# N14923: 2000 Embraer EMB-145LR, registration cancelled 2018-09-25

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 25, 2018
- Exported to: Ethiopia
- 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: 145318
- Year built: 2000
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 25, 2000
- Certificate issued: July 6, 2018
- Last registry action: July 6, 2018
- Mode S code: A0C6D9
- Owner when cancelled: [Flight Lease Xv LLC](https://openairdocs.org/faa-owner/FLIGHT%20LEASE%20XV%20LLC)
- Location: [West Palm Beach, FL](https://openairdocs.org/faa-place/FL/West%20Palm%20Beach)
- Owner type: Corporation
- Owner's area on the map: 26.7158° N, 80.0668° W: Placed by OpenAirDocs at the center of ZIP code 33401, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N14923
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14923
- Page: https://openairdocs.org/deregistered/N14923-2018-09-25

From the FAA registry file of October 31, 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 (69, newest 50)

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

- [SDR 2017FA0000498](https://openairdocs.org/sdr/2017FA0000498), Sep 20, 2017: SPACER. LOOSE. WHEN INSPECTING THE AILERON CABLES INSPECTOR FOUND THAT THE SPACER (BELOW) USED HAD GAP IN IT CAUSING THE BOLT TO WOBBLE IN THE HOLE AND THE BELLCRANK TO DEFLEC
- [SDR ASOA20160412021C](https://openairdocs.org/sdr/ASOA20160412021C), Apr 12, 2016: CONTROL PANEL. MALFUNCTIONED. THE CREW REPORTED LAV SMOKE WARNING INDICATION AT 4000 FT ON CLIMB OUT. THE ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FOR
- [SDR ASOA20160409035H](https://openairdocs.org/sdr/ASOA20160409035H), Apr 9, 2016: SMOKE DETECTOR. DEFECTIVE. THE CREW REPORTED A LAV SMOKE WARNING AFTER TAKEOFF WITH NO SMOKE NOTED. THE ACFT CONTINUED TO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE R & R THE LAV SMOKE
- [SDR ASOA20160404014](https://openairdocs.org/sdr/ASOA20160404014), Apr 4, 2016: SMOKE DETECTOR. FAULTY. CREW REPORTED A "LAV SMOKE" INDICATION IN FLIGHT. MAINTENANCE R & R LAV SMOKE DETECTOR WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150902172V](https://openairdocs.org/sdr/ASOA20150902172V), Sep 2, 2015: YOKE. CRACKED. DURING C-CHECK. RT ENGINE FWD LOWER YOKE IS CRACKED. R & R RT LOWER FWD YOKE FITTING IAW EC5450-01172. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150902171V](https://openairdocs.org/sdr/ASOA20150902171V), Sep 2, 2015: YOKE. CRACKED. DURING C-CK. LT ENGINE FWD LOWER YOKE IS CRACKED. R & R LT ENGINE FWD LWR YOKE IAW EC5450-01172. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150902170](https://openairdocs.org/sdr/ASOA20150902170), Sep 2, 2015: SUPPORT ANGLE. CORRODED. DURING C-CK. CARGO DOOR LOWER SUPPORT ANGLE CORRODED AROUND NUTPLATE HOLES. R & R CARGO DOOR LOWER SUPPORT ANGLE IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO S
- [SDR ASOA20150902169](https://openairdocs.org/sdr/ASOA20150902169), Sep 2, 2015: FLOOR SUPPORT. CORRODED. DURING C-CK. CENTER OMEGA BEAM CORRODED BETWEEHN FRAME 59-60. REPAIRED OMEGA BEAM IAW EC5310-01473. ACFT IS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150828161V](https://openairdocs.org/sdr/ASOA20150828161V), Aug 28, 2015: FRAME. CORRODED. DURING C-CHECK, THE CARGO DOOR LOWER FRAME WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE FRAME IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150828160](https://openairdocs.org/sdr/ASOA20150828160), Aug 28, 2015: SKIN. CORRODED. DURING C-CHECK, CARGO DOOR LOWER SKIN WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE SKIN IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150605054H](https://openairdocs.org/sdr/ASOA20150605054H), Jun 5, 2015: ACM. INOPERATIVE. THE CREW REPORTED SMOKE IN THE COCKPIT. THE ACFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE R & R BOTH ACM'S, OPERATIONALLY TESTED WITH NO DEFECTS NOTED AND THE 
- [SDR ASOA20150605053](https://openairdocs.org/sdr/ASOA20150605053), Jun 5, 2015: ACM. INOPERATIVE. THE CREW REPORTED SMOKE IN THE COCKPIT. THE ACFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE R & R BOTH ACM'S, OPERATIONALLY TESTED WITH NO DEFECTS NOTED AND THE 
- [SDR ASOA20141109127](https://openairdocs.org/sdr/ASOA20141109127), Nov 9, 2014: RETAINING RING. BROKEN. MAIN CABIN DOOR WOULD NOT OPEN FROM THE INSIDE OF ACFT. MAINTENANCE FOUND THE MAIN CABIN DOOR RETAINER RING OUT OF PLACE AND R & R RETAINER RING ON TORQUE TUBE.
- [SDR ASOA20140827073](https://openairdocs.org/sdr/ASOA20140827073), Aug 27, 2014: DEFLECTOR. MISINSTALLED. DURING ROUTINE MAINTENANCE, THE RT OVERWING EMERGENCY EXIT WOULD NOT OPEN. CATHES ON SIDEWALL DEFLECTOR. FURTHER INSPECTION FOUND THE SIDE WALL DEFLECTOR WAS IN
- [SDR ASOA20140728060](https://openairdocs.org/sdr/ASOA20140728060), Jul 28, 2014: HOUSING. FAULTY. THE CREW REPORTED LAVATORY SMOKE WARNING, ELECTRICAL FIRE ODOR IN AND AROUND LAV. LAVATORY LIGHT WARM TO TOUCH. MAINTENANCE INSPECTED AND REPLACED THE LAVATORY 
- [SDR ASOA20140724082](https://openairdocs.org/sdr/ASOA20140724082), Jul 24, 2014: ENGINE. BIRD INGESTION. PILOT REPORTED A STRONG ODOR OF SMOKE APPROACH AND SHUTOFF PACKS AND ODOR WENT AWAY. MX INSPECTED ACFT AND DETERMINED NR 1 ENGINE INGESTED A BIRD. MX PERFORMED 
- [SDR ASOA20140122007](https://openairdocs.org/sdr/ASOA20140122007), Jan 22, 2014: INVERTER. MALFUNCTIONED. THE CREW REPORTED EMERGENCY LIGHT WAS INOPERATIVE FROM EXIT ROW ON BACK. MAINTENANCE INSPECTED AND PERFORMED RERACK OF NR 4 AND NR 6 EMERGENCY LIGHT INVERTER'S.
- [SDR ASOA20130901217](https://openairdocs.org/sdr/ASOA20130901217), Sep 1, 2013: FRAME. CRACKED. DURING C-CHECK, FRAME 10 CRACKED UNDER LT DV WINDOW CUTOUT. MX R & R FRAME 10 CHANNEL UNDER LT DV WINDOW CUTOUT SIDE IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR
- [SDR ASOA20130901216](https://openairdocs.org/sdr/ASOA20130901216), Sep 1, 2013: SKIN. CORRODED. DURING C-CHECK SKIN SPLICE HAS CORROSION, FR 13-14, STR 21L-21R. MX PERFORMED AND COMPLETED REPAIR OF SKIN SPLICE FR 13-14, STR 21L-21R IAW SRM 53-00-02 AND CPM
- [SDR ASOA20130831215](https://openairdocs.org/sdr/ASOA20130831215), Aug 29, 2013: TRUNNION. CORRODED. DURING C-CHECK, THE LT AFT MLG TRUNNION FITTING WAS FOUND TO HAVE CORROSION IN MULTIPLE AREAS OF THE BACK WALL AND IN THE GREASE CHANNEL. MX PERSONNEL PERFORMED
- [SDR ASOA20130803089](https://openairdocs.org/sdr/ASOA20130803089), Aug 3, 2013: SMOKE DETECTOR. FALSE INDICATION. CREW REPORTED A LAVATORY SMOKE INDICATION ON EICAS TWICE DURING FLIGHT. CREW PERFORMED QRH AND CONTINUED TO DESTINATION. MX INSPECTED AND FOUND NO EVIDENCE OF L
- [SDR ASOA20120522079](https://openairdocs.org/sdr/ASOA20120522079), May 24, 2012: LIGHT. BURNED OUT. THE CREW REPORTED SMOKE IN THE CABIN NEAR SEAT 2A & NEAR THE GALLEY COMING FROM CEILING PANELS. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT.
- [SDR ASOA20120214013](https://openairdocs.org/sdr/ASOA20120214013), Feb 14, 2012: LIGHT. INOPERATIVE. DURING SCHEDULED MX INSPECTION, THE LT WING/FUSELAGE EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MX R & R THE EMERGENCY EXIT LIGHT IAW AMM 33-50-07. OPS CHECKED
- [SDR ASOA20120214012](https://openairdocs.org/sdr/ASOA20120214012), Feb 14, 2012: INVERTER. INOPERATIVE. DURING SCHEDULED MX INSPECTION, THE FWD CABIN EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. MX R & R THE FWD CABIN EMERGENCY EXIT INVERTER IAW AMM 33-50-11 WITH OP
- [SDR C2XA11RI149](https://openairdocs.org/sdr/C2XA11RI149), Sep 11, 2011: SIGN. INOPERATIVE. DURING ROUTINE MAINTENANCE, RIC MX FOUND THE EMERGENCY EXIT SIGN IN FRONT OF SEAT 3B INOPERATIVE. RIC MX REMOVED AND REPLACED EXIT SIGN AT 3B AND PERFORMED OPER
- [SDR C2XA10CL191](https://openairdocs.org/sdr/C2XA10CL191), Dec 3, 2010: CONNECTOR. CORRODED. THE CREW REPORTED A LAV SMOKE MESSAGE ON THE EICAS WHILE PARKED AT THE GATE. MAINTENANCE INSPECTED AND REPLACED THE LAV SMOKE DETECTOR CONNECTOR. OPERATIONAL CH
- [SDR C2XA10IA301](https://openairdocs.org/sdr/C2XA10IA301), Nov 21, 2010: ROTARY SWITCH. INOPERATIVE. DSM - FLIGHT 6008 OMA-ORD DIVERTED TO DSM DUE TO AN ELECTRICAL EMERGENCY ABNORMAL MESSAGE IN FLIGHT. THE AIRCRAFT LANDED AT DSM WITHOUT INCIDENT WHERE MAINTENAN
- [SDR C2XA10CL149](https://openairdocs.org/sdr/C2XA10CL149), Sep 20, 2010: BLEED VALVE. FAULTY. THE CREW REPORTED A FUEL SMELL WHEN THE APU WAS STARTED. MAINTENANCE INSPECTED AND REPLACED THE APU BLEED VALVE. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA10CL147](https://openairdocs.org/sdr/C2XA10CL147), Sep 16, 2010: DUCT. CONTAMINATED. THE CREW REPORTED APU GENERATOR OFF BUS MESSAGE AFTER PUSHBACK DURING NR 2 ENGINE START ACCOMPANIED BY FAINT ACRID SCENT. MAINTENANCE INSPECTED AND PERFORMED EN
- [SDR C2XA10SH221](https://openairdocs.org/sdr/C2XA10SH221), Jun 29, 2010: BATTERY. OVERHEATED. ACFT N14923 HAD BATT NR 2 OVERTEMP REACHED 83 DEGS CELSIUS DURING DESCENT. MAINTENANCE REMOVED AND REPLACED BATT NR 2 IAW EMB-145 AMM 24-36-01. OPERATIONAL CHEC
- [SDR C2XA10CL075](https://openairdocs.org/sdr/C2XA10CL075), May 12, 2010: RELAY. FAULTY. CAK FLT 5781 THE CREW REPORTED THE BAG SMOKE PUSH BUTTON LIGHT WOULD NOT TEST. MAINTENANCE INSPECTED AND REPLACED RELAY KO629. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA10TY073](https://openairdocs.org/sdr/C2XA10TY073), Apr 27, 2010: LIGHT. INOPERATIVE. EXIT ROW EMERGENCY CEILING LIGHT INOP. REMOVED AND REPLACED LIGHT BULB IAW EMB 145 AMM 33-50-08. OPS CHECK GOOD.
- [SDR C2XA10TY072](https://openairdocs.org/sdr/C2XA10TY072), Apr 27, 2010: LIGHT. INOPERATIVE. MAIN PAX DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT BULB IAW EMB 145 AMM 33-50-06. OPS CHECK GOOD.
- [SDR C2XA09RI227](https://openairdocs.org/sdr/C2XA09RI227), Dec 25, 2009: LINE. CONTAMINATED. FLIGHT 2068 - JAX - FLIGHT CREW REPORTED LOST OF AIRSPEED INDICATION IN CRUISE. FLIGHT CREW PERFORMED EMERGENCY DESCENT AND LANDED UNEVENTFULLY. MX DRAINED WATE
- [SDR C2XA09SH383](https://openairdocs.org/sdr/C2XA09SH383), Oct 24, 2009: FLOOR SUPPORT. CORRODED. SHV - DURING C-CK, RT OMEGA BEAM HAS CORROSION AT FR 23. REPAIRED OMEGA BEAM IAW EC 5320-01443. A/C WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH381](https://openairdocs.org/sdr/C2XA09SH381), Oct 21, 2009: DOUBLER. CORRODED. SHV - DURING C-CHECK DOUBLER AT FRAME 22 IS CORRODED (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED DOUBLER AT FRAME 22. THE AIRCRAFT WAS APPROVED FOR RETURN
- [SDR C2XA09SH380](https://openairdocs.org/sdr/C2XA09SH380), Oct 21, 2009: DOUBLER. CORRODED. SHV - DURING C-CHECK DOUBLER AT FRAME 20 IS CORRODED (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED DOUBLER AT FRAME 20 IAW EMB-145 SRM 51-40-02. THE AIRCRAF
- [SDR C2XA09SH379](https://openairdocs.org/sdr/C2XA09SH379), Oct 21, 2009: FITTING. CRACKED. SHV - DURING C-CHECK SHEAR CLIP AT FRAME 81 AT 3 O'CLOCK POSITION GOUGED. MAINTENANCE REMOVED AND REPLACED CRACKED AND GOUGED SHEAR CLIP AT FRAME 81 AT 3 O'CLOC
- [SDR C2XA09SH378](https://openairdocs.org/sdr/C2XA09SH378), Oct 21, 2009: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM AFT DOUBLER (AFT OF CROSSBEAM) IS CORRODED (LEVEL 2 LOCAL) AT FRM 20A. MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM AT FRAME
- [SDR C2XA09SH377](https://openairdocs.org/sdr/C2XA09SH377), Oct 21, 2009: FITTING. CORRODED. SHV - DURING C-CHECK CORROSION (LEVEL 2 LOCAL) ON FRAME 68 SHEAR CLIP NEAR STRINGER 17L. MAINTENANCE FABRICATED AND INSTALLED REPAIR ON FRAME 68 SHEAR CLIP STRI
- [SDR C2XA09SH376](https://openairdocs.org/sdr/C2XA09SH376), Oct 21, 2009: FLOOR SUPPORT. DAMAGED. SHV - DURING C-CHECK CENTER OMEGA BEAM AT FRAMES 22-23 HAS TOOLING MARKS. MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM AT FRAMES 18-24 IAW EMB-145 SRM 51-
- [SDR C2XA09SH375](https://openairdocs.org/sdr/C2XA09SH375), Oct 21, 2009: FITTING. CRACKED. SHV - DURING C-CHECK SHEAR CLIP CRACKED AT FRAME 73 BETWEEN STRINGERS 8R AND 9R. MAINTENANCE REMOVED AND REPLACED SHEAR CLIP AT FRAME 73 BETWEEN STRINGERS 8R AN
- [SDR C2XA09TY217](https://openairdocs.org/sdr/C2XA09TY217), Aug 7, 2009: DUCT. UNSECURE. AIRCRAFT DIVERTED INTO TYS FOR A BLEED 1 LEAK. SECURED DUCT LINE TO PAC 1 AND HEAT EXCHANGER. OPS AND LEAK CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE
- [SDR C2XA09RI119](https://openairdocs.org/sdr/C2XA09RI119), Jun 21, 2009: STRUT. LEAKING. FLIGHT 2554 - EWR - FLIGHT CREW REPORTED LANDING GEAR AIR GROUND FAIL MESSAGE ON EICAS AND GEAR WOULD NOT RETRACT. CREW PERFORMED AIR RETURN AND LANDED ACFT UNE
- [SDR C2XA09CL013](https://openairdocs.org/sdr/C2XA09CL013), Jan 27, 2009: ELECTRONIC UNIT. FAULTY. CLE FLIGHT NR 2890 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MSG DURING CLIMBOUT. THE ACFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MX R&R THE LANDIN
- [SDR C2XA09IA015](https://openairdocs.org/sdr/C2XA09IA015), Jan 9, 2009: ELECTRONIC UNIT. INOPERATIVE. MFE - FLIGHT 2451, THE CREW REPORTED THAT A LANDING GEAR LEVER DISAGREE MSG WAS RECEIVED AND THE LANDING GEAR DID NOT RETRACT. THE ACFT LANDED AT MFE WITHOUT IN
- [SDR C2XA09IA018](https://openairdocs.org/sdr/C2XA09IA018), Jan 9, 2009: CONTROL LEVER. INOPERATIVE. CREW REPORTED THAT A LANDING GEAR LEVER DISAGREE MESSAGE WAS RECEIVED AND THE LANDING GEAR DID NOT RETRACT. THE ACFT LANDED WITHOUT INCIDENT WHERE MX INSPECTED 
- [SDR C2X2008F00041](https://openairdocs.org/sdr/C2X2008F00041), Sep 4, 2008: LIGHT. BURNED. AC WAS IN FOR A SERVICE/ ROUTINE CHECK AND THE LOWER SERVICE DOOR EMERGENCY EXIT SIGN WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT
- [SDR C2XA08CL008](https://openairdocs.org/sdr/C2XA08CL008), Jan 15, 2008: RELAY. BURNED. CMH FLIGHT NR 3142 - THE CREW REPORTED PITOT 2 INOP MESSAGE ON THE EICAS IN FLIGHT AT 25000. THEY ALSO REPORTED SMOKE IN COCKPIT AND CABIN. EMERGENCY DECLARED A
- [SDR C2XA07TY069](https://openairdocs.org/sdr/C2XA07TY069), Nov 14, 2007: BATTERY PACK. INOPERATIVE. NR 3 EMERGENCY LIGHT BATTERY INOP. REMOVED AND REPLACED NR 3 EMERGENCY LIGHT BATTERY IAW EMB 145MM 33-50-04. OPS CHECK GOOD, AIRCRAFT RELEASED AND RETURNED TO S

All 69: https://openairdocs.org/deregistered/N14923-2018-09-25/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 20040409009269I](https://openairdocs.org/incident/20040409009269I), Apr 9, 2004: Emb EMB145LR (N14923), Houston, TX, Minor damage. (-23) Marshaller directed aircraft from remote parking spot without properly clearing area. Aircraft proceeded along center taxiway stripe and left wing tip…

## Other aircraft with N14923

- [Cancelled 1941-04-22](https://openairdocs.org/deregistered/N14923-1941-04-22): Douglas DC2, S/N 1403. Exported to United Kingdom. Owner: [British Purchasing Commission](https://openairdocs.org/faa-owner/BRITISH%20PURCHASING%20COMMISSION)

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