# N14920: 2001 Embraer EMB-145LR, registration cancelled 2018-08-22

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 22, 2018
- Exported to: Argentina
- 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: 145380
- Year built: 2001
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 1, 2001
- Certificate issued: August 21, 2018
- Last registry action: August 21, 2018
- Mode S code: A0C6D6
- Owner when cancelled: [Southern Aircraft Consultancy Inc Trustee](https://openairdocs.org/faa-owner/SOUTHERN%20AIRCRAFT%20CONSULTANCY%20INC%20TRUSTEE)
- Location: Suffolk, United Kingdom
- Owner type: Corporation
- The mark today: https://openairdocs.org/aircraft/N14920
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14920
- Page: https://openairdocs.org/deregistered/N14920-2018-08-22

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 (76, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR ASOA20160916048](https://openairdocs.org/sdr/ASOA20160916048), Sep 16, 2016: COFFEEMAKER. BURNED OUT. CREW REPORTED A BURNING ODOR IN THE GALLEY AREA AND DID NOT INDICATE IF ON GROUND OR IN FLIGHT. MX REMOVED AND REPLACED NR 1 COFFEE BREWER WITH OPS CHECKED GOOD
- [SDR ASOA20160402020](https://openairdocs.org/sdr/ASOA20160402020), Apr 2, 2016: BATTERY PACK. DISCHARGED. THE CREW REPORTED EMERGENCY LIGHT ABOVE F/A WAS INOPERATIVE. MAINTENANCE PERFORMED RECHARGE OF EMERGENCY LIGHT BATTERY WITH APU RUNNNING. OPS CHECK OF EMERGENCY
- [SDR ASOA20150312018](https://openairdocs.org/sdr/ASOA20150312018), Mar 13, 2015: YOKE. CRACKED. DURING ROUTINE MAINTENANCE THE LT ENGINE FORWARD LOWER YOKE FITTING WAS FOUND CRACKED. MAINTENANCE REPLACED THE FITTING IAW SB 145-54-0013 AND STS EA 26-2014-06
- [SDR ASOA20150226015C](https://openairdocs.org/sdr/ASOA20150226015C), Feb 26, 2015: INVERTER. FAULTY. DURING ROUTINE MAINTENANCE THE AFT CABIN EXIT SIGN DID NOT ILLUMINATE DURING TEST. MAINTENANCE REPLACED THE NR4 EMERGENCY LIGHT DC/AC INVERTER. OPS CHECKS WERE 
- [SDR ASOA20141221153](https://openairdocs.org/sdr/ASOA20141221153), Dec 21, 2014: INVERTER. INOPERATIVE. DURING PREFLIGHT INSPECTION, THE CREW REPORTED AN EMERGENCY EXIT ROW EXIT LIGHT TO BE INOPERATIVE. MAINTENANCE R & R THE INVERTER, OPS TESTED WITH NO DEFECTS NO
- [SDR ASOA20140325031](https://openairdocs.org/sdr/ASOA20140325031), Mar 25, 2014: ATTACH BRACKET. WORN. DURING C-CHECK,M LT OTBD AILERON PCA BRACKET OTBD TAB HAS WORN LUG HOLE. MAINTENANCE R & R PCA FITTING FOR LT AILERON IAW EC5750-01177(C). THE ACFT WAS APPROVED
- [SDR ASOA20140317030](https://openairdocs.org/sdr/ASOA20140317030), Mar 17, 2014: FITTING. CRACKED. DURING C-CHECK. NR 2 ENGINE FWD LOWER YOKE FITTING CRACKED. R & R NR 2 ENGINE FWD LOWER ENGINE YOKE FITTING IAW EC 5450-01073. ACFT WAS APPROVED FOR RETURN TO S
- [SDR ASOA20120131015](https://openairdocs.org/sdr/ASOA20120131015), Jan 31, 2012: PRECOOLER. CRACKED. THE CREW REPORTED A BLEED NR 2 OVERTEMP MESSAGE IN FLIGHT. ALSO REPORTED A BURNING SMELL. MX INSPECTED AND REPLACED THE NR 2 ENGINE PRECOOLER. OPS CHECKS WERE G
- [SDR C2XA11RI132](https://openairdocs.org/sdr/C2XA11RI132), Aug 9, 2011: SMOKE WARNING. FALSE ACTIVATION. FLIGHT 6030 - SYR - FLIGHT CREW REPORTED BAGG SMOKE INDICATION ON EICAS. SYSTEM RESET WAS PERFORMED SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA11CL172](https://openairdocs.org/sdr/C2XA11CL172), Jul 22, 2011: SENSE LINE. LOOSE. EWR FLT 2609 THE CREW REPORTED A WING ANTI/ICE FAIL MESSAGE DURING ICE TEST ON CLIMBOUT. THE AIRCRAFT DIVERTED INTO CLE. MAINTENANCE INSPECTED AND SECURED SENSE
- [SDR C2XA11RI126](https://openairdocs.org/sdr/C2XA11RI126), Jul 18, 2011: UNKNOWN. ODOR. FLIGHT 2956 - EWR - FLIGHT CREW REPORTED LIGHTNING STRIKE FOLLOWED BY ELECTRICAL SMELL SHORTLY AFTER. EWR MX PERFORMED LIGHTNING STRIKE INSPECTION AND NO DEFECT
- [SDR C2XA10CL109](https://openairdocs.org/sdr/C2XA10CL109), Jul 9, 2010: TUBE. FAULTY. BIS FLT 5655 THE CREW REPORTED A "ENGINE NR 1 ATTCS NO MARGIN" MESSAGE ON TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE COMPRESSOR AIR DISCHARGE T
- [SDR C2XA10CL108](https://openairdocs.org/sdr/C2XA10CL108), Jul 8, 2010: TUBE. FAULTY. BIS FLT 5800 THE CREW REPORTED A "ENGINE NR 1 ATTCS NO MARGIN" MESSAGE ON TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE 14TH STAGE CUSTOMER TUBE. 
- [SDR C2XA10CL100](https://openairdocs.org/sdr/C2XA10CL100), Jun 25, 2010: FUEL CONTROL. LEAKING. THE CREW REPORTED A FUEL SMELL COMING FROM THE APU. MAINTENANCE INSPECTED AND REPLACED THE APU FUEL CONTROL. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA10CL097](https://openairdocs.org/sdr/C2XA10CL097), Jun 23, 2010: BLEED VALVE. FAULTY. FLT 5779 THE CREW REPORTED A FUEL SMELL IN THE CABIN WITH THE APU RUNNING. MAINTENANCE INSPECTED AND REPLACED THE APU BLEED VALVE. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA10CL067](https://openairdocs.org/sdr/C2XA10CL067), May 10, 2010: LIGHT. INOPERATIVE. DURING ROUTINE MAINTENANCE THE AFT AISLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS 
- [SDR C2XA10TY065](https://openairdocs.org/sdr/C2XA10TY065), Apr 26, 2010: INVERTER. INOPERATIVE. TYS - FLOOR PROXIMITY EMERGENCY LIGHTS BETWEEN SEATS 8 THRU 12 INTERMITTENT. REMOVED AND REPLACED EMERGENCY LIGHT INVERTER NR 5. OPS CHECK GOOD.
- [SDR C2XA10TY062](https://openairdocs.org/sdr/C2XA10TY062), Apr 23, 2010: STRINGER. CORRODED. TYS - A/C CURRENTLY IN C-CHECK WHEN INSPECTION FOUND CORROSION AT STRINGER 21R AND SPLICE CORRODED BETWEEN FRAMES 14 AND 15. MAINTENANCE REPAIRED THE AREA IAW E
- [SDR C2XA10TY064](https://openairdocs.org/sdr/C2XA10TY064), Apr 22, 2010: ANGLE. CORRODED. AFT GALLEY STEP UP CORRODED AT OUTBOARD END. REPLACED LWR AFT STEP UP ANGLE, FABRICATED, INSTALLED, ALODINED, PRIMED AND PAINTED OUTBOARD ANGLE IAW EMB 145 SRM 
- [SDR C2XA10TY070](https://openairdocs.org/sdr/C2XA10TY070), Apr 21, 2010: STRINGER SPLICE. CORRODED. TYS - STRINGER 21R AND SPLICE CORRODED BETWEEN FRAMES 14 AND 15. REPAIRED AREA IAW EMB 145 SRM 51-40-02 AND 51-20-03. RESTORED SURFACE FINISH IAW EMB 145 CPM 51
- [SDR C2XA10TY059](https://openairdocs.org/sdr/C2XA10TY059), Apr 21, 2010: SUPPORT. CORRODED. A COUPLE OF BOLT HOLES OUTBOARD OF THE NR 2 GENERATOR SUPPORT ON THE NR 2 ENG INLET FLANGE HAS CORROSION. REMOVED CORROSION AND INSTALLED BUSHINGS IAW EC5420-01
- [SDR C2XA10TY069](https://openairdocs.org/sdr/C2XA10TY069), Apr 15, 2010: SUPPORT BRACKET. CORRODED. TYS - CORROSION ON SUPPORT ASSY FOR AILERON TORQUE TUBE ON SKIN SIDE BETWEEN FRAMES 11 AND 12 BETWEEN STRINGERS 21R AND 20R. REMOVED AND REPLACED SUPPORT ASSY.
- [SDR C2XA10TY068](https://openairdocs.org/sdr/C2XA10TY068), Apr 15, 2010: FITTING. CORRODED. TYS - SHEAR CLIP CORRODED AT FRM 12 STRINGER 21R. REMOVED AND REPLACED SHEAR CLIP.
- [SDR C2XA10TY067](https://openairdocs.org/sdr/C2XA10TY067), Apr 15, 2010: SKIN SPLICE. CORRODED. TYS - INNER SKIN SPLICE BETWEEN FRMS 12 AND 13 AND BETWEEN STRINGERS 19L AND 19R CORRODED. FOUND TO BE STR 20L AND 20R. REMOVED AND REPAIRED SECTION OF SKIN BUT
- [SDR C2XA10TY066](https://openairdocs.org/sdr/C2XA10TY066), Apr 15, 2010: SKIN. CORRODED. TYS - CORRODED HARDWARE AND EVIDENCE OF CORROSION ON INTERNAL SKIN BETWEEN FRAMES 13 AND 14 AND STRINGERS 21L AND 21R. REMOVED DAMAGED SECTION OF SKIN BUTTSTRAP
- [SDR C2XA10CL035](https://openairdocs.org/sdr/C2XA10CL035), Feb 25, 2010: DISPLAY. SHORTED. IAD FLT 5701 THE CREW REPORTED A EICAS FAIL AND A BURNT SMELL IN THE COCKPIT. THE C/B WAS POPPED AS WELL. MAINTENANCE INSPECTED AND REPLACED THE FIRST OFFICER'S
- [SDR C2XA09CL163](https://openairdocs.org/sdr/C2XA09CL163), Dec 17, 2009: FIREWALL. CRACKED. DURING ROUTINE 3A INSPECTION THE APU FIREWALL HAD MULTIPLE CRACKS AROUND THE LEFT UPPER SUPPORT AREA. THE FIREWALL WAS REPAIRED IAW SRM 53-32-13, 4 CRACKS TOTAL
- [SDR C2XA09IA311](https://openairdocs.org/sdr/C2XA09IA311), Dec 13, 2009: WIRE. OUT OF POSITION. IAH - FLIGHT 2119, DURING POST FLIGHT INSPECTION THE CREW REPORTED EMERGENCY LIGHTS NOT WORKING BETWEEN ROWS 8-11 WITH WIRES STICKING OUT AT ROW 8. MAINTENANCE 
- [SDR C2XA09IA292](https://openairdocs.org/sdr/C2XA09IA292), Nov 23, 2009: PUMP. FAILED. IAH - FLIGHT 2989, DURING CRUISE FLIGHT THE CREW REPORTED LOSING THE NUMBER TWO HYDRAULIC SYSTEM. THE CREW DECLARED AN EMERGENCY, AND LANDED AT IAH WITHOUT INCI
- [SDR C2XA09RI197](https://openairdocs.org/sdr/C2XA09RI197), Nov 11, 2009: ENGINE. INOPERATIVE. DURING APU START, APU FIRE INDICATION ON EICAS WITH SMOKE COMING FROM APU TAIL CONE. APU CUT, NO FIRE NOTICED. EWR MX REMOVED AND REPLACED APU AND PERFORMED OPE
- [SDR C2XA09IA190](https://openairdocs.org/sdr/C2XA09IA190), Jul 27, 2009: INVERTER. INOPERATIVE. IAH - DURING A-CHECK INSPECTION THE NUMBER TWO AND THREE EMERGENCY LIGHT AISLE PATH LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED 
- [SDR C2XA09CL085](https://openairdocs.org/sdr/C2XA09CL085), Jun 17, 2009: POWER SUPPLY. INOPERATIVE. CREW REPORTED VERIOUS EMERGENCY LIGHTS INOPERATIVE. MX RESET FWD EMERGENCY LIGHT POWER SUPPLY. CHECKS WERE GOOD AND ACFT WAS RETURNED TO SERVICE.
- [SDR C2XA09IA076](https://openairdocs.org/sdr/C2XA09IA076), Mar 14, 2009: UNKNOWN. ODOR. IAH - FLIGHT 2850, AFTER LANDING THE CREW REPORTED A FUEL SMELL IN THE AIRCRAFT AFTER STARTING THE APU. THE AIRCRAFT MADE IT TO THE GATE WITHOUT INCIDENT. MAINT
- [SDR C2XA08RI139](https://openairdocs.org/sdr/C2XA08RI139), Sep 9, 2008: BATTERY. INOPERATIVE. FLIGHT 2516 EWR FLIGHT CREW REPORTED FORWARD EMERGENCY LIGHTS VERY DIM AND STAYS ON WHILE SWITCH IS IN OFF POSITION. EWR MX R&R EMERGENCY LIGHT BATTERY NR 2 AND
- [SDR C2XA08RI114](https://openairdocs.org/sdr/C2XA08RI114), Aug 7, 2008: INVERTER. INOPERATIVE. RIC - DURING ROUTINE MAINTENANCE, RIC MAINTENANCE EMERGENCY LIGHT STRIP INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT INVERTER AND PERFORMED OPE
- [SDR C2AO8SH079](https://openairdocs.org/sdr/C2AO8SH079), May 22, 2008: BEAM. CORRODED. SHV - DURING C-CHECK CARGO DOOR LOWER BEAM HAS CORROSION. MX REMOVED AND REPLACED CARGO DOOR CUTOUT LOWER BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROV
- [SDR C2XA08SH078](https://openairdocs.org/sdr/C2XA08SH078), May 22, 2008: ATTACH BRACKET. DAMAGED. LEFT DAMPER ATTACHMENT BRACKET ON AILERON SPAR O/B HAT BUSHING IS MIGRATED. MX REMOVED AND REPLACED LEFT AILERON DAMPER ATTACH BRACKET IAW EMB 145 SRM 51-40-02.
- [SDR C2XA07TY016](https://openairdocs.org/sdr/C2XA07TY016), Mar 29, 2007: THERMAL SWITCH. TRIPPED. FLT 2807, F/A NOTED THERMAL SWITCH FOR GALLEY POPPED IN FLIGHT WITH ASSOCIATED BURNING ODOR. AC RELEASED IAW MEL 25-60-02 (3) CAT D.
- [SDR C2XA06RI011](https://openairdocs.org/sdr/C2XA06RI011), Nov 24, 2006: LIGHT. INOPERATIVE. RIC MX - DURING ACFT ROUTINE MAINTENANCE, MX FOUND RT OVERWING LIGHT INOP. MX REMOVED AND REPLACED THE BULB. OPERATIONAL CHECK WAS PERFORMED SUCCESSFULLY. ACFT 
- [SDR C2XA06BT053](https://openairdocs.org/sdr/C2XA06BT053), Nov 22, 2006: SMOKE DETECTOR. INTERMITTENT. EWR LOG SQUAWK LAV SMOKE WARNING AFTER DEPARTURE. NO SMOKE NOTICED. WARNING WENT AWAY AFTER 1 MINUTE. REMOVED AND REPLACED LAV SMOKE DETECTOR IAW EMB-145 AMM 26
- [SDR C2XA05CL076](https://openairdocs.org/sdr/C2XA05CL076), Sep 5, 2005: LEVER. LOOSE. CLE - FLIGHT NR 3264 - THE CREW REPORTED, THE MAIN CABIN DOOR IS VERY HARD TO OPEN. IT STICKS AND CAN TAKE SEVERAL TRIES TO OPEN. MAINTENANCE INSPECTED AND RE-S
- [SDR C2XA05CL058](https://openairdocs.org/sdr/C2XA05CL058), Jul 17, 2005: PROXIMITY SWITCH. FAILED. LOUD RUMBLING SOUND FROM NOSE. CAME SUDDENLY DURING CLIMB-OUT. SOUNDED LIKE NOSE GEAR DOOR OPENED UP. MAINTENANCE INSPECTED AND FOUND NOSE GEAR DOORS WOULD NOT 
- [SDR C2XA04BT111](https://openairdocs.org/sdr/C2XA04BT111), Oct 19, 2004: POWER SUPPLY. FAULTY. EWR - CREW REPORTED, EMERGENCY LIGHTS AT EXIT ROWS ARE REAL DIM. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY UNDER FLOORBOARD IAW EMB1
- [SDR C2XA04CL064](https://openairdocs.org/sdr/C2XA04CL064), Jun 19, 2004: LIGHT. INOPERATIVE. CLE FLIGHT 2314 THE CREW REPORTED THE EMERGENCY LIGHT WAS INOPERATIVE AT 12A ON CEILING. MAINTENANCE REPLACED THE EMERGENCY LIGHT ON THE CEILING AT ROW 12A. OPE
- [SDR C2XA04SH338](https://openairdocs.org/sdr/C2XA04SH338), Jun 1, 2004: BUTTSTRAP. CORRODED. DURING C CHECK THE CENTER BUTTSTRAP AT FRAME 14 WAS FOUND TO BE CORRODED AROUND THE NUTPLATES. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPA
- [SDR C2XA04SH337](https://openairdocs.org/sdr/C2XA04SH337), May 31, 2004: RIB. CHAFED. SHV - DURING C-CHECK THE LEFT HAND LOWER COWLING RIB AT STATION NX-2180.0 WAS FOUND TO HAVE A HOLE CHAFED IN IT. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE A
- [SDR C2XA04SH329](https://openairdocs.org/sdr/C2XA04SH329), May 29, 2004: BUTTSTRAP. CORRODED. SHV - DURING C-CHECK THE FORWARD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED ON THE LEFT HAND SIDE AT FRAME 14. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORME
- [SDR C2XA04SH319](https://openairdocs.org/sdr/C2XA04SH319), May 25, 2004: STIFFENER. CHAFED. DURING C-CHECK THE NR 1 ENGINE LOWER ENGINE COWLING AFT EDGE MEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EDGE MEMBER IAW EMB 14
- [SDR C2XA04SH318](https://openairdocs.org/sdr/C2XA04SH318), May 25, 2004: BEAM. CORRODED. SHV - DURING C-CHECK THE CARGO DOOR LOWER CUTOUT BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE
- [SDR C2XA04SH317](https://openairdocs.org/sdr/C2XA04SH317), May 23, 2004: GUSSET. CORRODED. SHV - DURING C-CHECK THE RIGHT FLOORBEAM DOUBLER AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 51-

All 76: https://openairdocs.org/deregistered/N14920-2018-08-22/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 20051010025549I](https://openairdocs.org/incident/20051010025549I), Oct 10, 2005: Emb EMB145LR (N14920), Wichita, KS. (-23) On October 10, 2005, Continental express flight number 3000 at 1915 local time while enroute from iah to ict declared an emergency due to both engines…

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