdr/C2XA08IA185), Aug 2, 2008: SIGN. DISCONNECTED. IAH - DURING MAINTENANCE INSPECTION LT EMERGENCY EXIT IDENTIFIER AT THE EXIT ROW WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE LIGHT, RESECURED THE CON - [SDR C2XA08IA184](https://openairdocs.org/sdr/C2XA08IA184), Aug 2, 2008: WIRE. BROKEN. IAH - DURING MAINTENANCE INSPECTION THE EMERGENCY LIGHT ON THE SERVICE DOOR SWING ARM WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE, OPERATIONAL - [SDR C2XA08SH095](https://openairdocs.org/sdr/C2XA08SH095), Jul 11, 2008: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM FR 21-23 HAS VARIOUS AREAS OF CORROSION ON LWR FLANGE WEB. MX REMOVED LT OMEGA BEAM FROM 17 SPLICE TO FR 26 AND INSTALLED WIT - [SDR C2XA08IA135](https://openairdocs.org/sdr/C2XA08IA135), Jun 5, 2008: BALLAST. INOPERATIVE. IAH - FLIGHT 2452, DURING PREFLIGHT INSPECTION THE CREW REPORTED AN ELECTRICAL ODOR IN THE CABIN. MAINTENANCE INSPECTED THE ACFT, AND REMOVED AND REPLACED THE L - [SDR C2XA08IA106](https://openairdocs.org/sdr/C2XA08IA106), Apr 8, 2008: CONNECTOR. DIRTY. IAH - FLIGHT 2791, DURING PREFLIGHT INSPECTION THE CREW REPORTED THE SECOND AND THIRD SECTION OF AISLE PATH LIGHTING TO BE INOPERATIVE. MAINTENANCE CLEANED THE - [SDR C2XA07IA227](https://openairdocs.org/sdr/C2XA07IA227), Oct 22, 2007: LIGHT. INOPERATIVE. DURING SCHEDULED MAINTENANCE THE EMERGENCY STRIP LIGHT AT ROW 3A TO 7A WAS FOUND TO BE INOPERATIVE. THE FLOOR STRIP WIRING WAS FOUND TO BE CHAFED. THE AFFECTED - [SDR C2XA07IA197](https://openairdocs.org/sdr/C2XA07IA197), Sep 9, 2007: UNKNOWN. ODOR. IAH - FLIGHT 2890, DURING PRE-FLIGHT INSPECTION, THE NUMBER ONE ELECTRIC HYDRAULIC PUMP FAILED AND A SMOKE SMELL WAS REPORTED IN THE COCKPIT. MAINTENANCE OPERAT - [SDR C2XA07IA126](https://openairdocs.org/sdr/C2XA07IA126), May 28, 2007: UNKNOWN. ODOR. SLP - FLIGHT 2148, THE CREW REPORTED A BURNING ODOR AT THE COFFEEMAKERS. THE AIRCRAFT RETURNED TO SLP WHERE THE COFFEEMAKERS WERE PLACED ON MEL AND THE AIRCRAFT - [SDR C2XA06IA157](https://openairdocs.org/sdr/C2XA06IA157), Sep 23, 2006: UNKNOWN. SMOKE. LEX - FLIGHT 2671, THE CREW REPORTED SMOKE IN THE COCKPIT AFTER AN ACARS MESSAGE FOR PACK 2 VALVE CLOSED MESSAGE. THE AIRCRAFT DIVERTED TO LEX WHERE IT LANDED W - [SDR C2XA06IA111](https://openairdocs.org/sdr/C2XA06IA111), Jul 18, 2006: CONTROLLER. FAULTY. DURING START, THE CREW REPORTED A BURNING SMELL IN THE COCKPIT AND CABIN. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE CABIN LIGHT CONTROLLER - [SDR C2XA06SH071](https://openairdocs.org/sdr/C2XA06SH071), Jul 1, 2006: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS - [SDR C2XA05IA083](https://openairdocs.org/sdr/C2XA05IA083), Jun 18, 2005: BALLAST. INOPERATIVE. THE CREW REPORTED A BURNED/HOT ELECTRICAL ODOR COMING FROM THE GALLEY. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE LIGHT BALLAST FOR THE GAL - [SDR C2XA05IA054](https://openairdocs.org/sdr/C2XA05IA054), Apr 18, 2005: RELAY. FAILED. THE CREW REPORTED THAT THE NR 3 PITOT INOPERATIVE WHILE CLIMBING THROUGH CLOUDS, AND THE COCKPIT FILLED WITH SMOKE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT - [SDR C2XA04IA126](https://openairdocs.org/sdr/C2XA04IA126), Oct 5, 2004: LIGHT. INOPERATIVE. IAH- FLIGHT 2621, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHT ON THE SERVICE DOOR WAS INOPERATIVE. MAINTENANCE REMOVED AND REPL - [SDR C2XA04IA108](https://openairdocs.org/sdr/C2XA04IA108), Aug 25, 2004: BULB. BURNED OUT. IAH - DURING 3A INSPECTION, THE AFT OVERHEAD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, AND THE AIRC - [SDR C2XA04TY070](https://openairdocs.org/sdr/C2XA04TY070), Apr 15, 2004: CARBON SEAL. LEAKING. AIR RETURN, FERRIED TO TYS FROM EWR, FOR LAV SMOKE ON EICAS, STRONG ODOR IN COCKPIT. MAINTENANCE REMOVED AND REPLACED THE ZERO CARBON SEAL ON THE LEFT ENGINE. O - [SDR C2XA04SH174](https://openairdocs.org/sdr/C2XA04SH174), Mar 20, 2004: BUTTSTRAP. CORRODED. SHV- DURING C-CHECK THE AFT FLOORBEAM BUTTSTRAP BETWEEN FRAMES 17 AND 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW E - [SDR C2XA04SH173](https://openairdocs.org/sdr/C2XA04SH173), Mar 20, 2004: SILL. CORRODED. SHV- DURING C-CHECK THE LT FLOOR SILL BETWEEN FRAMES 18 AND 24 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 135 SRM 51-4 - [SDR C2XA04SH172](https://openairdocs.org/sdr/C2XA04SH172), Mar 20, 2004: BUTTSTRAP. CORRODED. SHV- DURING C-CHECK THE FORWARD FLOORBEAM BUTTSTRAP AT FRAME 14 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IA - [SDR C2XA04SH167](https://openairdocs.org/sdr/C2XA04SH167), Mar 17, 2004: FLOORBEAM. CORRODED. SHV - DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A FILLER SHIM REPAIR IAW EMB 13 - [SDR C2XA04SH170](https://openairdocs.org/sdr/C2XA04SH170), Mar 17, 2004: SUPPORT BRACKET. CORRODED. SHV - DURING C-CHECK THE PASSENGER DOOR THRESHOLD AFT U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 135 SRM - [SDR C2XA04SH169](https://openairdocs.org/sdr/C2XA04SH169), Mar 17, 2004: BRACKET. CORRODED. SHV - DURING C-CHECK THE PASSENGER DOOR THRESHOLD FORWARD U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 135 - [SDR C2XA04SH168](https://openairdocs.org/sdr/C2XA04SH168), Mar 17, 2004: SUPPORT BEAM. CORRODED. SHV - DURING C-CHECK THE AFT GALLEY SUPPORT BEAM BETWEEN FRAMES 22 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 1 - [SDR C2XA04SH166](https://openairdocs.org/sdr/C2XA04SH166), Mar 17, 2004: FLOORBEAM. CRACKED. SHV - DURING C-CHECK, THE T-SECTION IN THE LOWER CARGO DOOR CUTOUT AT FRAME 67 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE CRACKED T-SECTION I - [SDR C2XA04SH165](https://openairdocs.org/sdr/C2XA04SH165), Mar 16, 2004: BEAM. CORRODED. SHV - DURING C-CHECK THE CARGO DOOR LOWER CUT BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 135 SRM 51-40-02. THE AI - [SDR C2XA04SH164](https://openairdocs.org/sdr/C2XA04SH164), Mar 16, 2004: FRAME. CRACKED. SHV - DURING C-CHECK THE ATTACH ANGLE ON THE LOWER END OF THE T-SECTION AT FRAME 66 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED THE CRACKED ANGLE, FABRICATED A - [SDR C2XA04SH163](https://openairdocs.org/sdr/C2XA04SH163), Mar 16, 2004: DOOR FRAME. CRACKED. SHV - DURING C-CHECK THE LEFT T-SECTION AT THE CARGO DOOR CUT FRAME 66 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE CRACKED SECTION IAW EMB 135 - [SDR C2XA04SH162](https://openairdocs.org/sdr/C2XA04SH162), Mar 16, 2004: SILL. CORRODED. SHV - DURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED AROUND THE NUT PLATES AT FRAME 21. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED - [SDR C2XA04SH152](https://openairdocs.org/sdr/C2XA04SH152), Mar 12, 2004: INTAKE. GOUGED. SHV - DURING C-CHECK, THE NR 2 ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE TOP COWLING GUIDE PIN HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUB - [SDR C2XA04SH151](https://openairdocs.org/sdr/C2XA04SH151), Mar 12, 2004: INTAKE. GOUGED. SHV - DURING C-CHECK, THE NR 1 ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE TOP COWLING GUIDE PIN HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUB - [SDR C2XA04IA004](https://openairdocs.org/sdr/C2XA04IA004), Jan 8, 2004: BRACKET. DISTORTED. FLIGHT 3250 - PILOT REPORTED THAT THE LANDING GEAR DID NOT RETRACT. THE AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE LANDING GEAR AN - [SDR C2XA02CL196](https://openairdocs.org/sdr/C2XA02CL196), Oct 7, 2002: SWITCH. INOPERATIVE. CLT FLIGHT#3177 THE CREW REPORTED A RUDDER 1/2 FAIL MESSAGE ON CLIMBOUT.THE AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE REPLACED TH - [SDR C2XA02CL133](https://openairdocs.org/sdr/C2XA02CL133), Jun 16, 2002: AUTOPILOT SYS. MALFUNCTIONED. CLE FLIGHT 4015 THE CREW REPORTED A AUTO PILOT FAIL MESSAGE AFTER FLIGHT INTO MODERATE TURBULENCE ASSOCIATED WITH BURNING SMELL IN THE COCKPIT AND CABIN. MAINTE - [SDR C2XA02CL056](https://openairdocs.org/sdr/C2XA02CL056), Feb 20, 2002: WIRE. BROKEN. CLE FLIGHT#3133 THE CREW REPORTED THE EMERGENCY EXIT LIGHT AT ROW 9 WAS INOPERATIVE.MAINTENANCE INSPECTED AND REPAIRED A WIRE ON THE EMERGENCY AISLE PATH LIGHTI - [SDR C2XA02TY003](https://openairdocs.org/sdr/C2XA02TY003), Jan 1, 2002: PROXIMITY SWITCH. CRACKED. TYS AT TAKEOFF THE LANDING GEAR/GROUND FAIL MESSAGE INDICATOR CAME ON. CREW RETURNED AND MAINTENANCE REMOVED AND REPLACED THE NLG WOW PROXIMITY SWITCH AND THEN - [SDR C2XA01TY226](https://openairdocs.org/sdr/C2XA01TY226), Jan 1, 2002: PROXIMITY SWITCH. CRACKED. TYS AT TAKEOFF THE LANDING GEAR/GROUND FAIL MESSAGE INDICATOR CAME ON. CREW RETURNED AND MAINTENANCE REMOVED AND REPLACED THE NLG WOW PROXIMITY SWITCH AND THEN - [SDR C2XA01TY223](https://openairdocs.org/sdr/C2XA01TY223), Dec 30, 2001: FLOORBEAM. CORRODED. TYS, DURING A SCHEDULED 1C INSPECTION, CORROSION WAS FOUND ON SEVERAL AREAS OF THE FORWARD DIGITAL. MAINTENANCE REMOVED FORWARD DIGITAL AND CUT OUT DAMAGED AREA - [SDR C2XA01TY222](https://openairdocs.org/sdr/C2XA01TY222), Dec 30, 2001: LIGHT. BROKEN. TYS, DURING A SCHEDULED 1C INSPECTION, THE NR 6 EMERGENCY TRACK LIGHT WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE NR 6 TRACK LIGHTING IAW EMB-135-AMM - [SDR C2XA01TY221](https://openairdocs.org/sdr/C2XA01TY221), Dec 30, 2001: SWITCH. FAULTY. TYS, During a scheduled 1C inspection, the oxygen deployement on step 13 of task card #35-20-00-770-001-A00 failed. Maintenance removed and replaced the altitud - [SDR C2XA01TY220](https://openairdocs.org/sdr/C2XA01TY220), Dec 30, 2001: ANGLE. CORRODED. TYS DURING A SCHEDULED 1-C INSPECTION CORROSION WAS DETECTED ON CENTER SUPPORT RAMP NEXT TO THE CARBON FIBER CROSSBEAM. MAINTENANCE REMOVED AND REPLACED THE RAM - [SDR C2XA01TY219](https://openairdocs.org/sdr/C2XA01TY219), Dec 30, 2001: ANTENNA. CORRODED. TYS DURING A SCHEDULED 1-C INSPECTION THE LOWER TCAS ANTENNA WAS CORRODED. MAINTENANCE REMOVED AND REPLACED THE TCAS ANTENNA IAW EMB 135 AMM34-43-03, PERFORMED - [SDR C2XA01TY218](https://openairdocs.org/sdr/C2XA01TY218), Dec 30, 2001: BYPASS JACKET. CORRODED. TYS DURING A SCHEDULED 1-C INSPECTION THE NR 1 FANCASE TO BYPASS HAD CORROSION. MAINTENANCE CLEANED UP THE CORROSION. APPLIED CHEMICAL FILM COATING TO THE MAGNE - [SDR C2XA01TY217](https://openairdocs.org/sdr/C2XA01TY217), Dec 30, 2001: RIVET. CORRODED. TYS DURING A SCHEDULED 1-C INSPECTION TWO RIVETS WERE FOUND CORRODED UNDERNEATH THE SERVICE DOOR THRESHOLD. MAINTENANCE REMOVED AND REPLACED THE TWO RIVETS. ALL - [SDR C2XA01TY216](https://openairdocs.org/sdr/C2XA01TY216), Dec 29, 2001: ATTACH FITTING. GOUGED. TYS DURING A SCHEDULED 1-C INSPECTION, NOTED THAT THE LEFT AILERON FITTING WAS GOUGED. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF C-CHECK All 65: https://openairdocs.org/deregistered/N14514-2018-10-30/reports.md ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20040107000729I](https://openairdocs.org/incident/20040107000729I), Jan 7, 2004: Emb EMB135LR (N14514), Houston, TX, Minor damage. (-23) "Industrial incident-no intent to fly" C2XA maintenance employee was taxiing aircraft from the gate for an operation check on the brakes. Upon completion… ## Other aircraft with N14514 - [Cancelled 1973-12-12](https://openairdocs.org/deregistered/N14514-1973-12-12): Beech T-34B, S/N 140925. Owner: [N C Forest Service](https://openairdocs.org/faa-owner/N%20C%20FOREST%20SERVICE), [Raleigh, NC](https://openairdocs.org/faa-place/NC/Raleigh) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.