# N11544: 2002 Embraer EMB-145LR, registration cancelled 2022-03-03

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 3, 2022
- Exported to: Bahamas
- 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: 145557
- Year built: 2002
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: January 26, 2002
- Certificate issued: October 14, 2021
- Last registry action: October 14, 2021
- Mode S code: A041C7
- Owner when cancelled: [Enterprise Aircraft Finance LLC](https://openairdocs.org/faa-owner/ENTERPRISE%20AIRCRAFT%20FINANCE%20LLC)
- Location: [Clayton, MO](https://openairdocs.org/faa-place/MO/Clayton)
- Owner type: LLC
- Owner's area on the map: 38.6443° N, 90.3281° W: Placed by OpenAirDocs at the center of ZIP code 63105, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N11544
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=11544
- Page: https://openairdocs.org/deregistered/N11544-2022-03-03

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 (90, newest 50)

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

- [SDR ASOA2020012395002](https://openairdocs.org/sdr/ASOA2020012395002), Jan 19, 2020: HANDLE. OUT OF ADJUST. CREW REPORTED MCD HANDLE JAMMED AND DOOR COULD NOT BE OPENED FROM THE INSIDE. GATE AGENT WAS ABLE TO OPEN THE DOOR FROM THE OUTSIDE AFTER SEVERAL ATTEMPTS. MX A
- [SDR ASOA201912247139](https://openairdocs.org/sdr/ASOA201912247139), Dec 19, 2019: YOKE. CRACKED. WHILE IN C CHECK, DISCOVERED THE RT ENGINE UPPER FORWARD PYLON YOKE CRACKED. REMOVED AND REPLACED YOKE FITTING. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE.
- [SDR ASOA201912037136](https://openairdocs.org/sdr/ASOA201912037136), Dec 3, 2019: RIB. CRACKED. L/H WING RIB 21 CRACKED. REPAIRED RIB 21 BU CUTTING OUT THE CRACKED FLANGE, FABRICATING, INSTALLING DOUBLER AND SHIM. AIRCRAFT STILL IN C CHECK
- [SDR ASOA201910257127](https://openairdocs.org/sdr/ASOA201910257127), Oct 25, 2019: FLOOR SUPPORT. CORRODED. TYS A/C IS IN C-CHECK WHEN INSPECTION FOUND THE CENTER OMEGA BEAM CORRODED AT FRAME 20.MAINTENANCE REPAIRED THE CENTER OMEGA BEAM BY CUTTING OUT THE DAMAGED ARE
- [SDR ASOA2018101515246](https://openairdocs.org/sdr/ASOA2018101515246), Oct 11, 2018: LIGHT. ARCED. FLT 4096 MKE-EWR PILOT REPORTED "STRONG ELECTRICAL SMELL DURING CRUISE FLIGHT. SMELL INIDENTIFIED 1 MIN DURATION THEN DISSIPATED". MX RELAMPED 4 EACH CEILING AN
- [SDR ASOA2018062203036](https://openairdocs.org/sdr/ASOA2018062203036), Jun 20, 2018: ACTUATOR. CRACKED. THE CREW REPORTED THE NR 1 HYDRAULIC QUANTITY WAS LOW DURING FLIGHT. AFTER LANDING THE CREW RECEIVED A NR 1 HYDRAULIC FAIL MESSAGE. MAINTENANCE INSPECTED AND FO
- [SDR ASOA201710065129](https://openairdocs.org/sdr/ASOA201710065129), Oct 6, 2017: BATTERY PACK. INOPERATIVE. PILOT REPORTED EMERGENCY LIGHTS OVER EXIT ROW OUT. MX REMOVED AND REPLACED NR 4 EMERGENCY BATTERY AND CHARGER WITH OPERATIONAL CHECK GOOD. ACFT WAS APPROVED FOR
- [SDR ASOA201708297012](https://openairdocs.org/sdr/ASOA201708297012), Aug 29, 2017: SEAL. LEAKING. ACFT HAD A STRONG OIL ODOR WHILE THE PACKS WERE BEING POWERED BY THE APU. MAINTENANCE R & R THE STARTER GENERATOR OIL SEAL ASSEMBLY IAW CMM 49-26-01-030-037 AND
- [SDR ASOA201704045031](https://openairdocs.org/sdr/ASOA201704045031), Apr 4, 2017: LAMP. BURNED OUT. PILOT REPORTED AN ELECTRICAL ODOR IN FWD CLOSET. MX REMOVED AND REPLACED TWO BURNED OUT GALLEY WORK AREA FLOURESCENT LAMPS. PERFORMED GENERAL VISUAL INSPECTION 
- [SDR ASOA201703285029](https://openairdocs.org/sdr/ASOA201703285029), Mar 28, 2017: BATTERY PACK. DISCHARGED. DURING SCHEDULED MX INSPECTION THE ROW 18 TOP CENTER AISLE FORWARD EMERGENCY SIGN WILL NOT ILLUMINATE. MX REMOVED AND REPLACED THE NR 4 BATTERY PACK WITH OPERAT
- [SDR ASOA201703085015](https://openairdocs.org/sdr/ASOA201703085015), Mar 8, 2017: BATTERY PACK. INOPERATIVE. PILOT REPORTED THE EMERGENCY LIGHTS ABOVE EXIT ROW FORWARD SIDE AND ON THE FLOOR WERE INOPERATIVE. MX REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY PACK
- [SDR ASOA201703023037](https://openairdocs.org/sdr/ASOA201703023037), Mar 2, 2017: STRUCTURE. CORRODED. CENTER FUSELAGE AT FRAME 59 CORRODED. REPLACED SRM 51-40-02.
- [SDR ASOA201703023036](https://openairdocs.org/sdr/ASOA201703023036), Mar 2, 2017: GUSSET. CORRODED. CENTER FUSELAGE BETWEEN FRAMES 49 AND 50 GUSSET CORRODED. THE GUSSET WAS REPLACED IAW SRM 51-40-02.
- [SDR ASOA201703023035](https://openairdocs.org/sdr/ASOA201703023035), Mar 2, 2017: CHANNEL. CORRODED. CENTER FUSELAGE SERVICE DOOR LOWER CHANNEL SURFACE CORRODED. CHANNEL REPLACED IAW SRM 51-40-02.
- [SDR ASOA201703023034](https://openairdocs.org/sdr/ASOA201703023034), Mar 2, 2017: DOOR FRAME. CORRODED. PAX DOOR CORRODED AROUND NUT PLATES TOP FRAME. DOOR FRAME REPAIRED IAW ETD2017-145-012899.
- [SDR ASOA201703023033](https://openairdocs.org/sdr/ASOA201703023033), Mar 2, 2017: SHEAR TIE. CORRODED. CARGO DOOR FORWARD L SHAPE DOOR SURROUND CORRODED BETWEEN STRINGERS 15 - 17L. SHEAR TIE REPLACED AND FRAME REPAIRED IAW SRM 53-31-04, ITEM 4.
- [SDR ASOA201703023032](https://openairdocs.org/sdr/ASOA201703023032), Mar 2, 2017: SKIN. CORRODED. REAR FUSELAGE SKIN UNDER FORWARD NR 2 RADIO ALTIMETER CORRODED. SKIN AREA REPAIRED IAW SRM 53-00-23, ITEM 3.
- [SDR ASOA201703023031](https://openairdocs.org/sdr/ASOA201703023031), Mar 2, 2017: STRUCTURE. CORRODED. CENTER FUSELAGE BETWEEN FRAMES 49 AND 50, STRUCTURE CORRODED. REPLACED IAW SRM 51-40-02.
- [SDR ASOA201703023030](https://openairdocs.org/sdr/ASOA201703023030), Mar 2, 2017: ANGLE. CORRODED. CENTER FUSELAGE BETWEEN FRAME 23 AND 24 LOWER WEB ANGLE CORRODED. THE ANGLE WAS REPLACED IAW SRM 53-22-10 AND SRM 51-40-02.
- [SDR ASOA201703023029](https://openairdocs.org/sdr/ASOA201703023029), Mar 2, 2017: BEAM. CORRODED. CARGO DOOR LOWER BEAM CORRODED. BEAM REPLACED IAW SRM 51-40-02.
- [SDR ASOA201703023028](https://openairdocs.org/sdr/ASOA201703023028), Mar 2, 2017: PLATE. CORRODED. REAR FUSELAGE CARGO DOOR FORWARD SIDE PLATE CORRODED. PLATE REPLACED IAW SRM 53-31-10 AND 51-40-02.
- [SDR ASOA201703023027](https://openairdocs.org/sdr/ASOA201703023027), Mar 2, 2017: DOUBLER. CORRODED. WATER SERVICING POINT DOUBLER CORRODED. DOUBLER REPLACED IAW SRM 51-40-02.
- [SDR ASOA201703023026](https://openairdocs.org/sdr/ASOA201703023026), Mar 2, 2017: DOOR FRAME. CORRODED. CORROSION AROUND PAX DOOR NUT PLATES, BOTTOM FRAME. FRAME REPAIRED IAW ETD2017-145-012912 REF: FCBS 52-10-01-001.
- [SDR ASOA201612263089](https://openairdocs.org/sdr/ASOA201612263089), Dec 26, 2016: BATTERY. INOPERATIVE. DURING ROUTINE MAINTNENACE, BOTH OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WER
- [SDR ASOA20160931024](https://openairdocs.org/sdr/ASOA20160931024), Sep 30, 2016: BATTERY. DISCHARGED. A/C WAS IN FOR AN A-CHECK WHEN INSPECTION FOUND THE LAST 3 FLOOR EMERGENCY STRIPS OUT. MAINTENANCE R&R THE BATTERY SUPPLY IAW AMM 25-22-04; IPC 33-50-04, FIGURE
- [SDR ASOA20160920072H](https://openairdocs.org/sdr/ASOA20160920072H), Sep 20, 2016: BATTERY PACK. DISCHARGED. DURING MAINTENANCE INSPECTION, THE AISLE PATH LIGHTING AT 18A TO 24A WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 4 EMERGENCY LIGHT BATTERY PACK, OPERA
- [SDR ASOA20160714063](https://openairdocs.org/sdr/ASOA20160714063), Jul 14, 2016: BATTERY PACK. DISCHARGED. DURING MAINTENANCE INSPECTION, THE LT AND RT OVERWING EMERGENCY LIGHTS AND AFT FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 3 EMERGENCY L
- [SDR ASOA20160617040C](https://openairdocs.org/sdr/ASOA20160617040C), Jun 17, 2016: BATTERY. DISCHARGED. DURING ROUTINE MAINTENANCE, BOTH AFT OVERWING EMERGENCY LIGHTS WERE FOUND DIM. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OPS CHECKS WERE GOOD.
- [SDR ASOA20160411016R](https://openairdocs.org/sdr/ASOA20160411016R), Apr 11, 2016: CHARGER. INOPERATIVE. DURING MAINTENANCE INSPECTION, THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE DISCOVERED INOPERATIVE. MAINTENANCE R & R THE NR 4 EMERGENCY LIGHT BATTERY CHARGER WI
- [SDR ASOA20150823047](https://openairdocs.org/sdr/ASOA20150823047), Aug 23, 2015: PUMP. LEAKING. THE CREW REPORTED HYDRAULIC LOW QUANITY ENROUTE. MAINTENANCE INSPECTED AND REPLACED THE LEAKING NR 1 ENGINE DRIVEN HYDRAULIC PUMP. OPS CHECKS WERE GOOD.
- [SDR ASOA20150621021](https://openairdocs.org/sdr/ASOA20150621021), Jun 18, 2015: BATTERY. INOPERATIVE. AFT EMERGENCY LIGHT BATTERY INOPERATIVE. R & R EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD. ACFT RELEASED AND RETURNED TO SERVICE.
- [SDR ASOA20150408011](https://openairdocs.org/sdr/ASOA20150408011), Apr 8, 2015: FUSE. BLOWN. LT AND RT OVERWING EMERGENCY LIGHTS INOPERATIVE. R & R FUSE ON NR 4 EMERGENCY LIGHT BATTERY TRAY. OPS CHECK GOOD.
- [SDR ASOA20150123013H](https://openairdocs.org/sdr/ASOA20150123013H), Jan 23, 2015: CHARGER. INOPERATIVE. DURING 2A INSPECTION, THE LT OVERWING EMEREGNCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 4 EMERGENCY LIGHT BATTERY CHARGER, OPERATIONALLY TES
- [SDR ASOA20150122012H](https://openairdocs.org/sdr/ASOA20150122012H), Jan 22, 2015: DRAG ANGLE. CRACKED. DURING 2A INSPECTION THE RT FUSELAGE TO VERTICLE STAB DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE R & R THE AFFECTED DRAG ANGLE, AND THE ACFT WAS APPROVED F
- [SDR ASOA20141027088C](https://openairdocs.org/sdr/ASOA20141027088C), Oct 27, 2014: WIRE HARNESS. DAMAGED. THE CREW REPORTED CABIN OVERHEAD LIGHTS WERE INOPERATIVE WITH A BURNING ODOR. MAINTENANCE INSPECTED AND REPLACED OVERHEAD LIGHT ELECTRICAL WIRING HARNESS AT SEA
- [SDR ASOA20140527094](https://openairdocs.org/sdr/ASOA20140527094), May 27, 2014: PRESSURE SWITCH. INOPERATIVE. RUDDER SYS 1 INOPERATIVE EICAS CAUTION MESSAGE DURING TAXI OUT. R & R RUDDER PRESSURE SWITCH IAW AMM 27-23-04. OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO
- [SDR ASOA20140305030](https://openairdocs.org/sdr/ASOA20140305030), Mar 5, 2014: SLEEVE. FAILED. PILOT REPORTED THE CABIN DEPRESSURIZED IN AIR MAX DELTA P1 PSI. MAINTENANCE R & R NR 1 PACK HEAT EXCHANGER SLEEVE AND PERFORMED OPS CHECK GOOD. ACFT WAS APPROVE
- [SDR ASOA20130117006](https://openairdocs.org/sdr/ASOA20130117006), Jan 17, 2013: CHARGER. INOPERATIVE. BOTH OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. ITEM WAS MOVED AND PLACED ON MEL 33-50-00-1. LATER THAT DAY, MX R & R NR4 EMERGENCY LIGHT POWER SUPPLY WI
- [SDR C2XA11TY143](https://openairdocs.org/sdr/C2XA11TY143), Sep 14, 2011: LIGHT. BLOWN. TYS - A/C IN FOR A SERVICE/ROUTINE WHEN INSPECTION FOUND THE EMERGENCY LIGHT INOP AT SEAT 11 TO SEAT 18. MAINTENANCE RELAMPED THE EMERGENCY LIGHT IAW EMB 145 AM
- [SDR C2XA11RI141](https://openairdocs.org/sdr/C2XA11RI141), Aug 3, 2011: FITTING. LOOSE. FLIGHT 2887 - IAD - FLIGHT CREW REPORTED FUEL ODOR IN CABIN AND COCKPIT DURING TAXI AND PUSHBACK. IAD MX FOUND FITTING LOOSE ON LOW PRESSURE SWITCH. MX TIGHTENE
- [SDR C2XA11CL110](https://openairdocs.org/sdr/C2XA11CL110), Apr 29, 2011: WIRE HARNESS. FAULTY. ORD FLT 5935 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE AFTER TAKEOFF. THEY WERE UNABLE TO RETRACT GEAR. THE AIRCRAFT RETURNED TO ORD AND LANDED W
- [SDR C2XA11CL068](https://openairdocs.org/sdr/C2XA11CL068), Mar 10, 2011: APU. FAILED. THE CREW REPORTED AN APU FAIL MESSAGE ALONG WITH A ELECTRICAL SMELL. MAINTENANCE INSPECTED AND REPLACED THE APU. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA11CL067](https://openairdocs.org/sdr/C2XA11CL067), Mar 9, 2011: UNKNOWN. MALFUNCTIONED. ORD FLT 5929 THE CREW REPORTED THE AIRCRAFT WOULD NOT PRESSURIZE ON CLIMB. LOUD SQUEAL FROM RIGHT SIDE WINDOW WAS REPORTED AS WELL. MAINTENANCE INSPECTED AND RE
- [SDR C2XA11CL065](https://openairdocs.org/sdr/C2XA11CL065), Mar 7, 2011: SMOKE DETECTOR. INTERMITTENT. PIA FLT 6118 THE CREW REPORTED A LAV SMOKE INDICATION. MAINTENANCE INSPECTED AND REPLACED THE LAV SMOKE DETECTOR. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA11TY023](https://openairdocs.org/sdr/C2XA11TY023), Mar 7, 2011: INDICATION SYS. MALFUNCTIONED. LAV SMOKE INDICATION. PERFORMED TEST OF LAV SMOKE INDICATION IAW EMB 145 AMM 26-14-00. OPS CHECK GOOD.
- [SDR C2XA11TY021](https://openairdocs.org/sdr/C2XA11TY021), Mar 6, 2011: FUSE. BLOWN. TYS - A/C WAS IN FOR A SERVICE CHECK WHEN THE LEFT AND RIGHT EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOP. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERG
- [SDR C2XA11RI016](https://openairdocs.org/sdr/C2XA11RI016), Feb 2, 2011: SMOKE DETECTOR. FALSE ACTIVATION. FLIGHT 6188 - ORF - FLIGHT CREW REPORTED LAV SMOKE DETECTOR GOING OFF. IAD MX REMOVED AND REPLACED LAV SMOKE DETECTOR AND PERFORMED OPERATIONAL CHECK SUCCESSFUL
- [SDR C2XA11CL033](https://openairdocs.org/sdr/C2XA11CL033), Feb 2, 2011: SMOKE DETECTOR. FALSE ACTIVATION. ORD FLT 6188 THE CREW REPORTED A LAV SMOKE WARNING ON THE EICAS. MAINTENANCE INSPECTED AND REPLACED THE LAV SMOKE DETECTOR. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA11TY010](https://openairdocs.org/sdr/C2XA11TY010), Jan 22, 2011: SKIN. DENTED. TYS - SKIN DENTED BETWEEN FRAMES 19 AND 20, STRINGERS 11L AND 12L. CUT OUT DAMAGED SECTION, FABRICATED FILLER AND DOUBLER. INSTALLED FILLER AND DOUBLER, SEALED,
- [SDR C2XA11TY009](https://openairdocs.org/sdr/C2XA11TY009), Jan 21, 2011: FITTING. CRACKED. TYS - A/C IS IN C-CHECK STATUS WHEN INSPECTION FOUND THE RT LOWER ENGINE YOLK, FWD MOUNT CRACKED. MAINTENANCE REMOVED THE FITTING AND REPLACED THE ENGINE IAW 54

All 90: https://openairdocs.org/deregistered/N11544-2022-03-03/reports.md

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