# N16911: 2001 Embraer EMB-145LR, registration cancelled 2023-05-16

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 16, 2023
- 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: 145446
- Year built: 2001
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 13, 2001
- Certificate issued: December 20, 2017
- Last registry action: April 7, 2023
- Mode S code: A115B2
- 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/N16911
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=16911
- Page: https://openairdocs.org/deregistered/N16911-2023-05-16

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 (49)

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

- [SDR ASOA2019080955094](https://openairdocs.org/sdr/ASOA2019080955094), Aug 5, 2019: CONTROLLER. FAILED. SMOKE IN COCKPIT FROM SUSPECT ELECTRICAL SHORT. FLT 4276. MX FOUND CAPTAIN`S WX RADAR CONTROLLER OVERHEATED. REMOVED AND REPLACED CAPT SIDE WX RADAR CONTROLLER 
- [SDR ASOA201908024040](https://openairdocs.org/sdr/ASOA201908024040), Aug 2, 2019: ACM. NOT REPORTED. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ACM, OPERATIONALLY TESTED WITH NO DEFECTS AND THE AIRCRAFT WAQS APPROVED FOR RETURN TO SERVICE. *** SDR CLOSED *
- [SDR ASOA2019080524040](https://openairdocs.org/sdr/ASOA2019080524040), Aug 2, 2019: ACM. FAILED. FLIGHT 4284 THE CREW REPORTED HEAVY DARK SMOKE IN THE COCKPIT AND ELECTRICAL BURN SMELL, WE DECLARED AN EMERGENCY, SMOKE CAME OUT OF CAPTAIN'S VENT BY WINDOW RA
- [SDR ASOA201907265088](https://openairdocs.org/sdr/ASOA201907265088), Jul 26, 2019: BATTERY PACK. DISCHARGED. DURING COMPLETION OF ADS-B MOD LINE IT WAS DISCOVERED THAT SEVERAL INSIDE AND OUTSIDE EMERGENCY LIGHTS DID NOT ILLUMINATE. MX REMOVED AND REPLACED #2 AND #4 EME
- [SDR ASOA201805225136](https://openairdocs.org/sdr/ASOA201805225136), May 22, 2018: TURBINE WHEEL. DAMAGED. CREW REPORTED SMOKE IN COCKPIT AND CABIN WITH APU RUNNING. MX FOUND DAMAGE TO APU TURBINE WHEEL. MX REMOVED AND REPLACED APU WITH OPERATIONAL CHECK GOOD. A/C WA
- [SDR ASOA201708014046](https://openairdocs.org/sdr/ASOA201708014046), Aug 1, 2017: INVERTER. INOPERATIVE. THE CREW REPORTED AN EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT INVERTER BEHIND THE F/A COAT CLOSET, OPERATIONALLY 
- [SDR ASOA201701240026](https://openairdocs.org/sdr/ASOA201701240026), Jan 24, 2017: TRUNNION. CRACKED. DURING C-CK. LT MLG AFT UPPER TRUNNION IS CRACKED. REMOVED AND REPLACED LT MLG AFT UPPER TRUNNION IAW ETD2016-145-11089 IN ET/EC W/O 4822331. AIRCRAFT WAS APPRO
- [SDR ASOA201701240016](https://openairdocs.org/sdr/ASOA201701240016), Jan 24, 2017: TRUNNION. CRACKED. DURING C-CK. RT MLG AFT UPPER TRUNNION IS CRACKED. REMOVED AND REPLACED RT MLG AFT UPPER TRUNNION IAW ETD216-145-110849 IN EC/TC W/O 482331. AIRCRAFT WAS APPROV
- [SDR ASOA20151022054](https://openairdocs.org/sdr/ASOA20151022054), Oct 22, 2015: WIRE HARNESS. DAMAGED. PILOT REPORTED A FUNNY ODOR IN CABIN NEAR MCD. MAINTENANCE R & R CABIN CEILING LIGHT HARNESS AT SEAT 1A WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SER
- [SDR ASOA20140404031](https://openairdocs.org/sdr/ASOA20140404031), Apr 4, 2014: CRADLE. BROKEN. THE CREW REPORTED BURNING ODOR AFTER TAKEOFF BUT NO VISIBLE SMOKE. ODOR DISSIPATED AFTER A FEW MINUTES. MAINTENANCE REPLACED THE F/O FLASHLIGHT BRACKET. OPS CHE
- [SDR ASOA20140403029](https://openairdocs.org/sdr/ASOA20140403029), Apr 3, 2014: CRADLE. FAULTY. THE CREW REPORTED SMOKE ODOR AFTER TAKEOFF. SMOKE DISIPATED AFTER 5 MINUTES. ALSO REPORTED ODOR ON DESCENT. THEY ALSO NOTED THE LOCALIZER DID NOT WORK ON CAPTAI
- [SDR C2XA10RI0146](https://openairdocs.org/sdr/C2XA10RI0146), Nov 21, 2010: WIRE. UNSECURE. FLIGHT 2369 - EWR - FLIGHT CREW REPORTED BAGG SMOKE LIGHT REMAINS ILLUMINATED AFTER APU FIRE TEST BUTTON IS RELEASED. EWR MX RE-SECURED WIRE TO PLUG AND PERFORM
- [SDR C2XA10IA288](https://openairdocs.org/sdr/C2XA10IA288), Nov 10, 2010: BAR. FAILED. IAH - FLIGHT 2129, THE CREW REPORTED A APU CONTACTOR FAIL MESSAGE ON EICAS. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT
- [SDR C2XA10SH389](https://openairdocs.org/sdr/C2XA10SH389), Nov 7, 2010: SUPPORT. CORRODED. SHV - DURING C-CHECK LT UPPPER SEAT TRACK SUPPORT HAS CORROSION (LEVEL 2 LOCAL) AT FRAME 50. MAINTENANCE PERFORMED REPAIR AT LT UPPER SEAT TRACK SUPPORT AT FRAM
- [SDR C2XA10SH388](https://openairdocs.org/sdr/C2XA10SH388), Nov 7, 2010: SUPPORT. CORRODED. SHV - DURING C-CHECK LT UPPER SEAT TRACK SUPPORT HAS CORROSION (LEVEL 2 LOCAL) AT FRAME 46. MAINTENANCE PERFORMED REPAIR AT LT UPPER SEAT TRACK SUPPORT AT FRAME
- [SDR C2XA10SH387](https://openairdocs.org/sdr/C2XA10SH387), Nov 7, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM LWR FLANGE FRAME 22-23 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM LOWER FLANGE FRAME 22-23 
- [SDR C2XA10SH386](https://openairdocs.org/sdr/C2XA10SH386), Nov 7, 2010: ATTACH BRACKET. WORN. SHV - DURING C-CHECK RT AILERON HAS 3 MIGRATED HAT BUSHINGS AT PCA ATTACH BRACKET ON AILERON. MAINTENANCE REMOVED AND REPLACED RT AILERON PCA ATTACHMENT BRACKET
- [SDR C2XA10SH385](https://openairdocs.org/sdr/C2XA10SH385), Nov 7, 2010: ATTACH BRACKET. LOOSE. SHV - DURING C-CHECK RT AILERON HAT BUSHING AT DAMPNER ATTACH BRACKET ON AILERON LOOSE. MAINTENANCE REMOVED AND REPLACED RT AILERON DAMPNER ATTACH BRACKET ON AI
- [SDR C2XA10SH384](https://openairdocs.org/sdr/C2XA10SH384), Nov 7, 2010: FRAME. CRACKED. SHV - DURING C-CHECK RT COCKPIT FRAME 10 CRACK BELOW DV WINDOW CUTOUT. MAINTENANCE REMOVED AND REPLACED RT COCKPIT FRAME 10 BELOW DV WINDOW IAW EMB-145 SRM 51-4
- [SDR C2XA10CL043](https://openairdocs.org/sdr/C2XA10CL043), Mar 15, 2010: SMOKE DETECTOR. NO TEST. CLE FLIGHT 2785 THE CREW REPORTED THE LAV SMOKE WOULD NOT TEST. MAINTENANCE REPLACED THE LAV SMOKE DETECTOR / SENSOR. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA09IA162](https://openairdocs.org/sdr/C2XA09IA162), Jun 21, 2009: LIGHT. INOPERATIVE. MCI - DURING MAINTENANCE INSPECTION THE FORWARD EMERGENCY LIGHT ABOVE THE F/A SEAT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LI
- [SDR C2XA09CL060](https://openairdocs.org/sdr/C2XA09CL060), May 6, 2009: TURBINE WHEEL. CRACKED. DURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 1 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASO
- [SDR C2XARI041](https://openairdocs.org/sdr/C2XARI041), Mar 6, 2009: INVERTER. INOPERATIVE. FLIGHT 2521 - EWR - FLIGHT CREW REPORTED LAST 3 FLOOR PROXIMITY LIGHT STRIPS NOT WORKING. EWR MX REMOVED AND REPLACED INVERTER NR 6 AND PERFORMED OPERATIONAL CH
- [SDR C2XA09RI025](https://openairdocs.org/sdr/C2XA09RI025), Feb 11, 2009: UNKNOWN. ODOR. FLT 2077 - FLIGHT CREW REPORTED LIGHT BEHIND CAPTAIN'S CLOCK AND RADIO PANEL WAS FLICKING AND BURNING ODOR WAS DETECTED. EWR MX PERFORMED VISUAL INSPECTION ON C
- [SDR C2XA08TY136](https://openairdocs.org/sdr/C2XA08TY136), Nov 29, 2008: LIGHT. INOPERATIVE. THE 1ST FLOOR EMERGENCY PROXIMITY STRIP WILL NOT ILLUMINATE. REMOVED AND REPLACED PROX LIGHT STRIP IAW EMB 145 AMM 33-50-08. OPS CHECK GOOD. AIRCRAFT STILL IN C
- [SDR C2XA08TY133](https://openairdocs.org/sdr/C2XA08TY133), Nov 20, 2008: HINGE BRACKET. CRACKED. RT HORIZONTAL STAB HINGE PIN RETENTION EAR IS CRACKED. REMOVED AND REPLACED RT HORZ STAB HINGE PIN BRACKET IAW EMB 145 SRM 51-40-02. AIRCRAFT STILL IN C CHECK.
- [SDR C2XA08TY132](https://openairdocs.org/sdr/C2XA08TY132), Nov 12, 2008: WIRE. BROKEN. NR 1 EMERGENCY LIGHT STRIP ON THE FLOOR HAD BROKEN WIRES. REMOVED AND REPLACED LIGHT STRIP IAW EMB 145 AMM 33-50-12. AIRCRAFT STILL IN C-CHECK.
- [SDR C2XA08CL120](https://openairdocs.org/sdr/C2XA08CL120), Nov 4, 2008: ACM. FAULTY. CLE FLIGHT 2368 THE CREW REPORTED SMOKE IN THE CABIN WHILE ON THE GROUND WITH THE APU RUNNING AND PACKS ON. MAINTENANCE INSPECTED AND REPLACED THE RIGHT AIR CYC
- [SDR C2XA08IA040](https://openairdocs.org/sdr/C2XA08IA040), Jan 29, 2008: SKIN. CRACKED. IAH - DURING PREFLIGHT INSPECTION THE RIGHT WING SKIN WAS FOUND TO BE CRACKED AT THE CENTER HINGE POINT CUTOUT FOR THE GROUND SPOILER. MAINTENANCE INSPECTED THE
- [SDR C2XA07CL003](https://openairdocs.org/sdr/C2XA07CL003), Jan 10, 2007: HUB CAP. UNSECURE. CLE FLIGHT 2098 AFTER TAKEOFF THE RIGHT MAIN GEAR DID NOT INDICATE LOCKED AND THE LANDING GEAR LEVER DISAGREE MESSAGE APPEARED ON THE EICAS. CYCLED GEAR 3 TIMES
- [SDR C2XA05TY051](https://openairdocs.org/sdr/C2XA05TY051), Aug 27, 2005: WIRE HARNESS. SHORTED. FLT NUMBER 2703, LANDING GEAR AIR/GROUND FAIL EICAS MESSAGE ON CLIMB-OUT. ACFT RETURNED TO FIELD. MAINTENANCE REMOVED AND REPLACED THE NLG PROXIMITY SENSE HARNE
- [SDR C2XA05BT060](https://openairdocs.org/sdr/C2XA05BT060), Aug 17, 2005: LANDING GEAR. COLLAPSED. CREW REPORTED, "NOSE LANDING GEAR COLLASPED ON PUSH BACK FROM GATE." MAINTENANCE TROUBLESHOOTING AND REPAIRING AIRCRAFT.
- [SDR C2XA04IA146](https://openairdocs.org/sdr/C2XA04IA146), Nov 20, 2004: POWER SUPPLY. DISCHARGED. IAH - FLIGHT 2680, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHTS AFT OF ROW SEVEN (7) WERE INOPERATIVE. MAINTENANCE REMOVED AND REPL
- [SDR C2XA04IA147](https://openairdocs.org/sdr/C2XA04IA147), Nov 20, 2004: POWER SUPPLY. DISCHARGED. IAH - FLIGHT 2680, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHTS AFT OF ROW SEVEN (7) WERE INOPERATIVE. MAINTENANCE REMOVED AND REPL
- [SDR C2XA04IA148](https://openairdocs.org/sdr/C2XA04IA148), Nov 20, 2004: POWER SUPPLY. INOPERATIVE. IAH- FLIGHT 2680, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHTS AFT OF ROW SEVEN (7) WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLA
- [SDR C2XA03TY209](https://openairdocs.org/sdr/C2XA03TY209), Dec 15, 2003: CONTROL UNIT. MALFUNCTIONED. PILOT REPORTED THE LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. THE AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED T
- [SDR C2XA03CL184](https://openairdocs.org/sdr/C2XA03CL184), Oct 29, 2003: CONTROL LEVER. FAULTY. THE CREW REPORTED DURING CLIMBOUT THE GEAR WOULD NOT RETRACT. THE CREW RECYCLED THE GEAR AND THE GEAR RETRACTED. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. M
- [SDR CX2A03RI003](https://openairdocs.org/sdr/CX2A03RI003), Sep 30, 2003: BULB. BURNED OUT. ROUTINE INSPECTION MAINTENANCE FOUND EMERGENCY LIGHT OVER THE LEFT HAND WING WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT BULB AND 
- [SDR C2XA03IA068](https://openairdocs.org/sdr/C2XA03IA068), Jun 28, 2003: BATTERY. DISCHARGED. IAH- DURING PREFLIGHT THE CREW NOTED THAT THE EMERGENCY LIGHTS FAILED TO ILLUMINATE. IAH- MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY BATTERY PACK, PERF
- [SDR C2XA03IA046](https://openairdocs.org/sdr/C2XA03IA046), May 1, 2003: SIGN. INOPERATIVE. EWR- ON POSTFLIGHT THE CREW NOTED THAT THE EMERGENCY EXIT SIGN ABOVE THE SERVICE DOOR FAILED TO ILLUMINATE. EWR- MAINTENANCE REMOVED AND REPLACED THE EMERGENCY 
- [SDR C2XA03IA027](https://openairdocs.org/sdr/C2XA03IA027), Mar 15, 2003: LIGHT. INOPERATIVE. FLT 2380 - DURING POSTFLIGHT INSPECTION THE AFT EMERGENCY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OP
- [SDR C2XA03TY035](https://openairdocs.org/sdr/C2XA03TY035), Mar 14, 2003: STRINGER. GOUGED. TYS, During a scheduled inspection a gouge was found at stringer 19R center fuselage IV. Maintenance blended, performed dye-pen inspection, fabricated and insta
- [SDR C2XA03TY034](https://openairdocs.org/sdr/C2XA03TY034), Mar 13, 2003: BEAM. CORRODED. DURING A SCHEDULED 1-C INSPECTION THE OMEGA BEAM AT FRAME 20 WAS CORRODED. MAINTENANCE CUT OUT DAMAGED AREA, FAB, ALODINE, PRIME, PAINTED AND INSTALLED REPAIRED
- [SDR C2XA03TY033](https://openairdocs.org/sdr/C2XA03TY033), Mar 13, 2003: SUPPORT. CORRODED. TYS DURING A SCHEDULED 1C INSPECTION THE TOP CAP ANGLE BEAM WAS CORRODED.MAINT.REPLACED RAMP ANGLE BEAM FOR TOP CAP IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS A
- [SDR C2XA03CL025](https://openairdocs.org/sdr/C2XA03CL025), Feb 3, 2003: CDU. FAILED. PHL FLIGHT#2062 THE CREW REPORTED #1 CDU/FMS FAILED IN FLIGHT.AFTER LANDING A STRONG BURNING/SMOKE ODOR IN COCKPIT AND CABIN WAS NOTICED.MAINTENANCE REPLACED TH
- [SDR C2XA02CL221](https://openairdocs.org/sdr/C2XA02CL221), Nov 4, 2002: LIGHT. INOPERATIVE. THE CREW REPORTED THE EMERGENCY EXIT LIGHT IN THE GALLEY WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA02CL197](https://openairdocs.org/sdr/C2XA02CL197), Oct 10, 2002: WIRE. LOOSE. CLE FLIGHT#3194 THE CREW REPORTED THE EMERGENCY EXIT LIGHT AT THE GALLEY SERVICE DOOR WAS INOPERATIVE.MAINTENANCE INSPECTED AND RESECURED LOOSE WIRE ON THE EMER
- [SDR C2XA02BT059](https://openairdocs.org/sdr/C2XA02BT059), Oct 2, 2002: INVERTER. LOOSE. EWR---CO3039, CREW REPORTED, THE GALLEY DOOR EMERGENCY LIGHT WAS INOPERATIVE....MAINTENANCE FOUND A LOOSE CONNECTOR AND RESECURED THE CANNON PLUG. OPS.CHECKED S
- [SDR C2XA02CL187](https://openairdocs.org/sdr/C2XA02CL187), Sep 24, 2002: INVERTER. INOPERATIVE. CLE FLIGHT#4368 THE CREW REPORTED THE EMERGENCY EXIT LIGHT ON THE GALLEY DOOR WAS INOPERATIVE.MAINTENANCE REPLACED THE EMERGENCY LIGHT INVERTER.OPERATIONAL CHEC

## 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 20050801025349I](https://openairdocs.org/incident/20050801025349I), Aug 1, 2005: Emb EMB145LR (N16911), Newark, NJ, Substantial damage. (-23) On August 16, 2005, aircraft N16911 was outbound while being towed, the aircraft experienced a nose landing gear collapse. Damage to aircraft consisted…

## Other aircraft with N16911

- [Cancelled 1947-03-25](https://openairdocs.org/deregistered/N16911-1947-03-25): Grumman G-21A, S/N 1002. Exported to Bahamas. Owner: [Pan American Airways Inc](https://openairdocs.org/faa-owner/PAN%20AMERICAN%20AIRWAYS%20INC), [Miami, FL](https://openairdocs.org/faa-place/FL/Miami)

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