# N13994: 2000 Embraer EMB-145LR, registration cancelled 2021-04-21 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: April 21, 2021 - 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: 145291 - Year built: 2000 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: July 21, 2000 - Certificate issued: June 6, 2017 - Last registry action: February 10, 2020 - Mode S code: A0A050 - Owner when cancelled: [Southern Aircraft Consultancy Inc Trustee](https://openairdocs.org/faa-owner/SOUTHERN%20AIRCRAFT%20CONSULTANCY%20INC%20TRUSTEE) - Location: Bungay Norfolk, United Kingdom - Owner type: Corporation - The mark today: https://openairdocs.org/aircraft/N13994 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=13994 - Page: https://openairdocs.org/deregistered/N13994-2021-04-21 From the FAA registry file of November 7, 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 (62, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASOA20150326030H](https://openairdocs.org/sdr/ASOA20150326030H), Mar 26, 2015: BATTERY PACK. INOPERATIVE. DURING MAINTENANCE INSPECTION THE EMERGENCY LIGHT IN THE COCKPIT CEILING AND 1ST EMERGENCY LIGHT IN CABIN CEILING WERE FOUND TO BE INOPERATIVE. MAINTENANCE R & - [SDR ASOA20150326029H](https://openairdocs.org/sdr/ASOA20150326029H), Mar 26, 2015: CHARGER. INOPERATIVE. DURING MAINTENANCE INSPECTION, THE EMERGENCY LIGHT IN THE COCKPIT CEILING AND 1ST EMERGENCY LIGHT IN CABIN CEILING WERE FOUND TO BE INOPERATIVE. MAINTENANCE R & - [SDR ASOA20150223021H](https://openairdocs.org/sdr/ASOA20150223021H), Feb 23, 2015: LIGHT. BURNED. THE CREW REPORTED A BURNING SMELL COMING FROM THE SIDEWALL LIGHTS NEAR 5D WITH SPARKING WIRE OBSERVED. MAINTENANCE R & R THE LIGHT ASSY AT SEAT 5D, OPERATIONALL - [SDR ASOA20150128008](https://openairdocs.org/sdr/ASOA20150128008), Jan 28, 2015: LIGHT. SMOKE. THE CREW REPORTED SMOKE IN CABIN COMING FROM VICINITY OF SEAT 4A. MAINTENANCE INSPECTED AND REPLACED SEAT 4A SIDEWALL CABIN LIGHT ASSY. OPS CHECKS WERE GOOD. - [SDR ASOA20141119094](https://openairdocs.org/sdr/ASOA20141119094), Nov 19, 2014: VALVE. LEAKING. THE CREW REPORTED LT WING TANK VENTED 100 LBS FUEL DURING CLIMB-OUT WITH WINGS LEVEL. MAINTENANCE INSPECTED AND REPLACED THE FUEL TANK FLAP VALVE. OPS CHECKS WE - [SDR ASOA20141107125](https://openairdocs.org/sdr/ASOA20141107125), Nov 7, 2014: SMOKE DETECTOR. FAULTY. A BAGGAGE SMOKE INDICATION WAS REPORTED BY THE CREW AFTER LANDING WITH NO EVIDENCE OF FIRE OR OVERHEATING. MX R & R THE FWD BAGGAGE SMOKE DETECTOR WITH OPERATIO - [SDR ASOA20140527092](https://openairdocs.org/sdr/ASOA20140527092), May 27, 2014: SENSOR. DIRTY. LAVATORY SMOKE ON EICAS AFTER TAKEOFF. PERFORMED LAVATORY SMOKE TROUBLESHOOTING IAW FIM 26-14-00-810-802-A. CLEANED LAVATORY SENSOR AND RAN ENGINES AT HIGH POWE - [SDR ASOA20140210014](https://openairdocs.org/sdr/ASOA20140210014), Feb 10, 2014: ENGINE. POWER LOSS. THE CREW REPORTED AN ABORTED TAKEOFF AT 125 KTS WITH TAKEOFF THRUST SELECTED. ENGINES ONLY PRODUCED 81 PERCENT N1 WITH THRUST LEVERS IN THE DETENT DURING TAKEOF - [SDR ASOA20130822099](https://openairdocs.org/sdr/ASOA20130822099), Aug 22, 2013: WIRE HARNESS. ARCED. PILOT REPORTED A BURNING ODOR IN THE FWD GALLEY NEAR SEAT 1A. MX INSPECTED AND FOUND SEATS 1A, 3A, AND 4A SOCKETS BURNED. R & R SEAT 1A AND 3A LIGHT SOCKETS AND - [SDR ASOA20130602045](https://openairdocs.org/sdr/ASOA20130602045), Jun 2, 2013: BULB. INOPERATIVE. DURING ROUTINE MX, THE LT OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MX REPLACED THE LT OVERWING EMERGENCY LIGHT BULB. OPS CHECKS WERE GOOD. - [SDR ASOA20111229021](https://openairdocs.org/sdr/ASOA20111229021), Dec 29, 2011: ELECTRONIC UNIT. MALFUNCTIONED. AFTER TAKEOFF, ATC REPORTED THAT IT APPEARED AS THOUGH THE NLG DID NOT FULLY RETRACT. THE CREW SELECTED GEAR DOWN AND RETURNED TO DEPARTURE, WHERE THE ACFT LAND - [SDR C2XA11CL251](https://openairdocs.org/sdr/C2XA11CL251), Nov 17, 2011: PROXIMITY SWITCH. FAULTY. THE CREW REPORTED AFTER TAKEOFF THE NOSE GEAR DOORS SOUNDED LIKE THEY DID NOT RETRACT. LANDING GEAR SOUNDED AS IF DOWN. NO INDICATIONS ON THE EICAS. THE AIRCRAF - [SDR C2XA11CL250](https://openairdocs.org/sdr/C2XA11CL250), Nov 15, 2011: WIRE HARNESS. FAULTY. IND - FLT 4283 THE CREW REPORTED THE NOSE GEAR DOORS DID NOT CLOSE AFTER TAKEOFF. THE AIRCRAFT RETURNED TO IND AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTE - [SDR C2XA11IA257](https://openairdocs.org/sdr/C2XA11IA257), Nov 14, 2011: RELAY. FAULTED. AFTER TAKEOFF THE CREW REPORTED THAT THE NOSE GEAR DOORS DID NOT RETRACT. THE AIRCRAFT CONTINUED TO IAH AND LANDED WITHOUT INCIDENT WHERE MAINTENANCE REPLACED N - [SDR C2XA11IA247](https://openairdocs.org/sdr/C2XA11IA247), Nov 2, 2011: SOLENOID VALVE. INOPERATIVE. ICT - FLIGHT 5931, THE CREW REPORTED A VERY LOUD NOISE FROM TAKEOFF TO LANDING, AND BELIEVED THAT THE NLG DOORS WERE OPEN. THE AIRCRAFT RETURNED TO ICT WHERE IT - [SDR C2XA11IA232](https://openairdocs.org/sdr/C2XA11IA232), Oct 7, 2011: WIRE HARNESS. OVERHEATED. IAH - FLIGHT 4445 THE CREW REPORTED A BURNING SMELL COMING FROM LIGHT OVER 8A. MAINTENANCE REMOVED AND REPLACED THE HARNESS FOR THE AFFECTED LIGHT, OPERATIONALL - [SDR C2XA11CL102](https://openairdocs.org/sdr/C2XA11CL102), Apr 23, 2011: SMOKE DETECTOR. FALSE ACTIVATION. THE CREW REPORTED A LAV SMOKE MESSAGE ON THE EICAS. MX INSPECTED AND REPLACED THE LAV SMOKE DETECTOR. OPS CHECKS WERE GOOD. - [SDR C2XA11SH080](https://openairdocs.org/sdr/C2XA11SH080), Mar 29, 2011: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION BETWEEN FR 23-29. REPAIRED OMEGA BEAM IAW EMB 145 SRM 51-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA11SH079](https://openairdocs.org/sdr/C2XA11SH079), Mar 29, 2011: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION BETWEEN FR 23-29. REPAIRED OMEGA BEAM IAW EMB 145 SRM 51-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE - [SDR C2XA11SH078](https://openairdocs.org/sdr/C2XA11SH078), Mar 29, 2011: FRAME. CRACKED. SHV - DURING C-CHECK FR 10 IS CRACKED JUST BELOW LT DV WINDOW. REPLACED SECTION OF FRAME IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA11SH077](https://openairdocs.org/sdr/C2XA11SH077), Mar 29, 2011: FRAME. CRACKED. SHV - DURING C-CHECK RT FRAME 10 IS CRACKED. REPLACED SECTION OF FRAME IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA11SH076](https://openairdocs.org/sdr/C2XA11SH076), Mar 27, 2011: SKIN. CRACKED. SHV - DURING C-CHECK POSSIBLE CRACKS AROUND 2EA RIVETS AT FRAME 77 STRINGER 4R. MAINTENANCE PERFORMED REPAIR AT FRAME 77 STRINGER 4R AND INITIATED DMI IAW EC533 - [SDR C2XA11SH075](https://openairdocs.org/sdr/C2XA11SH075), Mar 27, 2011: SKIN. CRACKED. SHV - DURING C-CHECK POSSIBLE CRACK AROUND 1EA RIVET AT FRAME 79 STRINGER 4R. MAINTENANCE PERFORMED REPAIRS AT FRAME 79 STRINGER 4R AND INITIATED DMI IAW EC5330 - [SDR C2XA11IA029](https://openairdocs.org/sdr/C2XA11IA029), Feb 6, 2011: LIGHT. MALFUNCTIONED. IAH FLIGHT 3060, DURING TAXI THE CREW REPORTED THAT THE EMERGENCY LIGHTS WERE INOP, AND THAT THE CREW KEPT GOING INTO ESSENTIAL POWER. THE AIRCRAFT ELECTRICAL S - [SDR C2XA10RI032](https://openairdocs.org/sdr/C2XA10RI032), Feb 17, 2010: INVERTER. INOPERATIVE. EWR - DURING ROUTINE MAINTENANCE, EWR MX FOUND EMERGENCY LIGHT AT SEAT 3BC INOPERATIVE. MX REMOVED AND REPLACED INVERTER NR 3 AND PERFORMED OPERATIONAL CHECK SU - [SDR C2XA10IA064](https://openairdocs.org/sdr/C2XA10IA064), Feb 12, 2010: PACKING. DAMAGED. IAH - FLIGHT 2617, THE CREW REPORTED LAV SMOKE IN FLIGHT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NU - [SDR C2XA10CL011](https://openairdocs.org/sdr/C2XA10CL011), Jan 25, 2010: FIRE DETECTOR. FAULTY. BWI FLT 2718 THE CREW REPORTED A FIRE DETECTION NR 1 FAIL MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE FIRE DETECTOR. OPERATIONAL CHECKS WERE GOO - [SDR C2XA10CL009](https://openairdocs.org/sdr/C2XA10CL009), Jan 20, 2010: O-RING. DETERIORATED. CLE FLT 2610 THE CREW REPORTED A BLEED 1 LEAK INDICATION DURING CLIMBOUT FROM CMH. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPE - [SDR C2XA09RI225](https://openairdocs.org/sdr/C2XA09RI225), Dec 23, 2009: WINDSHIELD. SPARKS. FLIGHT 2490 - EWR - FLIGHT CREW REPORTED F/O WINDSHIELD HEAT GLOWING AND SPARKING. EWR MX REMOVED AND REPLACED F/O WINDSHIELD AND PERFORMED OPERATIONAL CHECK SU - [SDR C2XA09RI102](https://openairdocs.org/sdr/C2XA09RI102), May 14, 2009: DOOR SEAL. LACK OF LUBE. FLIGHT 2745, FLIGHT CREW REPORTED MAIN CABIN DOOR STICKS AND HARD TO OPEN. MX CLEANED AND LUBED MAIN CABIN DOOR SEAL AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT - [SDR C2XA07RI102](https://openairdocs.org/sdr/C2XA07RI102), Dec 7, 2007: STRUCTURE. LOOSE. FLT 2289 - EWR - CREW REPORTED DOOR DIFFICULT TO OPEN AND CLOSE. EWR MX RE-SECURED HANDLE BOX BOLTS AND APPLIED LUBE TO DOOR SEAL AND PERFORMED OPERATIONAL CHEC - [SDR C2XA07IA221](https://openairdocs.org/sdr/C2XA07IA221), Oct 10, 2007: WIRE. BROKEN. MCI - FLIGHT 2955, THE CREW REPORTED THAT THE EMERGENCY LIGHTS ILLUMINATE INTERMITTANTLY DURING FLIGHT. THE AIRCRAFT LANDED AT MCI WITHOUT INCIDENT WHERE MAINTE - [SDR C2XA07TY041](https://openairdocs.org/sdr/C2XA07TY041), Aug 5, 2007: BRACKET. DAMAGED. TYS - DURING A CURRENT C-CHECK INSPECTION, ELONGATED HOLES WERE FOUND ON NR 2 RUDDER AT SPAR 1. HOLES MEASURED (1) .249 (2) .228 AND (3) .338. HOLES WERE REAMED - [SDR C2XA07TY040](https://openairdocs.org/sdr/C2XA07TY040), Jul 23, 2007: HINGE FITTING. CRACKED. HORZ STAB LT HINGE PIN SAFETY PIN STRUCTRAL FITTING BROKEN ON LT ROOT FITTING. REMOVED AND REPLACED LT OUTBOARD SIDE HORZ STAB HINGE FITTING. REAMED LT OUTBOARD - [SDR C2XA05BT074](https://openairdocs.org/sdr/C2XA05BT074), Oct 21, 2005: LEG ASSY. FAULTY. CREW REPORTED, LANDING GEAR AIR/GROUND FAILURE, GEAR WOULD NOT RETRACT. RETRACTED GEAR WITH DOWNLOCK RLS. MAINTENANCE REMOVED AND REPLACED THE NOSE GEAR LEG IAW - [SDR C2XA05BT070](https://openairdocs.org/sdr/C2XA05BT070), Oct 6, 2005: PROXIMITY SWITCH. FAULTY. DURING TAKEOFF, A LANDING GEAR AIR/GROUND FAIL MESSAGE SHORTLY AFTER TAKEOFF & LANDING GEAR LEVER WOULD NOT MOVE TO UP/LOCK POSITION. AIRCRAFT RETURNED AND LAND - [SDR C2XA05SH112](https://openairdocs.org/sdr/C2XA05SH112), Sep 10, 2005: FIREWALL. CHAFED. SHV - DURING C-CHECK, APU LOWER FIREWALL HAS SEVERAL CHAFED DAMAGED RIVETS. MAINTENANCE REPAIRED APU LOWER FIREWALL CHAFED DAMAGE RIVETS IAW EC 5330-01500. THE - [SDR C2XA05BT047](https://openairdocs.org/sdr/C2XA05BT047), Jul 19, 2005: MODULE. FAULTY. CREW REPORTED, LANDING GEAR AIR/GROUND FAIL CAUTION LIGHT ON TAKEOFF, LANDING GEAR LEVER WOULD NOT RETRACT AIRCRAFT AIR RETURNED TO BOSTON, AIRCRAFT MAINTENANCE - [SDR C2XA05IA085](https://openairdocs.org/sdr/C2XA05IA085), Jul 4, 2005: LANDING GEAR. MALFUNCTIONED. CREW REPORTED LANDING GEAR DID NOT RETRACT. LANDING GEAR SELECTOR DID NOT MOVE TO UP POSITION AND MANUAL OVER RIDE WAS NOT USED. DURING THIS TIME, LANDING GEAR - [SDR C2XA05CL038](https://openairdocs.org/sdr/C2XA05CL038), May 20, 2005: LAMP. INOPERATIVE. DURING ROUTINE MAINTENANCE, THE EMERGENCY LIGHT AT SEAT 12A WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE LAMP. OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA04BT130](https://openairdocs.org/sdr/C2XA04BT130), Dec 11, 2004: ODOR. DETECTED. DURING TAXI CREW REPORTED VERY STRONG BURNING SMELL FOLLOWED BY GRINDING NOISE AND VIBRATION. SHUTDOWN APU AND INDICATIONS WENT AWAY. INSPECTED APU, ENGINES AND - [SDR C2XA04IA095](https://openairdocs.org/sdr/C2XA04IA095), Aug 7, 2004: BATTERY PACK. DISCHARGED. IAH - FLIGHT 2699, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EME - [SDR C2XA04IA094](https://openairdocs.org/sdr/C2XA04IA094), Aug 7, 2004: BATTERY PACK. DISCHARGED. IAH - FLIGHT 2699, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 EME - [SDR C2XA04IA093](https://openairdocs.org/sdr/C2XA04IA093), Aug 7, 2004: BATTERY PACK. DISCHARGED. IAH - FLIGHT 2699, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 EME - [SDR C2XA04IA092](https://openairdocs.org/sdr/C2XA04IA092), Aug 7, 2004: BATTERY PACK. DISCHARGED. IAH - FLIGHT 2699, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 EME - [SDR C2XA03TY179](https://openairdocs.org/sdr/C2XA03TY179), Oct 16, 2003: FLOORBEAM. CORRODED. DURING A SCHEDULED 2C INSPECTION THE RT FLOORBEAM TOP PLATES AT FR 20 AND FR 22 WERE CORRODED AT THE NUT PLATE HOLES. MAINT INSTALLED THE RT FLOORBEAM TOP PLATE - [SDR C2XA03TY180](https://openairdocs.org/sdr/C2XA03TY180), Oct 16, 2003: NUT PLATE. CORRODED. TYS DURING A SCHEDULED 2C INSPECTION THE CENTER SERVICE DOOR SILL NUT PLATES WERE CORRODED. MAINT REPAIRED THE CENTER DOOR SILL IAW EMB 135/145 GST-1927-02A AND - [SDR C2XA03TY178](https://openairdocs.org/sdr/C2XA03TY178), Oct 16, 2003: ANGLE. CORRODED. DURING A SCHEDULED 2C INSPECTION THERE WAS EVIDENCE OF CORROSION BENEATH THE CARBON FIBER FLOOR SUPPORT AT FR 20. MAINT REMOVED AND REPLACED THE RAMP ANGLE IN T - [SDR C2XA03TY176](https://openairdocs.org/sdr/C2XA03TY176), Oct 5, 2003: FLOORBEAM. CORRODED. TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE GALLEY FLOOR SUPPORT CENTER OMEGA BEAM. MAINTENANCE REMOVED AND REPLACED THE OMEGA BEAM IAW EMB SRM - [SDR C2XA03TY175](https://openairdocs.org/sdr/C2XA03TY175), Oct 5, 2003: GUSSET. CORRODED. DURING A SCHEDULED INSPECTION THE FORWARD FUSELAGE GUSSET WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION. MAINTENANCE REMOVED AND REPLACED THE FUSELAGE GUSSET IAW All 62: https://openairdocs.org/deregistered/N13994-2021-04-21/reports.md ## Other aircraft with N13994 - [Cancelled 1975-07-17](https://openairdocs.org/deregistered/N13994-1975-07-17): Piper PA-23-250, S/N 27-4612, built 1971. Exported to Canada. Owner: [Maxwell Farms Co](https://openairdocs.org/faa-owner/MAXWELL%20FARMS%20CO), [Morrison, CO](https://openairdocs.org/faa-place/CO/Morrison) - [Cancelled 1937-04-27](https://openairdocs.org/deregistered/N13994-1937-04-27): Spartan 7W, S/N 7W-3, built 1936. Exported to Mexico. Owner: [Spartan Aircraft Co](https://openairdocs.org/faa-owner/SPARTAN%20AIRCRAFT%20CO), [Tulsa, OK](https://openairdocs.org/faa-place/OK/Tulsa) --- 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.