# N14953: 1998 Embraer EMB-145LR, registration cancelled 2016-02-03 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 3, 2016 - Exported to: Mexico - Status when cancelled: Valid registration - Airframe: [Embraer EMB-145LR](https://openairdocs.org/model/embraer-emb-145lr) (registry code 3260212) - 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: 145071 - Year built: 1998 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: August 3, 1998 - Certificate issued: January 28, 2016 - Last registry action: January 28, 2016 - Mode S code: A0C742 - Owner when cancelled: [Spectre Air Capital LLC](https://openairdocs.org/faa-owner/SPECTRE%20AIR%20CAPITAL%20LLC) - Location: [Horseshoe Bay, TX](https://openairdocs.org/faa-place/TX/Horseshoe%20Bay) - Owner type: Corporation - Owner's area on the map: 30.5258° N, 98.3759° W: Placed by OpenAirDocs at the center of ZIP code 78657, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N14953 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14953 - Page: https://openairdocs.org/deregistered/N14953-2016-02-03 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-145LR: https://openairdocs.org/model/embraer-emb-145lr.md ## Service difficulty reports (72, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASOA20140913278V](https://openairdocs.org/sdr/ASOA20140913278V), Sep 13, 2014: SKIN. DENTED. DURING C-CHECK, REAR FUSELAGE HAS DENT BETWEEN FRAME 77 AND SPLICE BETWEEN STRINGERS 18 - 19R, REPAIRED DENT IAW EC5330-02939. THE ACFT WAS APPROVED FOR RETURN - [SDR ASOA20140911273](https://openairdocs.org/sdr/ASOA20140911273), Sep 11, 2014: FLOOR SUPPORT. CORRODED. DURING C-CHECK, CORROSION FOUND ON OMEGA BEAM NUTPLATE HOLES AT FRAME 59-61. MAINTENANCE R & R CENTER OMEGA BEAM BUTTSTRAP IAW EC5310-01473, REV D. THE ACFT WAS - [SDR ASOA20140909272](https://openairdocs.org/sdr/ASOA20140909272), Sep 9, 2014: BEAM. CORRODED. DURING C-CHECK, CARGO DOOR LOWER CUTOUT CORRODED. R & R CARGO DOOR LOWER CUTOUT IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20140906271](https://openairdocs.org/sdr/ASOA20140906271), Sep 6, 2014: FLOOR SUPPORT. CORRODED. DURING C-CHECK, RT OMEGA BEAM BETWEEN FRAMES 59-61 CORRODED. MAINTENANCE FABRICATED AND INSTALLED REPAIR PARTS ON RT OMEGA BEAM IAW EC5310-01473, REV D. THE ACF - [SDR ASOA20130708100](https://openairdocs.org/sdr/ASOA20130708100), Jul 8, 2013: SKIN. CRACKED. DURING 4A INSPECTION THE LT FUSELAGE 1 SKIN WAS FOUND TO BE CRACKED AT FRAME 75 IN 2 PLACES BELOW STRINGER 1R. MX PERFORMED A DOUBLER REPAIR IAW ENGINEERING CHA - [SDR ASOA20130708099](https://openairdocs.org/sdr/ASOA20130708099), Jul 8, 2013: SKIN. CRACKED. DURING 4A INSPECTION THE REAR FUSELAGE 1 SKIN WAS FOUND TO BE CRACKED AT FRAME 75 BETWEEN STRINGERS 1R AND 2R. MX PERFORMED A DOUBLER REPAIR IAW ENGINEERING CHA - [SDR ASOA20121018153](https://openairdocs.org/sdr/ASOA20121018153), Oct 17, 2012: SKIN. CRACKED. LT WING UPPER SKIN T/E WAS FOUND CRACKED AT THE LT GROUND SPOILER HINGE POINT. CUTOUT THE CRACKED AREA, FABRICATED AND INSTALLED DOUBLER AND TRIPLER. ACFT STILL - [SDR ASOA20121017152](https://openairdocs.org/sdr/ASOA20121017152), Oct 17, 2012: WINDOW FRAME. CORRODED. LEFT & RIGHT WINDSHIELD FRAME HAS CORROSION IN SEVERAL HOLES. REMOVED CORROSION FROM BOLT HOLES AND SOME OF THE HOLES REQUIRED BUSHINGS TO BE INSTALLED IAW ETD2 - [SDR C2XA11IA185](https://openairdocs.org/sdr/C2XA11IA185), Aug 27, 2011: UPLOCK. INOPERATIVE. IAH - FLIGHT 2174, THE CREW REPORTED THAT THE LEFT MAIN LANDING GEAR INDICATION WAS SHOWING DASHES OF YELLOW AND GREEN, AND ALTERNATING BACK AND FORTH. THE AIRC - [SDR C2XA11CL157](https://openairdocs.org/sdr/C2XA11CL157), Jun 27, 2011: INVERTER. FAULTY. GRR FLT 2904 THE CREW REPORTED THE OVERWING CEILING EXIT LIGHT DID NOT TEST. MAINTENANCE INSPECTED AND REPLACED THE NR 4 EMERGENCY LIGHT INVERTER. OPERATIONAL C - [SDR C2XA11RI113](https://openairdocs.org/sdr/C2XA11RI113), Jun 20, 2011: CONTROLLER. INOPERATIVE. FLIGHT 2287 - EWR - FLIGHT CREW REPORTED THAT, EN ROUTE FROM EWR TO CMH, FMS FAILED, BOTH PFD'S AND NAVS ALSO WENT OUT. CREW PERFORMED AIR RETURN AND LANDED UNE - [SDR C2XA11TY028](https://openairdocs.org/sdr/C2XA11TY028), Mar 15, 2011: SHIM. WORN. TYS - A/C WAS TAXI FOR TAKEOFF AND IN CLIMBOUT, WHEN GEAR STOWED, CREW REPORTED A RATTLING NOISE WHEN GEAR STOWED. A/C WAS FERRIED TO TYS FROM BNA WHERE MAINTEN - [SDR C2XA10SH372](https://openairdocs.org/sdr/C2XA10SH372), Oct 29, 2010: FITTING. CRACKED. SHV - DURING C-CHECK NR 1 ENGINE FORWARD LOWER YOKE FORWARD FLANGE CRACKED. MAINTENANCE REMOVED AND REPLACED NR1 ENGINE FORWARD LOWER YOKE FITTING IAW EC5450-01 - [SDR C2XA10SH371](https://openairdocs.org/sdr/C2XA10SH371), Oct 29, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM L-FLANGE AT FRAME 38 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM L-FLANGE AT FRAME 38 IAW EM - [SDR C2XA10SH370](https://openairdocs.org/sdr/C2XA10SH370), Oct 29, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM L-FLANGE BETWEEN FRAME 43-44 HAS CORROSION. MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM L-FLANGE BETWEEN FRAME 43-44 IAW EM - [SDR C2XA10SH369](https://openairdocs.org/sdr/C2XA10SH369), Oct 29, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK CENTER OMEGA BEAM L-FLANGE BETWEEN FRAME 43-44 HAS CORROSION. MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM L-FLANGE BETWEEN FRAME 43-4 - [SDR C2XA10SH368](https://openairdocs.org/sdr/C2XA10SH368), Oct 29, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM L-FLANGE BETWEEN FRAME 49-50 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM L-FLANGE BETWEEN FR - [SDR C2XA10SH367](https://openairdocs.org/sdr/C2XA10SH367), Oct 29, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK CENTER OMEGA BEAM L-FLANGE BETWEEN FRAME 49-50 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM L-FLANGE BE - [SDR C2XA10SH366](https://openairdocs.org/sdr/C2XA10SH366), Oct 29, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM L-FLANGE AT FRAME 54 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM L-FLANGE AT FRAME 54 REPAIR - [SDR C2XA10SH365](https://openairdocs.org/sdr/C2XA10SH365), Oct 29, 2010: FRAME. CORRODED. SHV - DURING C-CHECK CORROSION (LEVEL 2 LOCAL) ON FRAME 65 STRINGER 16L-17L. MAINTENANCE PERFORMED REPAIR ON FRAME 65 STRINGER 16L-17L IAW EMB-145 EC5310-01529. - [SDR C2XA10SH364](https://openairdocs.org/sdr/C2XA10SH364), Oct 29, 2010: FITTING. CORRODED. SHV - DURING C-CHECK CORROSION (LEVEL 2 LOCAL) ON SHEAR CLIP FRAME 65 STRINGER 16L-17L. MAINTENANCE PERFORMED REPAIR ON SHEAR CLIP FRAME 65 STRINGER 16L-17L IAW - [SDR C2XA10CL096](https://openairdocs.org/sdr/C2XA10CL096), Jun 14, 2010: PROXIMITY SWITCH. OUT OF ADJUST. CLE FLT 2632 - THE CREW REPORTED AN AIR/GROUND FAIL MESSAGE. MAINTENANCE INSPECTED AND COULD NOT DUPLICATE BUT CHANGED THE LGEU, ADJUSTED 1 PROXIMITY SWITCH ON - [SDR C2XA10RI002](https://openairdocs.org/sdr/C2XA10RI002), Jan 5, 2010: CHARGER. DEFECTIVE. FLIGHT 2531 - EWR - FLIGHT CREW REPORTED EMERGENCY LIGHT WOULD NOT TURN OFF. EWR MX REMOVED AND REPLACED NR 2 BATTERY CHARGER ASSY AND PERFORMED OPERATIONAL CHE - [SDR C2XA09TY265](https://openairdocs.org/sdr/C2XA09TY265), Oct 27, 2009: BATTERY. DISCHARGED. TYS - A/C WAS IN FOR A SERVICE CHECK WHEN INSPECTION FOUND THE AED DEFIBRILLATOR BATTERY INOP. MAINTENANCE REMOVED AND REPLACED THE AED DEFIBRILLATOR BATTERY IA - [SDR C2XA09IA263](https://openairdocs.org/sdr/C2XA09IA263), Oct 14, 2009: INVERTER. INOPERATIVE. MCI - DURING MAINTENANCE INSPECTION THE NUMBER FOUR AND FIVE AISLE PATH LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER F - [SDR C2XA09RI148](https://openairdocs.org/sdr/C2XA09RI148), Aug 19, 2009: ALTIMETER. MALFUNCTIONED. FLIGHT 2790 - EWR - DURING DESCENT, FLIGHT CREW REPORTED AN AMBER INDICATION FOR RADIO ALTIMETER ON PFD WITH LANDING GEAR AURAL SOUND FOR 5 SECONDS THEN CLEARED - [SDR C2XA09TY107](https://openairdocs.org/sdr/C2XA09TY107), Jun 16, 2009: PROXIMITY SWITCH. BROKEN. TYS - AIRCRAFT WAS EN ROUTE TO IAH FROM EWR WITH A STOP AT TYS, WHEN LEAVING TYS THE LDG WOULDN'T RETRACT SO CREW RETURN TO BASE. MAINTENANCE REMOVED AND REPLAC - [SDR C2XA09TY106](https://openairdocs.org/sdr/C2XA09TY106), Jun 16, 2009: BULB. FAILED. ACFT IN OVERNIGHT FOR A 2A CHECK, WHEN INSP FOUND THE RT OVERWING EMERGENCY LIGHT INOP. MX REMOVED AND REPLACED THE THE BULB FOR THE LIGHT IAW AMM 33-50-07, OPS - [SDR C2XA09RI043](https://openairdocs.org/sdr/C2XA09RI043), Mar 20, 2009: POWER SUPPLY. DISCHARGED. FLIGHT 2996 - EWR - FLIGHT CREW REPORTED FORWARD EMERGENCY LIGHT INOPERATIVE ABOVE F/A SEAT. EWR MX REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY AND PERFOR - [SDR C2XA08CL101](https://openairdocs.org/sdr/C2XA08CL101), Aug 27, 2008: WARNING SYSTEM. ACTIVATED. DSM FLIGHT NR 2636 THE CREW REPORTED A FUEL 1 LOW LEVEL MSG IN FLIGHT. THE FLIGHT DIVERTED IN DSM AND LANDED WITHOUT INCIDENT. THE FUEL QUANTITY INDICATOR WAS A - [SDR C2XA08RI084](https://openairdocs.org/sdr/C2XA08RI084), Jun 13, 2008: HANDLE. UNSECURE. FLIGHT 2807 - EWR - FLIGHT CREW REPORTED MAIN CABIN DOOR WOULD NOT OPEN OR CLOSE FROM INSIDE. EWR MAINTENANCE SECURED MAIN CABIN DOOR HANDLE AND PERFORMED OPERA - [SDR C2XA08IA044](https://openairdocs.org/sdr/C2XA08IA044), Jan 29, 2008: SKIN. CRACKED. IAH - DURING PREFLIGHT INSPECTION THE RIGHT WING SKIN WAS FOUND TO BE CRACKED AT THE CENTER HINGE POINT CUTOUT FOR THE GROUND SPOILER. MAINTENANCE INSPECTED THE - [SDR C2XA08IA029](https://openairdocs.org/sdr/C2XA08IA029), Jan 17, 2008: FUSE. BLOWN. IAH - FLIGHT 2099 DURING PREFLIGHT INSPECTION SOME EMERGENCY LIGHTS WERE INOP. MAINTENANCE REMOVED AND REPLACED A FUSE, OPERATIONALLY CHECKED WITH NO DEFECTS, A - [SDR C2XA07TY065](https://openairdocs.org/sdr/C2XA07TY065), Oct 31, 2007: HANDLE. FAILED. LANDING GEAR FAILED TO RETRACT. REPLACED LANDING GEAR HANDLE IAW EMB 145 MM 32-32-02, OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE. - [SDR C2XA07CL092](https://openairdocs.org/sdr/C2XA07CL092), Oct 30, 2007: COMPUTER. SHORTED. CLEVELAND MAINTENANCE REPORTED THE GUIDANCE CONTROL UNIT (GC-550) HAD SMOKE COMING FROM IT. MAINTENANCE INSPECTED AND REPLACED THE GUIDANCE CONTROL COMPUTER. OP - [SDR C2XA07TY060](https://openairdocs.org/sdr/C2XA07TY060), Oct 15, 2007: DOUBLER. MISSING. TYS - A/C WAS FOUND WITH A NUT PLATE MISSING AND THE HOLE ELONGATED ON THE RUDDER 2. MAINTENANCE FABRICATED A FILLER AND A INTERNAL DOUBLER. ALODINED AND EPOXY - [SDR C2XA07RI052](https://openairdocs.org/sdr/C2XA07RI052), Jul 3, 2007: LIGHT. MALFUNCTIONED. FLT 2774 - DAY - CREW REPORTED MAIN CABIN DOOR EMERGENCY LIGHT INOPERATIVE. DAY MX RECYCLED BATTERY SWITCHES AND PERFORMED OPERATIONAL TEST SUCCESSFULLY. ACFT W - [SDR C2XA07IA047](https://openairdocs.org/sdr/C2XA07IA047), Feb 26, 2007: LIGHT. MALFUNCTIONED. IAH - FLT NR 3116, DURING A TEST THE EMERGENCY EXIT LIGHTING FAILED TO ILLUMINATE. MAINTENANCE RESET THE EMERGENCY LIGHTING SYSTEM AND OPERATIONALLY TESTED THE - [SDR C2XA06IA141](https://openairdocs.org/sdr/C2XA06IA141), Aug 27, 2006: WIRE. LOOSE. IAH - DURING A-CHECK INSPECTION, THE EMERGENCY EXIT LIGHT ABOVE THE F/A SEAT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED THE SIGN, RE-SECURED THE CONNECTOR - [SDR C2XA06IA053](https://openairdocs.org/sdr/C2XA06IA053), Apr 1, 2006: ACM. OVERHEATED. FLT 2862 - CREW REPORTED SMOKE IN THE CABIN AFTER REACHING 10,000 FT CLIMBOUT. THE AIRCRAFT LANDED AT IAH WHERE MAINTENANCE FOUND THE NR 2 ACM TO BE OVERHEATING - [SDR C2XA05TY004](https://openairdocs.org/sdr/C2XA05TY004), Jan 13, 2005: FITTING. CORRODED. TYS, DURING A SCHEDULED INSPECTION, THE VERTICAL STAB TO FUSELAGE FITTING ATTACH BRACKET WAS FOUND FRETTING ON SKIN AT FRAME 75. MAINTENANCE REMOVED THE STAB FI - [SDR C2XA05TY003](https://openairdocs.org/sdr/C2XA05TY003), Jan 13, 2005: SILL. CORRODED. TYS, DURING A SCHEDULED INSPECTION THE SERVICE DOOR SILL WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE DOOR SILL IAW EMB-145-AMM-21-31-00 / 135/145 S - [SDR C2XA05TY002](https://openairdocs.org/sdr/C2XA05TY002), Jan 4, 2005: HINGE. WORN. DURING A 4C INSPECTION THE RT AND LT VERTICAL STABLIZER SPHERICAL BEARING HOUSINGS WERE FOUND WORN. MAINTENANCE REAM AND INSTALL NEW BUSHINGS IAW EC5510-01107. - [SDR C2XA04BT110](https://openairdocs.org/sdr/C2XA04BT110), Oct 17, 2004: BATTERY. INOPERATIVE. BTV, DURING SERVICE AND ROUTINE CHECK ON RON, MAINTENANCE FOUND THE PASSENGER DOOR EMERGENCY LIGHT TO BE INOPERATIVE. REMOVED AND REPLACED NR 1 EMERGENCY LIGHT - [SDR C2XA04CL044](https://openairdocs.org/sdr/C2XA04CL044), Apr 28, 2004: CONTROLLER. FAILED. BTV FLIGHT NR 2441 THE CREW REPORTED SMOKE COMING FROM THE DIGITAL PRESSURE CONTROLLER. MAINTENANCE REPLACED THE DIGITAL PRESSURE CONTROLLER. OPERATIONAL CHECKS - [SDR C2XA03IA105](https://openairdocs.org/sdr/C2XA03IA105), Nov 20, 2003: LAMP. LOOSE. DURING SCHEDULED MAINTENANCE THE LEFT AFT EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND RE-SECURED THE LAMP IN THE LIGHT FIXTURE - [SDR C2XA03BT064](https://openairdocs.org/sdr/C2XA03BT064), Jun 6, 2003: BULB. BURNED OUT. DURING 3A INSPECTION MAINTENANCE FOUND PASSENGER DOOR EMERGENCY LIGHT TO BE INOPERATIVE. REMOVED AND REPLACED PASSENGER DOOR EMERGENCY LIGHT BULB IAW EMB145 AMM - [SDR C2XA03SH082](https://openairdocs.org/sdr/C2XA03SH082), Mar 31, 2003: SILL. CORRODED. DURING C-CHECK FOWARD SILL HAS CORROSION BETWEEN FRAMES 18 AND 20. MAINTENANCE REMOVED DAMAGE AND MADE A DOUBLER REPAIR ON AFFECTED SILL IAW EMB 145 SRM 53-21-0 - [SDR C2XA03SH081](https://openairdocs.org/sdr/C2XA03SH081), Mar 31, 2003: SKIN. GOUGED. DURING C-CHECK SKIN WAS FOUND GOUGED UNDER GPU ACCESS PANEL BETWEEN FRAMES 6 AND 8. MAINTENACE REMOVED DAMAGE AND REPAIRED SKIN IAW EMB 145 SRM 53-11-01. THE AI - [SDR C2XA03SH080](https://openairdocs.org/sdr/C2XA03SH080), Mar 31, 2003: SUPPORT. CORRODED. DURING C-CHECK THE SUPPORT PLATE BETWEEN LT OMEGA BEAM AND LT SILL WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 60 AND 61. MAINTENANCE REMOVED AND REPLACED THE AF All 72: https://openairdocs.org/deregistered/N14953-2016-02-03/reports.md ## FAA accident and incident reports (2) 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 20030110007349I](https://openairdocs.org/incident/20030110007349I), Jan 10, 2003: Emb EMB145LR (N14953), Knoxville, TN. (-23) After departure, smoke started entering the cabin. Aircraft returned to tys and passengers were evacuated. Maintenance determined that deice fluid had… - [Incident 19991017029309I](https://openairdocs.org/incident/19991017029309I), Oct 17, 1999: Emb EMB145LR (N14953), Kansas City, MO, Minor damage. (-23) On October 17, 1999, Continental express airline, flight 4108, an Emb-145LR, was enroute from mci to cle, when a smoke warning indication was noted in… ## Other aircraft with N14953 - [Cancelled 1939-06-05](https://openairdocs.org/deregistered/N14953-1939-06-05): Ryan Aeronautical ST-A, S/N 109. Owner: [Browne Walter Jay](https://openairdocs.org/faa-owner/BROWNE%20WALTER%20JAY), [Sacramento, CA](https://openairdocs.org/faa-place/CA/Sacramento) --- 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.