# N13968: 1999 Embraer EMB-145LR, registration cancelled 2016-03-01 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 1, 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 AE3007C series](https://openairdocs.org/engine/allison-ae3007c-series) (registry code 03028) - Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (OpenAirDocs) - Serial number: 145138 - Year built: 1999 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 4, 1999 - Certificate issued: February 18, 2016 - Last registry action: February 18, 2016 - Mode S code: A09FEB - 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/N13968 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=13968 - Page: https://openairdocs.org/deregistered/N13968-2016-03-01 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 (57, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASOA20140503083](https://openairdocs.org/sdr/ASOA20140503083), May 3, 2014: YOKE. CRACKED. DURING C-CHECK INSPECTION, FOUND THE NR 1 ENGINE LOWER YOLK FITTING CRACKED AND VERIFIED BY NDT METHODS. MAINTENANCE R & R THE ENGINE YOKE IAW EC 5450-010073B. - [SDR ASOA20131209136R](https://openairdocs.org/sdr/ASOA20131209136R), Dec 9, 2013: BATTERY PACK. DISCHARGED. GALLEY SERVICE DOOR EMERGENCY LIGHT REPORTED NOT TO BE ILLUMINATING. MX R & R NR 2 EMERGENCY LIGHT BATTERY AND SIGN WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED - [SDR ASOA20121020096R](https://openairdocs.org/sdr/ASOA20121020096R), Oct 20, 2012: UNKNOWN. ODOR. PASSENGERS REPORTED ELECTRICAL BURNING ODOR COMING FROM VENTS AROUND ROWS 3,4,5 AND 6. MX PERFORMED SUCCESSFUL OPS CHECK OF BOTH PACKS RUNNING WITH NO EVIDENCE - [SDR ASOA20120613085](https://openairdocs.org/sdr/ASOA20120613085), Jun 13, 2012: INVERTER. INOPERATIVE. DURING ROUTINE CHECK, MX REPORTED THE EXIT SIGN AT SEAT 12A TO BE INOPERATIVE. MX R & R THE INVERTER FOR AFFECTED EMERGENCY LIGHT, OPS TESTED WITH NO DEFECTS, A - [SDR ASOA20120404028](https://openairdocs.org/sdr/ASOA20120404028), Apr 4, 2012: INVERTER. INOPERATIVE. DURING SCHEDULED MX INSPECTION, AFT CABIN FLOOR PATHWAY EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. R & R THE NR 6 INVERTER IAW AMM 33-50-11 WITH OPS CHECKED S - [SDR C2XA11CL239](https://openairdocs.org/sdr/C2XA11CL239), Oct 30, 2011: SWITCH. FAULTY. BNA FLT 5955 THE CREW REPORTED THE NR 1 BLEED VALVE WOULD NOT OPEN DURING FLIGHT. CLOSED INDICATION ON THE EICAS. THE AIRCRAFT RETURNED TO BNA AND LANDED WITHOU - [SDR C2XA11TY166](https://openairdocs.org/sdr/C2XA11TY166), Oct 29, 2011: RELAY. BROKEN. TYS FOR BNA A/C ON CLIMBOUT HAD A EICIAS WITH A MESSAGE THAT THE NR 1 BLEED VALVE WAS CLOSED IN FLIGHT. THE CREW RETURNED TO BNA AND SWAPPED A/C. MAINTENANCE RE - [SDR C2XA11IA191](https://openairdocs.org/sdr/C2XA11IA191), Aug 31, 2011: ENGINE. VIBRATION. DURING CLIMB THE CREW REPORTED A ENGINE ONE HIGH VIBRATION. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE - [SDR C2XA11TY063](https://openairdocs.org/sdr/C2XA11TY063), May 23, 2011: PROXIMITY SENSOR. CRACKED. TYS - A/C WAS FERRIED FROM ATL TO TYS FOR A SPOILER FAIL MESSAGE AND CIRCUIT BREAKER POP. MAINTENANCE REMOVED AND REPLACED THE LEFT SPEED BRAKE PROX SENSOR IAW - [SDR C2XA11IA082](https://openairdocs.org/sdr/C2XA11IA082), May 5, 2011: HYDRAULIC LINE. RUPTURED. IAH - FLIGHT 2044, THE CREW REPORTED THE NUMBER TWO HYDRAULIC SYSTEM HAD A LOW QUANTITY FOLLOWED BY A NR 2 ENGINE DRIVEN HYDRAULIC PUMP FAILURE. THE AIRCRAFT RE - [SDR C2XA11RI054](https://openairdocs.org/sdr/C2XA11RI054), Apr 16, 2011: UNKNOWN. ODOR. FLIGHT 3064 - EWR - FLIGHT CREW REPORTED POSSIBLE LIGHTNING STRIKE - CLICKING SOUND IN CEILING AND BURNING SMELL TEMPORARELY. EWR MX PERFORMED LIGHTNING STRIKE - [SDR C2XA10SH265](https://openairdocs.org/sdr/C2XA10SH265), Aug 11, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 29. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53 - [SDR C2XA10SH264](https://openairdocs.org/sdr/C2XA10SH264), Aug 11, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 37-38. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW E - [SDR C2XA10SH263](https://openairdocs.org/sdr/C2XA10SH263), Aug 11, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53 - [SDR C2XA10SH262](https://openairdocs.org/sdr/C2XA10SH262), Aug 11, 2010: SKIN. CORRODED. SHV - DURING C-CHECK THE LOWER SKIN WAS FOUND TO BE CORRODED BETWEEN FRAMES 62-63 AND STRINGERS 20-21R. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLE - [SDR C2XA10SH261](https://openairdocs.org/sdr/C2XA10SH261), Aug 11, 2010: SKIN. CRACKED. SHV - DURING C-CHECK THE LT AFT SKIN WAS FOUND TO BE CRACKED AROUND A FASTENER AT FRAME 75, STRINGER 2L. MAINTENANCE REMOVED THE CRACK AND PERFORMED A BUSHING R - [SDR C2XA09IA251](https://openairdocs.org/sdr/C2XA09IA251), Oct 5, 2009: SKIN. CRACKED. IAH - DURING MAINTENANCE INSPECTION THE CROWN SKIN PANEL WAS FOUND TO HAVE A 55MM CRACK ON THE LOWER LEG BETWEEN THE CAPTAINS WINDSHIELD AND DV WINDOW. MAINTENA - [SDR C2XA09CL113](https://openairdocs.org/sdr/C2XA09CL113), Sep 12, 2009: ACTUATOR. FAULTY. CLE - FLT 2861 - THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON THE EICAS WHEN THE GEAR WAS SELECTED DOWN AND THEN CLEARED ONCE THE GEAR WAS DOWN. - [SDR C2XA08CL117](https://openairdocs.org/sdr/C2XA08CL117), Oct 17, 2008: OIL SYSTEM. FLUCTUATES. EWR FLIGHT NR 2142 THE CREW REPORTED DURING TAKEOFF ROLL AND INITIAL CLIMBOUT THE OIL PRESSURE REMAINED ABOVE 115 PSI FOR 2 MIN ON THE NR 1 ENGINE. ALSO BELOW 1 - [SDR C2XA08CL102](https://openairdocs.org/sdr/C2XA08CL102), Aug 31, 2008: WIRE HARNESS. DEFECTIVE. CLE FLIGHT NR 2320 THE CREW REPORTED AN AIR/GROUND FAIL MESSAGE IN FLIGHT. THE GEAR WOULD NOT RETRACT. THE ACFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MX - [SDR C2XA08RI088](https://openairdocs.org/sdr/C2XA08RI088), Jun 15, 2008: SOLENOID VALVE. DEFECTIVE. FLIGHT 3001 - EWR - FLIGHT CREW REPORTED THAT IT SOUNDED LIKE LANDING GEAR DOORS OPEN IN FLIGHT. EWR MAINTENANCE REMOVED AND REPLACED NOSE LANDING GEAR DOOR SOL - [SDR C2XA08SH075](https://openairdocs.org/sdr/C2XA08SH075), May 14, 2008: SUPPORT. CRACKED. SHV - DURING C-CHECK PAX DOOR INTERNAL HANDLE SUPPORT CRACKED. MX REMOVED AND REPLACED PAX DOOR INTERNAL HANDLE SUPPORT IAW EMB SRM 51-40-02. THE AIRCRAFT WAS A - [SDR C2XA08SH074](https://openairdocs.org/sdr/C2XA08SH074), May 13, 2008: SUPPORT BRACKET. CORRODED. SHV - DURING C-CHECK WASTE DRAIN SUPPORT CORRODED INSIDE AIRCRAFT. MX REMOVED AND REPLACED WASTE DRAIN DUMP VALVE SUPPORT ASSY IAW EMB 145SRM 51-40-02. THE AIRC - [SDR C2XA08SHO76](https://openairdocs.org/sdr/C2XA08SHO76), Apr 14, 2008: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LEFT OMEGA BEAM REPAIR AT FR 20 IS CORRODED. MX REMOVED AND REPLACED PREVIOUS REPAIR ON LEFT OMEGA BEAM AT FR 20 IAW EMB 145 SRM 51-40-02. - [SDR C2XA08CL018](https://openairdocs.org/sdr/C2XA08CL018), Feb 3, 2008: INVERTER. INOPERATIVE. DURING ROUTINE MAINTENANCE, THE EXIT MARKER LIGHT AT ROW 3 BC WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT INVERTER. OPERATIONA - [SDR C2XA07IA228](https://openairdocs.org/sdr/C2XA07IA228), Oct 30, 2007: BATTERY PACK. INOPERATIVE. IAH - FLIGHT 2618, DURING PREFLIGHT INSPECTION THE CREW REPORTED THE CENTER AISLE PATH EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE - [SDR C2XA07IA190](https://openairdocs.org/sdr/C2XA07IA190), Aug 30, 2007: ENGINE. MALFUNCTIONED. ATL - FLIGHT 3067, THE CREW REPORTED LAV SMOKE WARNING & HAZE IN CABIN DURING FLIGHT. DIVERTED TO ATL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE OPS CHECK NR - [SDR C2XA07IA072](https://openairdocs.org/sdr/C2XA07IA072), Mar 24, 2007: LIGHT. INOPERATIVE. IAH FLIGHT 2305, DURING POST FLIGHT INSPECTION THE CREW REPORTED THAT THE LAST ROW OF AISLE PATH LIGHTING WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE - [SDR C2XA07IA064](https://openairdocs.org/sdr/C2XA07IA064), Mar 15, 2007: ACM. FROZEN. IAH - FLIGHT 2082, DURING TAKEOFF ROLL, THE CREW REPORTED A STRONG SMOKE ODOR INVADED THE CABIN AND FLIGHT DECK. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GA - [SDR C2XA06IA114](https://openairdocs.org/sdr/C2XA06IA114), Jul 19, 2006: SMOKE. DETECTED. THE CREW REPORTED SMOKE IN THE COCKPIT AND MOISTURE IN THE LINES. MAINTENANCE INSPECTED THE AIRCRAFT AND OPERATIONALLY CHECKED BOTH PACKS WITH NO DEFECTS NOTED. - [SDR C2XA06TY035](https://openairdocs.org/sdr/C2XA06TY035), Jun 12, 2006: LIGHT. BURNED. CLT, FLIGHT ATTENDANT REPORTED SMOKE IN CABIN, ELECTRICAL ODOR, CREW DID AN AIR RETURN, OVERWEIGHT LANDING, NORMAL LANDING AND ROLL OUT. MAINTENANCE FOUND SOURC - [SDR C2XA05BT063](https://openairdocs.org/sdr/C2XA05BT063), Aug 20, 2005: SIGN. FAULTY. DURING 5A INSPECTION, MAINTENANCE FOUND THE AFT GALLEY EMERGENCY EXIT SIGN FAULTY. REMOVED AND REPLACED EMERGENCY EXIT SIGN IAW EMB145 AMM 33-50-14. OPS CHECKED - [SDR C2XA04TY108](https://openairdocs.org/sdr/C2XA04TY108), Jul 1, 2004: BUSHING. CORRODED. DURING A SCHEDULED 3C INSPECTION MAINT FOUND CORRODED BUSHING ON ALL RUDDER 2 HINGE POINTS. MAINT REMOVED AND REPLACED ALL OF THE HINGE POINT BUSHINGS IAW EMB 2 - [SDR C2XA04TY107](https://openairdocs.org/sdr/C2XA04TY107), Jul 1, 2004: BRACKET. CORRODED. DURING A SCHEDULED 3C INSPECTION CORROSION WAS FOUND ON THE SINK DRAIN BRACKETS. MAINT REMOVED THE SINK BRACKETS, FAB A NEW PART, ALODINED, PRIMED AND PAINTED A - [SDR C2XA04TY106](https://openairdocs.org/sdr/C2XA04TY106), Jul 1, 2004: FLOORBEAM. CORRODED. DURING A SCHEDULED 3C INSPECTION THE LEFT INBD FLOOR SUPPORT WAS FOUND CORRODED AT BOTTOM OF RAMP IN GALLEY. MAINT CUT OUT DAMAGE AND FAB A NEW REPAIR FOR THE E - [SDR C2XA04TY105](https://openairdocs.org/sdr/C2XA04TY105), Jul 1, 2004: FRAME. GOUGED. DURING A SCHEDULED 3C INSPECTION THE BOTTOM OF THE APU FIREWALL HAD A GOUGE. MAINT FOUND THE GOUGES TO BE ON FR 81, BLENDED DYE PEEN GOUGE AREA, REMOVED RIVETS, - [SDR C2XA04TY104](https://openairdocs.org/sdr/C2XA04TY104), Jul 1, 2004: FLOORBEAM. CORRODED. DURING A SCHEDULED 3C INSPECTION, CORROSION WAS FOUND ON THE RIGHT LAV FLOORBEAM TOP CAP IN SEVERAL PLACES. MAINT REMOVED AND REPLACED THE RIGHT TOP CAP IAW EMB - [SDR C2XA04TY103](https://openairdocs.org/sdr/C2XA04TY103), Jul 1, 2004: FLOOR SUPPORT. CORRODED. DURING A SCHEDULED 3C INSPECTION CORROSION WAS FOUND ON LEFT SIDE LAV FLANGE. MAINT REMOVED AND REPLACED THE FLOOR SUPPORT FLANGE IAW EMB 135/145 SRM 51-40-02. - [SDR C2XA04TY102](https://openairdocs.org/sdr/C2XA04TY102), Jul 1, 2004: SILL. CORRODED. DURING A SCHEDULED 3C INSPECTION THE PAX DOOR SILL WAS FOUND CORRODED. MAINT REMOVED AND REPLACED THE DOOR SILL IAW EMB 135/145 SRM 51-40-02; 03 AND EMB CPM51-2 - [SDR C2XA04TY094](https://openairdocs.org/sdr/C2XA04TY094), Jun 23, 2004: GUSSET. CORRODED. DURING A SCHEDULED 3C INSPECTION FR 22 GUSSET CAP WAS FOUND CORRODED AROUND THE RIVETS. REMOVED FR 22 GUSSET CAP, FAB A NEW CAP, ALODINED, PRIMED AND PAINTED. T - [SDR C2XA04TY098](https://openairdocs.org/sdr/C2XA04TY098), Jun 22, 2004: FLOORBEAM. CORRODED. DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER OMEGA BEAM AT FRAME 16. MAINTENANCE REMOVED AND REPLACED THE CENTER OMEGA BEAM IAW EMB SRM 51-40 - [SDR C2XA04TY097](https://openairdocs.org/sdr/C2XA04TY097), Jun 21, 2004: ANGLE. CORRODED. DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE RAMP ANGLE UNDER THE CARBON FIBER BEAM AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE CENTER RAMP AN - [SDR C2XA04TY096](https://openairdocs.org/sdr/C2XA04TY096), Jun 21, 2004: ANGLE. CORRODED. DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE RAMP ANGLE AND AFT NUT PLATE OF THE CENTER TOP CAP UNDER THE GALLEY FLOOR. MAINTENANCE REMOVED AND REPL - [SDR C2XA03CL197](https://openairdocs.org/sdr/C2XA03CL197), Dec 5, 2003: FAN. SEIZED. CLE FLIGHT NR 2123) THE CREW REPORTED A VERY STRONG SMELL OF SMOKE FROM CABIN ON APPROACH. TURNED OFF NR 2 PACK AND SMELL DISSIPATED. AIRCRAFT LANDED WITHOUT FU - [SDR C2XA03CL194](https://openairdocs.org/sdr/C2XA03CL194), Nov 29, 2003: SMOKE. DETECTED. CLE) FLIGHT NR 3230, THE CREW REPORTED THE COCKPIT AND CABIN FILLED WITH SMOKE ON DESCENT INTO CLEVELAND.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENAN - [SDR C2XA03CL171](https://openairdocs.org/sdr/C2XA03CL171), Oct 1, 2003: ENGINE. FAILED. STL FLIGHT NR 2368 THE CREW REPORTED THE NR 1 ENGINE UNCOMMANDED SHUT DOWN ON APPROACH INTO STL.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLAC - [SDR C2XA03TY043](https://openairdocs.org/sdr/C2XA03TY043), Mar 28, 2003: PROXIMITY SWITCH. OUT OF ADJUST. DURING CLIMB RECEIVED A ICAS MESSAGE OF LDG AIR/GND FAIL AT ROTATION. LANDING GEAR WOULDN'T RETRACT. AIR RETURN AND MAINT FOUND PROX SWITCHES OUT OF ADJUSTMENT. - [SDR C2XA03BT037](https://openairdocs.org/sdr/C2XA03BT037), Mar 13, 2003: APU. SEIZED. EWR FLT2578 CREW REPORTED DURING APU START APU FAILED INDICATION WAS INSTRUCTED I HAD A FIRE BLEW EXTINGUISHER BOTTLE. MX FOUND APU SIEZED INSPECTED AND PLACED - [SDR C2XA02SH042](https://openairdocs.org/sdr/C2XA02SH042), Aug 6, 2002: SILL. CORRODED. SHV- DURING C-CHECK INSPECTION, FRAME 18-19 RIGHT HAND OUTBOARD SILL FORWARD OF SERVICE DOOR HAD THREE AREAS OF CORROSION. MAINTENANCE REMOVED AND REPLACED THE - [SDR C2XA02SH041](https://openairdocs.org/sdr/C2XA02SH041), Aug 6, 2002: SILL. CORRODED. SHV- DURING C-CHECK INSPECTION, FRAME 22 RIGHT HAND OUTBOARD SILL AFT OF SERVICE DOOR WAS FOUND TO HAVE FOUR AREAS OF CORROSION. MAINTENANCE OUT OF LIMITS RIGHT All 57: https://openairdocs.org/deregistered/N13968-2016-03-01/reports.md ## Other aircraft with N13968 - [Cancelled 1971-06-16](https://openairdocs.org/deregistered/N13968-1971-06-16): Piper PA-23-250 (6PCLM), S/N 27-4583. Exported to Singapore. Owner: [Moody Walter](https://openairdocs.org/faa-owner/MOODY%20WALTER), [Lock Haven, PA](https://openairdocs.org/faa-place/PA/Lock%20Haven) --- 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.