# N11548: 2002 Embraer EMB-145LR, registration cancelled 2022-02-23

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 23, 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: 145565
- Year built: 2002
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 22, 2002
- Certificate issued: October 16, 2017
- Last registry action: June 18, 2020
- Mode S code: A041CB
- 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/N11548
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=11548
- Page: https://openairdocs.org/deregistered/N11548-2022-02-23

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 (67, newest 50)

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

- [SDR ASOA2019121945118](https://openairdocs.org/sdr/ASOA2019121945118), Dec 14, 2019: YOKE. CRACKED. DURING MX INSPECTION THE #1 ENGINE FORWARD UPPER YOKE FITTING WAS FOUND CRACKED. MX R&R THE #1 ENGINE FORWARD UPPER YOKE FITTING IAW STS EA26-2014-063. A/C WAS 
- [SDR ASOA201908305098](https://openairdocs.org/sdr/ASOA201908305098), Aug 30, 2019: LIGHT. INOPERATIVE. DURING MX INSPECTION THE RIGHT OVER WING EMERGENCY LIGHT WAS NOT ILLUMINATING. MX REMOVED AND REPLACED RT OVER WING EMERGENCY LIGHT IAW AMM 33-50-07 OPS CHECKED
- [SDR ASOA201908305097](https://openairdocs.org/sdr/ASOA201908305097), Aug 30, 2019: LIGHT. INOPERATIVE. DURING MX INSPECTION THE EMERGENCY LIGHT SYSTEM BATTERY POWERED FLOOR PROXIMITY STRIP AT SEATS 18 THROUGH 20 NOT ILLUMINATING ( EMERGENCY LIGHTING SYSTEM (BATTE
- [SDR ASOA2019021974006](https://openairdocs.org/sdr/ASOA2019021974006), Feb 17, 2019: LIGHT. INOPERATIVE. IAH - DURING MAINTENANCE INSPECTION THE R/H EMERGENCY OVERWING EXTERIOR LIGHT WAS FOUND TO BE INOP. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY
- [SDR ASOA201802144010](https://openairdocs.org/sdr/ASOA201802144010), Feb 14, 2018: ENGINE. FAILED. THE CREW REPORTED AN UINCOMMANDED SHOUTDOWN OF THE NR 2 ENGINE DURING FLIGHT. THE AIRCRAFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE R
- [SDR ASOA201711064058](https://openairdocs.org/sdr/ASOA201711064058), Nov 6, 2017: WIRE. BROKEN. THE AISLE EMERGENCY LIGHT STRIP BETWEEN SEATS 8A - 9A WAS FOUND TO HAVE A BROKEN WIRE. REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP, OPS TESTED WITH NO DEFECT
- [SDR ASOA201710047019](https://openairdocs.org/sdr/ASOA201710047019), Oct 2, 2017: FRAME. DAMAGED. FRAME 62 DAMAGED BETWEEN STRINGERS 4R & 5R. REMOVED AND REPLACED THE DAMAGED SECTION OF THE FRAME. RETURNED TO SERVICE
- [SDR ASOA201710047020](https://openairdocs.org/sdr/ASOA201710047020), Sep 30, 2017: FUSE. BLOWN. EMERGENCY LIGHT ON COCKPIT CEILING PANEL 225CTC INOPERATIVE. REMOVED AND REPLACED THE FUSE IN THE NR 1 EMERGENCY LIGHT BATTERY TRAY. OPS CHECKED GOOD.
- [SDR ASOA201709107013](https://openairdocs.org/sdr/ASOA201709107013), Sep 10, 2017: FRAME. DAMAGED. A/C IS IN FOR A C-CHECK INSPECTION WHEN THE INSPECTOR FOUND FRAME 62 DAMAGED BETWEEN STRINGER 4R AND 5R. MAINTENANCE R&R THE DAMAGED SECTION OF FRAME 62 AT STR.
- [SDR ASOA201611054107](https://openairdocs.org/sdr/ASOA201611054107), Nov 5, 2016: DRAG ANGLE. CRACKED. DURING AN A CHECK INSPECTION, THE RIGHT VERTICAL STAB DRAG ANGLE WAS FOUND TO BE CRACKED AT FRAME 76, MAINTENANCE REMOVED AND REPLACED THE AFFECTED DRAG ANGLE, 
- [SDR ASOA201611054105](https://openairdocs.org/sdr/ASOA201611054105), Nov 5, 2016: SKIN. CRACKED. DURING AN A CHECK INSPECTION, THE RIGHT AFT FUSELAGE SKIN WAS FOUND TO HAVE A 20MM CRACK AT FRAME 75 STRINGER 1R, MAINTENANCE PERFORMED A DOUBLER REPAIR TOP THE
- [SDR ASOA20161004054C](https://openairdocs.org/sdr/ASOA20161004054C), Oct 4, 2016: LAMP. INOPERATIVE. DURING ROUTINE MAINTENANCE, THE RIGHT AFT EXTERNAL EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE LAMPS. OPS CHECKED GOOD.
- [SDR ASOA201704044016](https://openairdocs.org/sdr/ASOA201704044016), Apr 4, 2016: SKIN. GOUGED. DURING MAINTENANCE INSPECTION, THE AIRCRAFT SKIN WAS FOUND TO BE GOUGED UNDER THE GPU DOOR. MAINTENANCE CUT OUT THE DAMAGE AND INSTALLED A DOUBLER AND FILLER RE
- [SDR ASOA20160306008R](https://openairdocs.org/sdr/ASOA20160306008R), Mar 6, 2016: CHARGER. INOPERATIVE. DURING MAINTENANCE INSPECTION, THE AFT OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE R & R THE NR 4 BATTERY CHARGER ASSY WITH OPS CHECK GOOD. AC
- [SDR ASOA20150611033](https://openairdocs.org/sdr/ASOA20150611033), Jun 11, 2015: BATTERY. DISCHARGED. THE CREW REPORTED EMERGENCY LIGHTS WERE INOPERATIVE AT ROW 18. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OPS CHECKS WERE GOOD.
- [SDR ASOA20141118132](https://openairdocs.org/sdr/ASOA20141118132), Nov 18, 2014: OUTFLOW VALVE. FAULTY. CREW REPORTED LOSS OF PRESSURIZATION AND CABIN ALTITUDE EXCEEDED 10000 FT ALONG WITH O2 MASKS DEPLOY. MAINTENANCE R & R THE PNUEMATIC OUTFLOW VALVE AND MANUAL P
- [SDR ASOA20140910098](https://openairdocs.org/sdr/ASOA20140910098), Sep 10, 2014: BATTERY PACK. INOPERATIVE. BOTH OF THE AFT EXTERIOR EMERGENCY LIGHTS AND LAST TWO EMERGENCY FLOOR PATH LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE R & R THE NR 4 EMERGENCY LIGHT SYSTEM BAT
- [SDR ASOA20140109003](https://openairdocs.org/sdr/ASOA20140109003), Jan 9, 2014: A/C PACK. SMOKE. THE CREW REPORTED NR 2 PACK INOPERATIVE. WHEN RUNNING, SMOKE IN CABIN. MAINTENANCE INSPECTED AND PERFORMED OPS CHECKS. NO DEFECTS OR SMOKE NOTED.
- [SDR ASOA20131127133](https://openairdocs.org/sdr/ASOA20131127133), Nov 27, 2013: VALVE. FAULTY. PILOT REPORTED BLEED VALVE NR 2 CLOSED ADVISORY MESSAGE PRESENT DURING CLIMBOUT, HIGH ALTITUDE WARNING PRESENT AT 17,000 FT, UNABLE TO REMAIN PRESSURIZED, DESCE
- [SDR ASOA20131029123](https://openairdocs.org/sdr/ASOA20131029123), Oct 29, 2013: BULB. BLOWN. DURING MX INSPECTION THE CEILING EMERGENCY LIGHT ABOVE SEAT ROW 12BC WAS FOUND INOPERATIVE. MX R & R THE 12BC LIGHT ASSY BULB WITH OPS CHECK SUCCESSFUL. ACFT WA
- [SDR ASOA201228111](https://openairdocs.org/sdr/ASOA201228111), Nov 28, 2012: LAMP. INOPERATIVE. DURING A-CHECK INSPECTION, IT WAS FOUND THAT THE LT OVERWING AND ROW 12 EMERGENCY LIGHTS WERE INOPERATIVE. MX R & R THE LIGHT BULBS IN BOTH THE LT OVERWING AND 
- [SDR ASOA20121002109](https://openairdocs.org/sdr/ASOA20121002109), Oct 2, 2012: SEAL. DAMAGED. CABIN ALTITUDE CLIMBED TO 11900 IN AUTO MODE, AND CONTINUED IN MANUAL MODE TO 12100. DIVERTED. MX FOUND CARGO DOOR SEAL DAMAGED, REMOVED AND INSTALLED CARGO DOO
- [SDR ASOA20120831072](https://openairdocs.org/sdr/ASOA20120831072), Aug 31, 2012: GCU. FAULTY. THE CREW REPORTED SMOKE IN THE COCKPIT & SPARKS COMING OUT OF APU STARTER GENERATOR APU OUTLET. MAINTENANCE REPLACED THE APU GENERATOR CONTROL UNIT AND REPLACED
- [SDR ASOA20120604081](https://openairdocs.org/sdr/ASOA20120604081), Jun 4, 2012: STIFFENER. CRACKED. DURING A-CHECK INSPECTION, APU FIREWALL WAS FOUND TO BE CRACKED AT THE TOP OF THE RT VERTICLE STIFFENER. MX PERFORMED A DOUBLER REPAIR, AND THE ACFT WAS APPROVE
- [SDR ASOA20120605083](https://openairdocs.org/sdr/ASOA20120605083), Jun 3, 2012: FIREWALL. CRACKED. DURING A-CHECK INSPECTION, THE APU FIREWALL WAS FOUND TO BE CRACKED ON THE RT STIFFENER. MX PERFORMED A DOUBLER REPAIR AND THE ACFT WAS APPROVED FOR RETURN TO S
- [SDR ASOA20120602082](https://openairdocs.org/sdr/ASOA20120602082), Jun 2, 2012: SKIN. DENTED. DURING A-CK INSPECTION, A DENT WAS FOUND IN THE LT REAR FUSELAGE BETWEEN FRAMES 77 AND 78 AND STRINGERS 15L & 16L. MX PERFORMED A DOUBLER REPAIR, AND THE ACFT W
- [SDR ASOA201201310011](https://openairdocs.org/sdr/ASOA201201310011), Jan 31, 2012: LIGHT. INOPERATIVE. DURING ROUTINE MX, THE AFT AISLE PATH EMERGENCY LIGHT STRIP WAS FOUND INOPERATIVE. MX REPLACED THE AFT EMERGENCY LIGHT STRIP. OPS CHECKS WERE GOOD.
- [SDR ASOA201201016004](https://openairdocs.org/sdr/ASOA201201016004), Jan 9, 2012: CONTROLLER. INTERMITTENT. THE CREW REPORTED THAT DURING FLIGHT THE CABIN EMERGENCY LIGHTS ILLUMINATED INTERMITTENTLY. THE ACFT LANDED WITHOUT INCIDENT WHERE MX REPLACED THE EMERGENCY LIG
- [SDR ASOA20111215021](https://openairdocs.org/sdr/ASOA20111215021), Dec 15, 2011: LIGHT. MALFUNCTIONED. THE CREW REPORTED THE EMERGENCY LIGHTS COME ON IN NORMAL POSITION. MX INSPECTED AND REPLACED RELAY KO275, REPLACED NR 2 AND NR 4 EMERGENCY LIGHT BATTERY CHARGER
- [SDR ASOA2011121300015](https://openairdocs.org/sdr/ASOA2011121300015), Dec 13, 2011: CONTROL MODULE. FAULTY. THE CREW REPORTED THE EMERGENCY EXIT LIGHTS WOULD NOT TURN OFF. MX INSPECTED AND REPLACED THE EMERGENCY LIGHT CONTROL MODULE AND THE NR 2 EMERGENCY LIGHT BATTER
- [SDR ASOA20111212013](https://openairdocs.org/sdr/ASOA20111212013), Dec 12, 2011: LIGHT. INTERMITTENT. THE CREW REPORTED THE CABIN EMEREGENCY LIGHTS COME ON INTERMITENTLY. MX INSPECTED AND PERFORMED OPS CHECK OF THE EMERGENCY LIGHTS. NO DEFECTS FOUND.
- [SDR ASOA20111208008](https://openairdocs.org/sdr/ASOA20111208008), Dec 8, 2011: DIODE. FAILED. DURING ROUTINE MX INSPECTION, IT WAS DISCOVERED ALL THE EMERGENCY LIGHTS ILLUMINATED WITH SWITCH IN THE ARM POSITION. MX R & R DIODE CR0220 AND THE F/A CONTROL 
- [SDR ASOA20111205010](https://openairdocs.org/sdr/ASOA20111205010), Dec 5, 2011: CONTROL MODULE. FAULTY. WHEN THE EMERGENCY LIGHT SWITCH WAS SELECTED TO THE "ARM" POSITION THE EMERGENCY LIGHTING ILLUMINATED. MX REPLACED THE EMERGENCY LIGHT CONTROL MODULE, OPERATION
- [SDR C2XA11TY168](https://openairdocs.org/sdr/C2XA11TY168), Nov 7, 2011: CONTROLLER. MALFUNCTIONED. FLIGHT CREW SMELLED SMOKE. REMOVED AND REPLACED WINDSHIELD HEATER CONTROLLER IAW EMB 145 30-42-01. OPS CHECK GOOD.
- [SDR C2XA11CL105](https://openairdocs.org/sdr/C2XA11CL105), Apr 25, 2011: CONNECTOR. CORRODED. THE CREW REPORTED A TAKEOFF CONFIG WARNING MESSAGE FOR SPOILERS OPEN ON TAKEOFF ROLL.SPOILERS THEN KEPT ALTERNATING OPEN/CLOSED. THE CREW ABORTED TAKEOFF. MX IN
- [SDR C2XA11CL103](https://openairdocs.org/sdr/C2XA11CL103), Apr 25, 2011: PROXIMITY SWITCH. FAULTY. CREW REPORTED A SPOILER FAIL MESSAGE IN LEVEL CRUISE FLIGHT, THEN PERFORMED THE CFM CHECK LIST AND THE MESSAGE CONTINUED WITH A NOTED CHANGE IN OPEN/CLOSED MESS
- [SDR C2XA11IA040](https://openairdocs.org/sdr/C2XA11IA040), Mar 2, 2011: ELECTRONIC UNIT. INOPERATIVE. OMA - FLIGHT 3044, THE CREW REPORTED A LANDING GEAR AIR/GRND FAIL EICAS MESSAGE AND THE GEAR WOULD NOT RETRACT ON CLIMB. THE AIRCRAFT RETURNED TO OMA WHERE IT L
- [SDR C2XA10RI083](https://openairdocs.org/sdr/C2XA10RI083), Jun 18, 2010: BATTERY. OVERTEMP. FLIGHT 3073 - GRR - FLIGHT CREW REPORTED NR 2 MAIN BATTERY OVERTEMP INDICATION ON EICAS. CREW LANDED ACFT UNEVENTFULLY. MX REMOVED AND REPLACED NR 2 MAIN BATTER
- [SDR C2XA09CL134](https://openairdocs.org/sdr/C2XA09CL134), Oct 12, 2009: WIRE. FAULTY. YYZ - FLT 2305 - THE CREW REPORTED A BAG SMOKE WARNING MESSAGE ON THE EICAS. MAINTENANCE INSPECTED AND RELEASED THE AIRCRAFT IAW MEL 26-15-00. MAINTENANCE REPAI
- [SDR C2XA09RI168](https://openairdocs.org/sdr/C2XA09RI168), Oct 2, 2009: SMOKE DETECTOR. FALSE ACTIVATION. FLIGHT 2897 - YQB - FLIGHT CREW REPORTED BAG SMOKE INDICATION ON EICAS. MX RESET THE SYSTEM AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO R
- [SDR C2XA09IA245](https://openairdocs.org/sdr/C2XA09IA245), Sep 29, 2009: SMOKE WARNING. FALSE ACTIVATION. CAE - FLIGHT 2622, THE CREW REPORTED A BAG SMOKE INDICATION. THE CREW PLACED THE BAGGAGE SMOKE DETECTOR ON MEL. THE AIRCRAFT SUBSEQUENTLY LANDED AT IAH WHERE MA
- [SDR C2XA09TY240](https://openairdocs.org/sdr/C2XA09TY240), Sep 18, 2009: RADAR. DEFECTIVE. TYS - AIRCRAFT DIVERTED INTO TYS FROM CLE DUE TO RADAR FAILING IN FLIGHT. A/C WAS SWAPPED TO ANOTHER A/C AND CONTINUED ON. MAINTENANCE REMOVED AND REPLACED THE 
- [SDR C2XA09CL086](https://openairdocs.org/sdr/C2XA09CL086), Jun 16, 2009: SMOKE DETECTOR. MALFUNCTIONED. THE CREW REPORTED A BAGGAGE SMOKE DETECTION LIGHT REMAINS ON. MX CONFIRMED NO SMOKE AND PLACED ON MEL 26-15-00. FLT NR 2600 MX RESET BAGGAGE SMOKE DETECTOR. OPS
- [SDR C2XA09TY114](https://openairdocs.org/sdr/C2XA09TY114), Jun 16, 2009: SMOKE DETECTOR. MALFUNCTIONED. TYS FOR IAH - THE BAGGAGE SMOKE DETECTOR LIGHT REMAINS ON ALL THE TIME. THE AIRCRAFT WAS RELEASED IAW MEL 26-15-00 CAT (C) CONTROL NUMBER 171219.
- [SDR C2XA09TY099](https://openairdocs.org/sdr/C2XA09TY099), May 27, 2009: FRAME SPLICE. CORRODED. TYS - AIRCRAFT CURRENTLY IN A C-CHECK STATUS, INSPECTION FOUND CORROSION AT FR 65 UNDER CARGO SEAL. MAINTENANCE REPAIRED FR 65 UNDER CARGO SEAL IAW EC 5330-0145
- [SDR C2XA09TY100](https://openairdocs.org/sdr/C2XA09TY100), May 26, 2009: SILL. CORRODED. TYS - AIRCRAFT CURRENTLY GOING INTO C-CHECK, INSPECTION FOUND THE CARGO SILL CORRODED. MAINTENANCE REMOVED AND REPLACED THE CARGO SILL IAW EMB 145SRM 51-40-02. 
- [SDR C2XA09TY097](https://openairdocs.org/sdr/C2XA09TY097), May 23, 2009: SILL. CORRODED. TYS - DURING C-CHECK THE LT FLOOR SILL UNDER FRAME 18 WAS FOUND CORRODED. THE LT FLOOR SILL WAS REMOVED AND REPLACED IAW EMB 135/145 SRM 51-40-02.
- [SDR C2XA09TY096](https://openairdocs.org/sdr/C2XA09TY096), May 23, 2009: THRESHOLD. CORRODED. TYS - DURING C-CHECK CORROSION WAS FOUND UNDER THE PAX DOOR THRESHOLD. SMALL SURFACE CORROSION WAS BLENDED OUT AND PRIMED AND PAINTED IAW EMB 135/145 SRM 51-10-
- [SDR C2XA09TY095](https://openairdocs.org/sdr/C2XA09TY095), May 23, 2009: SILL. CORRODED. TYS - DURING C-CHECK CORROSION WAS FOUND AT THE LT WALL FLOOR SILL AT FRAME 30 TO FRAME 35. THE SILL WAS REMOVED AND REPLACED IAW EMB 135/145 SRM 51-40-02.
- [SDR C2XA09TY094](https://openairdocs.org/sdr/C2XA09TY094), May 22, 2009: FLOOR SUPPORT. CORRODED. TYS - DURING C-CHECK, CORROSION WAS FOUND ON THE LT OMEGA BEAM AT NUT PLATE AT PAX DOOR ENTRY WAY. THE AREA WAS REPAIRED IAW EC5320-01449. A/C STILL IN C-CHECK.

All 67: https://openairdocs.org/deregistered/N11548-2022-02-23/reports.md

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