# N19554: 2002 Embraer EMB-145LR, registration cancelled 2022-03-03

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 3, 2022
- Exported to: Nigeria
- Status when cancelled: Valid registration
- Airframe: [Embraer EMB-145LR](https://openairdocs.org/model/embraer-emb-145lr) (registry code 3260212)
- Engine: [Rolls-Royce AE-3007A1P](https://openairdocs.org/engine/rolls-royce-ae-3007a1p) (registry code 54571)
- Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (OpenAirDocs)
- Serial number: 145587
- Year built: 2002
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 26, 2002
- Certificate issued: December 14, 2018
- Last registry action: September 30, 2021
- Mode S code: A17DE2
- Owner when cancelled: [United Airlines Inc](https://openairdocs.org/faa-owner/UNITED%20AIRLINES%20INC)
- Location: [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago)
- Owner type: Corporation
- Owner's area on the map: 41.8813° N, 87.6375° W: Placed by OpenAirDocs at the center of ZIP code 60606, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N19554
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=19554
- Page: https://openairdocs.org/deregistered/N19554-2022-03-03

From the FAA registry file of November 5, 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 (58, newest 50)

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

- [SDR ASOA2020050414017](https://openairdocs.org/sdr/ASOA2020050414017), May 1, 2020: BATTERY PACK. DISCHARGED. IAH- FLIGHT 4289 DURING MAINTENANCE INSPECTION THE R/H EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE #2 EMERGENCY LIGHT POWE
- [SDR ASOA20200205004](https://openairdocs.org/sdr/ASOA20200205004), Feb 1, 2020: LAMP. ODOR. PILOT REPORTED ELECTRICAL SMELL BY SEAT 4CD AND 5CD. ITEM PLACED ON MEL. ON 2/3/20 MX REMOVED AND REPLACED SIDEWALL LAMP AND RESEATED CONNECTOR WITH OPERATIONAL
- [SDR ASOA2018091845203](https://openairdocs.org/sdr/ASOA2018091845203), Sep 14, 2018: INVERTER. DEFECTIVE. PILOT REPORTED "FLOOR PATH EMERG LIGHT A/C LEFT AT WINDOW EXIT AND EXIT CEILING BACK SIDE OF LIGHT CAME ON IN FLIGHT" MX REMOVED AND REPLACED THE NR 5 INVERTER 
- [SDR ASOA201807257142](https://openairdocs.org/sdr/ASOA201807257142), Jul 25, 2018: BRACE. SCORED. TYS A/C IS IN C-CHECK WHEN INSPECTION FOUND THE RT MLG SIDE BRACE FWD AFT FITTING BEARING BORE SCORED AND HAD A SMALL AREA OF CORROSION. ALL WORK WAS ACCOMPLISH
- [SDR ASOA201807257141](https://openairdocs.org/sdr/ASOA201807257141), Jul 25, 2018: BEARING. WORN. TYS A/C IS IN C-CHECK WHEN INSPECTION FOUND EVIDENCE OF SOME WEAR ON THE VERTICAL STAB BORES OR SPHERICAL BEARINGS. MAINTENANCE PERFORMED OPS CHECKS OF BOTH DIH
- [SDR ASOA201807237139](https://openairdocs.org/sdr/ASOA201807237139), Jul 21, 2018: TRUNNION. CORRODED. LT AND RT MLG AFT TRUNNION FITTINGS INTERNAL DIAMETER HAS CORROSION. COMPLETED REWORK OF THE MLG TRUNNION IN ACCORDANCE WITH ETD 2018-145-079169.
- [SDR ASOA201807177131](https://openairdocs.org/sdr/ASOA201807177131), Jul 17, 2018: SKIN. DAMAGED. TYS A/C IS IN C-CHECK WHEN INSPECTION FOUND THE RIGHT ELEVATOR LOWER OUTBOARD FLANGE AT SCREW HOLE DAMAGED. MAINTENANCE REPAIRED DAMAGED AREA BY CUTTING OUT DAM
- [SDR ASOA201807177130](https://openairdocs.org/sdr/ASOA201807177130), Jul 17, 2018: SKIN. DENTED. TYS A/C IS IN FOR A C-CHECK WHEN INSPECTION FOUND A DENT IN THE NR 2 LEADING EDGE LEFT WING. MAINTENANCE REPAIRED AREA BY CUTTING OUT THE DENT AND FABRICATED A 
- [SDR ASOA201807177129](https://openairdocs.org/sdr/ASOA201807177129), Jul 17, 2018: SKIN. CRACKED. TYS A/C IS IN FOR A C-CHECK WHEN INSPECTION FOUND THE LEFT REAR EXTERNAL FUSELAGE BETWEEN FRAME 75 AND 76,STRINGER 2L TO 4L CRACKED. MAINTENANCE PERFORMED A REP
- [SDR ASOA201807177128](https://openairdocs.org/sdr/ASOA201807177128), Jul 17, 2018: STRINGER. CRACKED. TYS A/C IS IN FOR A C-CHECK WHEN INSPECTION FOUND A CRACK AT STRINGER 2L AND FRAME 75. MAINTENANCE REPAIRED AREA IAW ETD 2018-145-077021. ALL WORK ACCOMPLISHED 
- [SDR ASOA201807097122](https://openairdocs.org/sdr/ASOA201807097122), Jul 9, 2018: FITTING. WORN. A/C IS IN C-CHECK WHEN INSPECTION FOUND RUDDER 1 UPPER ACTUATOR ATTACH POINT UPPER LUG HAT BUSHING MISSING AND FELL OUT. MAINTENANCE FOUND THE ATTACH POINT ELON
- [SDR ASOA201807257140](https://openairdocs.org/sdr/ASOA201807257140), Jun 29, 2018: FRAME. CRACKED. CP SIDE FRAME ABOVE WS SIDE POST CRACKED. SPLICED IN NEW SECTION OF FRAME ABOVE WS SIDE POST IN ACCORDANCE WITH ETD 2018-145-072956.
- [SDR ASOA20160522050](https://openairdocs.org/sdr/ASOA20160522050), May 22, 2016: INVERTER. INOPERATIVE. FLIGHT CREW REPORTED THAT THE EMERGENCY LIGHT ON THE BULKHEAD AT SEAT 3D WAS INOPERATIVE. THE ACFT WAS FERRIED WHERE MAINTENANCE R & R THE NR 3 EMERGENCY LIGHT 
- [SDR ASOA20160324019](https://openairdocs.org/sdr/ASOA20160324019), Mar 24, 2016: BATTERY. INOPERATIVE. EMERGENCY FLOOR LIGHTS AT ROW 8-11 AND EXIT LIGHT AT OVERWING EXITS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 3 EMERGENCY LIGHT BATTERY. OPS CHECKS WE
- [SDR ASOA20151201068C](https://openairdocs.org/sdr/ASOA20151201068C), Dec 1, 2015: POWER SUPPLY. FAULTY. THE CREW REPORTED EMERGENCY LIGHTS REMAIN ON AT ROW 5-18. MAINTENANCE INSPECTED AND REPLACED THE NR 3 EMERGENCY LIGHT BATTERY POWER SUPPLY. OPS CHECKS WERE GOOD
- [SDR ASOA20141121135](https://openairdocs.org/sdr/ASOA20141121135), Nov 21, 2014: RELAY. INOPERATIVE. THE CREW REPORTED A BAGGAGE SMOKE INDICATION IN FLIGHT ON EICAS AND EXT/BAGG PUSHBUTTON. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MAINTE
- [SDR ASOA20141121134](https://openairdocs.org/sdr/ASOA20141121134), Nov 21, 2014: RELAY. INOPERATIVE. THE CREW REPORTED A BAGGAGE SMOKE INDICATION IN FLIGHT ON EICAS AND EXT/BAG PUSHBUTTON. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MAINTEN
- [SDR ASOA20141113115](https://openairdocs.org/sdr/ASOA20141113115), Nov 12, 2014: LIGHT. INOPERATIVE. EMERGENCY LIGHT INOPERATIVE. R & R LIGHT. OPS CHECKED GOOD. ACFT RELEASED AND RETURNED TO SERVICE.
- [SDR ASOA20140616071](https://openairdocs.org/sdr/ASOA20140616071), Jun 16, 2014: INVERTER. INOPERATIVE. DURING MX INSPECTION THE EMERGENCY LIGHT BELOW THE COCKPIT STEP WAS DISCOVERED INOPERATIVE. MX R & R THE NR 1 EMERGENCY LIGHT SYS INVERTER AND LIGHT ASSY WITH O
- [SDR ASOA20140424082](https://openairdocs.org/sdr/ASOA20140424082), Apr 23, 2014: POWER SUPPLY. INOPERATIVE. LEFT AND RT OVERWING EMERGENCY LIGHTS INOPERATIVE. R & R NR 4 BATTERY POWER SUPPLY. OPS CHECKED GOOD.
- [SDR ASOA20140419036](https://openairdocs.org/sdr/ASOA20140419036), Apr 19, 2014: BOLT. SHEARED. DURING FLIGHT, AFTER A SERIES OF BUMPS OR WHAT SOUNDED LIKE A BACKFIRE. NR 2 ENGINE ITT SPIKED INTO THE RED FOLLOWED BY NR 2 ENGINE OUT. RESTART WAS SUCCESSFUL,
- [SDR ASOA20140207022](https://openairdocs.org/sdr/ASOA20140207022), Feb 7, 2014: BEARING. MIGRATED. DURING C CHECK, INSPECTION FOUND RT AILERON PCA ATTACHMENT BRACKET BEARING MIGRATED. MAINTENANCE R & R THE RT PCA BRACKET IAW EC 5750-01177.
- [SDR ASOA20130612059](https://openairdocs.org/sdr/ASOA20130612059), Jun 12, 2013: ROLLER. OUT OF ADJUST. PILOT REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN. MX ADJUSTED THE MAIN CABIN DOOR ROLLERS WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SER
- [SDR ASOA20130427043R](https://openairdocs.org/sdr/ASOA20130427043R), Apr 27, 2013: CHARGER. FAULTY. CREW REPORTED SECTIONS OF THE FLOOR EMERGENCY LIGHTS TURNING ON AND OFF INTERMITTENTLY. MX R & R THE NR 3 BATTERY CHARGER ASSY AND BATTERY PACK WITH OPS CHECKS 
- [SDR ASOA20121009080](https://openairdocs.org/sdr/ASOA20121009080), Oct 9, 2012: CONTACTOR. FAULTY. F/A SMELLED ELECTRIC BURNING ODOR AFTER LANDING. MX INSPECTED AND REPLACED NOSE LANDING LIGHT CONTACTOR K0237. OPS CHECKED WERE GOOD.
- [SDR ASOA20111212014](https://openairdocs.org/sdr/ASOA20111212014), Dec 12, 2011: GENERATOR. FAULTED. DURING CLIMB THE CREW REPORTED THAT THE NR 3 GENERATOR DROPPED OFF LINE. THE ACFT WAS OPERATING WITH THE NR1 GENERATOR ON MEL AND WITH THE NR 3 DROPPING OFF LIN
- [SDR C2XA11TY163](https://openairdocs.org/sdr/C2XA11TY163), Oct 24, 2011: SKIN. DAMAGED. AIRCRAFT STRUCK BY LIGHTNING. PERFORMED LIGHTNING STRIKE INSPECTION IAW EMB 145 5-50-01. REMOVED AND REPLACED DAMAGE RIVET AT FRAME 8 STRINGER 16L-17L. REPAIRED
- [SDR C2XA11RI166](https://openairdocs.org/sdr/C2XA11RI166), Oct 13, 2011: BATTERY. DISCHARGED. FLT 6145 IAD SECTION OF AISLE PATH LIGHTING INOP AROUND EMERGENCY EXIT ROW 12 NOTED. IAD MX REMOVED AND REPLACED NR 3 EMERGENCY LIGHT BATTERY POWER SUPPLY IAW E
- [SDR C2XA11CL230](https://openairdocs.org/sdr/C2XA11CL230), Oct 13, 2011: CHARGER. FAULTY. THE CREW REPORTED THE AILE PATH EMERGENCY LIGHTS AT ROW 8 THRU 12 WILL NOT GO OFF. MAINTENANCE INSPECTED AND REPLACED THE NR 3 EMERGENCY LIGHT BATTERY CHARGER A
- [SDR C2XA11IA231](https://openairdocs.org/sdr/C2XA11IA231), Oct 4, 2011: CONNECTOR. DIRTY. MCI - DURING MAINTENANCE INSPECTION THE EMERGENCY EXIT LIGHTS OVER BOTH EXITS AND THE AISLE PATH LIGHTS FROM RO 8 TO 12 WERE FOUND TO BE INOPERATIVE. MAINTENANC
- [SDR C2XA11CL178](https://openairdocs.org/sdr/C2XA11CL178), Jul 31, 2011: BATTERY. DISCHARGED. DURING ROUTINE MAINTENANCE THE EMERGENCY AISLE PATH LIGHTING WAS FOUND INOPERATIVE AT THE EXIT ROW. MAINTENANCE REPLACED THE NR 3 EMERGENCY LIGHT BATTERY. OPERA
- [SDR C2XA11TY038](https://openairdocs.org/sdr/C2XA11TY038), Mar 23, 2011: SMOKE DETECTOR. ACTIVATED. LAV SMOKE INDICATION ON THE EICAS SHORTLY AFTER TAKEOFF. FOGGY CABIN/POSSIBLY DE-ICING FLUID IN AIR CONDITIONING SYSTEM. PERFORMED ENGINE RUNS IAW RR MM71-00-80
- [SDR C2XA10RI087](https://openairdocs.org/sdr/C2XA10RI087), Jun 24, 2010: TRIM SWITCH. BROKEN. FLIGHT 2476 - EWR - FLIGHT CREW REPORTED BACK UP PITCH TRIM SWITCH INOPERATIVE. CREW PERFORMED AIR RETURN UNEVENTFULLY. EWR MX REMOVED AND REPLACED SWITCH AND P
- [SDR C2XA10IA173](https://openairdocs.org/sdr/C2XA10IA173), Jun 13, 2010: CONTROL MODULE. FAULTY. THE CREW REPORTED THAT WHEN THE EMERGENCY LIGHT SWITCH WAS PLACED IN THE ARMED POSITION THE CABIN EMERGENCY LIGHTS WOULD COME ON. MAINTENANCE REMOVED AND REPLAC
- [SDR C2XA10SH180](https://openairdocs.org/sdr/C2XA10SH180), May 20, 2010: ATTACH BRACKET. WORN. SHV - DURING C-CHECK THE RT AILERON PCA ATTACHMENT BRACKET WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MAINTENANCE REMOVED AND REPLACED THE AFFE
- [SDR C2XA10SH179](https://openairdocs.org/sdr/C2XA10SH179), May 20, 2010: SKIN. CRACKED. SHV - DURING C-CHECK THE AFT RT SKIN WAS FOUND TO BE CRACKED AT A RIVET AT FRAME 79 AND STRINGER 4R. MAINTENANCE PERFORMED A BUSHING REPAIR IAW EC5330-02130. TH
- [SDR C2XA09CL139](https://openairdocs.org/sdr/C2XA09CL139), Oct 28, 2009: SWITCH. INOPERATIVE. CLE FLT 2580 - THE CREW REPORTED A BLEED 1 VALVE CLOSED MESSAGE AFTER TAKEOFF. COULD NOT GET THE NR 1 BLEED VALVE TO OPEN. MAINTENANCE INSPECTED AND REPLACED TH
- [SDR C2XA09TY058](https://openairdocs.org/sdr/C2XA09TY058), Apr 3, 2009: TUBE. LEAKING. AIRCRAFT ON CLIMBOUT FROM EWR TO TYS REACH A HIGH ITT. MAINTENANCE REPLACED THE RT COMPRESSOR AIR TUBE ON THE E1 IAW ROLLS ROYCE MM 75-00-00, OPS AND LEAK CHECK
- [SDR C2XA07ON050](https://openairdocs.org/sdr/C2XA07ON050), Dec 21, 2007: VALVE. MALFUNCTIONED. FLT 421 - SMF TO GEG - FLIGHT CREW REPORTED PACK 1 VALVE FAILED TO CLOSED NUMEROUS TIMES ON CLIMB. MX PERSONNEL REMOVED AND REPLACED NR 1 PACK VALVE, OPERATIONA
- [SDR C2XA07ON021](https://openairdocs.org/sdr/C2XA07ON021), Sep 3, 2007: CONNECTOR. UNSECURE. FLT 524 - MCI TO RDU - DURING PREFLIGHT CK, FLIGHT CREW DISCOVERED THE EMERGENCY LIGHTS WILL NOT SHUT OFF. MX PERSONNEL INSPECTED AND FOUND CONNECTOR ON NR 3 EM
- [SDR C2XA07IA195](https://openairdocs.org/sdr/C2XA07IA195), Sep 2, 2007: BATTERY PACK. DISCHARGED. MCI - DURING MAINTENANCE INSPECTION THE NUMBER 5 & 6 AISLE PATH EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE
- [SDR C2XA07IA185](https://openairdocs.org/sdr/C2XA07IA185), Aug 9, 2007: POWER SUPPLY. DISCHARGED. AUS - FLIGHT 308, DURING PREFLIGHT INSPECTION AN EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SU
- [SDR C2XA07IA182](https://openairdocs.org/sdr/C2XA07IA182), Aug 2, 2007: BATTERY PACK. DISCHARGED. AUS - DURING MAINTENANCE INSPECTION, THE FORWARD THREE AISLE PATH LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERG
- [SDR C2XA07BT019](https://openairdocs.org/sdr/C2XA07BT019), Feb 19, 2007: BATTERY. DISCHARGED. EWR LOG SQUAWK FLT 2665 EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY IAW EMB145 AMM 37-50-04. OPS CHECK GOOD.
- [SDR C2XA06SH008](https://openairdocs.org/sdr/C2XA06SH008), Jan 28, 2006: FRAME. CORRODED. SHV - DURING C-CHECK THE CARGO DOOR INTERNAL FRAME WAS FOUND TO BE CORRODED AROUND A NUT PLATE. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS E
- [SDR C2XA06SH007](https://openairdocs.org/sdr/C2XA06SH007), Jan 28, 2006: FIREWALL. CHAFED. SHV - DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CHAFED AT THE 6 O`CLOCK POSITION. MAINTENANCE BLENDED OUT THE DAMAGED AREA AND PERFORMED A SHIM REPAIR IAW
- [SDR C2XA05BT082](https://openairdocs.org/sdr/C2XA05BT082), Nov 19, 2005: BULB. BLOWN. DURING SERVICE AND ROUTINE INSPECTION CHECK, MAINTENANCE FOUND THAT THE LEFT OVERWING EMERGENCY LIGHT WAS NOT WORKING. REMOVED AND REPLACED BULB IN LEFT OVERWIN
- [SDR C2XA04TY044](https://openairdocs.org/sdr/C2XA04TY044), Mar 4, 2004: SILL. CORRODED. TYS DURING A SCHEDULED 1C INSPECTION THE SERVICE DOOR FWD SILL HAS AREAS OF CORROSION. MAINT BLENDED AFT AREA AND FOUND TO BE WITHIN LIMITS; ALODINED, PRIMED, P
- [SDR C2XA04TY043](https://openairdocs.org/sdr/C2XA04TY043), Mar 4, 2004: PLATE. CORRODED. TYS DURING A SCHEDULED 1C INSPECTION THE FWD DIGITAL PLATE HAD AREAS OF CORROSION. MAINT CUT THE DAMAGED AREA OUT, FAB DOUBLERS AND DRILLED HOLES ON NEW FWD DIG
- [SDR C2XA04TY042](https://openairdocs.org/sdr/C2XA04TY042), Mar 4, 2004: STIFFENER. CRACKED. TYS DURING A SCHEDULED 1C INSPECTION THE RT UPPER STIFFENER ON THE APU FIREWALL WAS FOUND CRACKED. MAINT FABBED A DOUBLER AND STOPPED DRILL CRACK. INSTALL DOUBL

All 58: https://openairdocs.org/deregistered/N19554-2022-03-03/reports.md

## Other aircraft with N19554

- [Cancelled 1989-05-05](https://openairdocs.org/deregistered/N19554-1989-05-05): Piper J-2, S/N 1754. N-number assigned, not yet registered

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