# N21537: 2001 Embraer EMB-145LR, registration cancelled 2022-08-16 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 16, 2022 - Exported to: Colombia - 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: 145523 - Year built: 2001 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: November 9, 2001 - Certificate issued: October 6, 2021 - Last registry action: October 6, 2021 - Mode S code: A1CEF6 - Owner when cancelled: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N21537 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=21537 - Page: https://openairdocs.org/deregistered/N21537-2022-08-16 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 (63, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASOA201906045074](https://openairdocs.org/sdr/ASOA201906045074), May 30, 2019: BATTERY PACK. INOPERATIVE. DURING MX INSPECTION THE #3 EMERGENCY LIGHT BATTERY WAS FOUND DEAD. MX R/R #3 BATTERY WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA201905075068](https://openairdocs.org/sdr/ASOA201905075068), May 7, 2019: LIGHT. INOPERATIVE. DURING MX INSPECTION THE CEILING EXIT LIGHT AT ROW 23 WAS INOP. REMOVED AND REPLACED AISLE CEILING EXIT LIGHT AT ROW 23 IAW AMM 33-50-08, OPS CHECK GOOD. A/C WA - [SDR ASOA201901145013](https://openairdocs.org/sdr/ASOA201901145013), Jan 14, 2019: CONNECTOR. DISCONNECTED. DURING MX INSPECTION THE EMERGENCY LIGHTS WERE INOP AT COCKPIT, MAIN ENTRANCE, AND SIGN ABOVE FLIGHT ATTENDANT SEAT. MX FOUND IN MAIN DOOR CEILING PANEL THE ELE - [SDR ASOA201705264028](https://openairdocs.org/sdr/ASOA201705264028), May 26, 2017: SEAT TRACK. CORRODED. DURING C-CHECK INSPECTION, THE LEFT OUTBOARD SEAT TRACK NR 5 AND RIGHT NR 4 WERE FOUND TO BE CORRODED BEYOND LIMITS. THE AFFECTED SEAT TRACKS WERE REMOVED AND R - [SDR ASOA201705264026](https://openairdocs.org/sdr/ASOA201705264026), May 26, 2017: FLOOR SUPPORT. CORRODED. DURING C-CHECK INSPECTION, THE RT INBD FLOOR SUPPORT BETWEEN FRAMES 59-61 WAS FOUND TO BE CORRODED BEYOND LIMITS. THE DAMAGE WAS REMOVED AND A DOUBLER REPAIR WA - [SDR ASOA201705254032](https://openairdocs.org/sdr/ASOA201705254032), May 25, 2017: BEARING CAP. CORRODED. DURING C-CHECK INSPECTION, THE FORWARD AND AFT MLG LOWER BEARING CAPS WERE FOUND TO BE CORRODED BEYOND LIMITS. THE AFFECTED BEARING CAPS WERE REMOVED AND REPLAC - [SDR ASOA201705254031](https://openairdocs.org/sdr/ASOA201705254031), May 25, 2017: BEARING CAP. CORRODED. DURING C-CHECK INSPECTION, THE FORWARD AND AFT MLG LOWER BEARING CAPS WERE FOUND TO BE CORRODED BEYOND LIMITS. THE AFFECTED BEARING CAPS WERE REMOVED AND REPLAC - [SDR ASOA201705254027](https://openairdocs.org/sdr/ASOA201705254027), May 25, 2017: DOUBLER. CORRODED. DURING C-CHECK INSPECTION, THE INTERNAL DOUBLE FOR THE FORWARD RADIO ALTIMETER 2 WAS FOUND TO BE CORRODED. A DOUBLER REPAIR WAS ACCOMPLISHED ON THE AFFECTED ARE - [SDR ASOA201705243174](https://openairdocs.org/sdr/ASOA201705243174), May 24, 2017: CROSSBEAM. CRACKED. NOSE LANDING GEAR UPLOCK FORWARD CROSSBEAM CRACKED. REPLACED FORWARD CROSSBEAM AS PER SRM 51-40-02. - [SDR ASOA201705243173](https://openairdocs.org/sdr/ASOA201705243173), May 24, 2017: ANGLE. CRACKED. CENTER FUSELAGE NR 3 OMEGA BEAM ANGLE CRACKED. OMEGA BEAM ANGLE REPLACED. - [SDR ASOA201705243172](https://openairdocs.org/sdr/ASOA201705243172), May 24, 2017: ANGLE. CRACKED. CENTER FUSELAGE 3 OMEGA BEAM ANGLE CRACKED. OMEGA BEAM ANGLE REPLACED. - [SDR ASOA201705243171](https://openairdocs.org/sdr/ASOA201705243171), May 24, 2017: ANGLE. CRACKED. CENTER FUSELAGE 3 R/H OMEGA ANGLE CRACKED. OMEGA ANGLE REPLACED. - [SDR ASOA201705243170](https://openairdocs.org/sdr/ASOA201705243170), May 24, 2017: ANGLE. CRACKED. CENTER FUSELAGE 3 RT OMEGA ANGLE CRACKED. OMEGA ANGLE REPLACED. - [SDR ASOA201705233169](https://openairdocs.org/sdr/ASOA201705233169), May 23, 2017: ANGLE. CRACKED. CENTER FUSELAGE 3 FRAME 46 LT FLOOR LEVEL FUSELAGE TO REAR SPAR ANGLE CRACKED. ANGLE REPLACED AS PER SRM 51-40-02. - [SDR ASOA201705233168](https://openairdocs.org/sdr/ASOA201705233168), May 23, 2017: ANGLE. CRACKED. CENTER FUSELAGE 3 FRAME 46 RT FLOOR LEVEL FUSELAGE TO REAR ANGLE CRACKED. ANGLE REPLACED AS PER SRM 51-40-02. - [SDR ASOA201703275028](https://openairdocs.org/sdr/ASOA201703275028), Mar 27, 2017: CONTROL UNIT. FAULTY. PILOT REPORTED INBOARD BRAKES DID NOT WORK ON LANDING BOTH TEMP PROBES SHOWING COLD AND COLD TO THE TOUCH. MX REMOVED AND REPLACED BCU WITH OPERATIONAL CHECK GO - [SDR ASOA20160326027](https://openairdocs.org/sdr/ASOA20160326027), Mar 26, 2016: LIGHT. INOPERATIVE. DURING CREW INSPECTION AN EMERGENCY LIGHT WAS FOUND TO BE DIMLY LIT. MAINTENANCE R & R THE AFFECTED EMERGENCY LIGHT, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, - [SDR ASOA20151028055](https://openairdocs.org/sdr/ASOA20151028055), Oct 28, 2015: LIGHT. ARCED. CREW REPORTED AN ACRID BURNING ODOR OBSERVED AROUND ROW 10A. MAINTENANCE R & R PASSENGER CABIN LIGHT ASSY AT SEAT 10A WITH OPS CHECK GOOD. ACFT APPROVED FOR RET - [SDR ASOA20151008077](https://openairdocs.org/sdr/ASOA20151008077), Oct 8, 2015: CONNECTOR. LOOSE. DURING MAINTENANCE INSPECTION THE FORWARD EXIT ROW CEILING EMERGENCY EXIT SIGN, LABEL, WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE ACFT AND FOUND A L - [SDR ASOA20150225057](https://openairdocs.org/sdr/ASOA20150225057), Feb 25, 2015: SKIN. CRACKED. DURING C-CHECK FUSELAGE SKIN AT FRAME 75, STRINGER 1R-2R CRACKS AT RIVET HOLE. MAINTENANCE PERFORMED REPAIR ON FUSELAGE SKIN AT FRAME 75, STRINGER 1R-2R IAW EC5 - [SDR ASOA20150225056V](https://openairdocs.org/sdr/ASOA20150225056V), Feb 25, 2015: SKIN. CRACKED. DURING C-CHECK FUSELAGE SKIN AT FRAME 75 AT STRINGER 1L-2L CRACKED RIVET HOLE SKIN. MAINTENANCE COMPLETED REPAIR ON FUSELAGE SKIN AT FRAME 75 STRINGER 1L-2L IAW - [SDR ASOA20150218055](https://openairdocs.org/sdr/ASOA20150218055), Feb 18, 2015: SUPPORT. CORRODED. CARGO LOWER BEAM CORRODED BETWEEN FRAMES 65-68. R & R LOWER CUTOUT IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20130601043](https://openairdocs.org/sdr/ASOA20130601043), Jun 1, 2013: INVERTER. INOPERATIVE. DURING MX THE AFT CABIN EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MX REPLACED THE AFT EMERGENCY LIGHT INVERTER. OPS CHECKED GOOD. - [SDR ASOA20130531042](https://openairdocs.org/sdr/ASOA20130531042), May 31, 2013: SOCKET. BURNED. CREW REPORTED A BURNED ODOR AT ROW 16A, 17A, 18A. MX INSPECTED AND FOUND BURNED LIGHT SOCKETS. - [SDR ASOA20121227093C](https://openairdocs.org/sdr/ASOA20121227093C), Dec 27, 2012: LIGHT. INOPERATIVE. DURING ROUTINE MX, THE LAST AFT EMERGENCY AISLE PATH LIGHT STRIP WAS FOUND INOPERATIVE. MX REPLACED THE AISLE PATH LIGHT STRIP AND OPS CHECKED GOOD. - [SDR ASOA20120930079](https://openairdocs.org/sdr/ASOA20120930079), Sep 30, 2012: LIGHT. BURNED. THE CREW REPORTED SMOKE ODOR IN COCKPIT. MX INSPECTED AND FOUND CABIN SIDE WALL LIGHT ASSY BURNED. THE LIGHT ASSY WAS DISCONNECTED. MX INSPECTED AND REPLACED 6A - [SDR ASOA20120507035](https://openairdocs.org/sdr/ASOA20120507035), May 7, 2012: UNKNOWN. ODOR. CREW REPORTED A STRONG ELECTRICAL ODOR ON CLIMBOUT. FLIGHT CONTINUED. MX RAN ENGINES IAW AMM 71-00-01 AND PERFORMED OPS CHECKS OF THE APU, PACK SYS, AND PNEUMAT - [SDR ASOA20120420041](https://openairdocs.org/sdr/ASOA20120420041), Apr 20, 2012: WIRE HARNESS. ODOR. CREW REPORTED A CHEMICAL OR ELECTRICAL ODOR IN FRONT OF CABIN NEAR ROW 3 AND 4. MX INSPECTED AND REPLACED THE CABIN CEILING LIGHT ELECTRICAL HARNESS. OPS CHECKE - [SDR C2XA11TY124](https://openairdocs.org/sdr/C2XA11TY124), Jul 20, 2011: BATTERY. OVERTEMP. TYS - A/C DIVERTED INTO BNA (LOGPAGE 2825614) WITH A OVERTEMP NR 2 BATTERY. MAINTENANCE REMOVED AND REPLACED THE NR 2 BATTERY IAE EMB 145 AMM 24-36-001, OPS CHE - [SDR C2XA10CL123](https://openairdocs.org/sdr/C2XA10CL123), Aug 3, 2010: STARTER GEN. FAILED. CLE FLT 2785 THE CREW REPORTED A BURNING SMELL IN THE COCKPIT FOLLOWED BY APU FAIL. MAINTENANCE INSPECTED AND REPLACED THE APU STARTER/GENERATOR. OPERATIONAL CH - [SDR C2XA10IA202](https://openairdocs.org/sdr/C2XA10IA202), Jul 17, 2010: O-RING. BLOWN. IAH - FLIGHT 2226, THE CREW REPORTED A BLEED ONE LEAK. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE O-RIN - [SDR C2XA10IA189](https://openairdocs.org/sdr/C2XA10IA189), Jul 3, 2010: THERMOSTAT. FAULTY. TUL - DURING CLIMB, AT FL250 IN ICING CONDITIONS THE CREW REPORTED A BLEED NR 2 OVERTEMP WARNING WITH INDICATIONS IN THE UPPER RED RANGE. THE CREW DIVERTED TO T - [SDR C2XA10IA186](https://openairdocs.org/sdr/C2XA10IA186), Jul 3, 2010: CLAMP. LOOSE. TUL - FLIGHT 2752, ON DESCENT INTO TUL THE CREW RECEIVED A PACK 1 FAIL AND PACK 2 INOP MESSAGE. THE CREW PERFORMED AN EMERGENCY DESCENT AND THE AIRCRAFT LANDED - [SDR C2XA10CL054](https://openairdocs.org/sdr/C2XA10CL054), Apr 4, 2010: PROBE. INOPERATIVE. CLE FLIGHT 2659 THE CREW REPORTED A NR 1 TAT HEAT INOP MESSAGE IN FLIGHT. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND RE - [SDR C2XA10CL027](https://openairdocs.org/sdr/C2XA10CL027), Feb 14, 2010: LEAD. LOOSE. DURING ROUTINE MAINTENANCE THE AFT OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND RE-SECURED THE POSITIVE POWER LEAD ON THE LIGH - [SDR C2XA09CL120](https://openairdocs.org/sdr/C2XA09CL120), Sep 21, 2009: BATTERY. DISCHARGED. CLE - FLT 2999 - THE CREW REPORTED THE CAPTAINS FLASHLIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE BATTERY. OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA09TY081](https://openairdocs.org/sdr/C2XA09TY081), Apr 28, 2009: SKIN. CHAFED. CHAFE ON AIRCRAFT SKIN INSIDE PANEL 414DB FROM LANYARD. FABRICATED AND INSTALLED DOUBLER IAW IC2009-145/03078A. - [SDR C2XA09TY076](https://openairdocs.org/sdr/C2XA09TY076), Apr 28, 2009: SKIN. DENTED. DENT LOCATED BETWEEN FR8 AND FR9 BETWEEN STR 20R AND 21R. REPAIRED DENTED AREA ON FUSELAGE SKIN IAW EMB 135/145 SRM 53-10-01. AIRCRAFT STILL IN C CHECK. - [SDR C2XA09TY067](https://openairdocs.org/sdr/C2XA09TY067), Apr 22, 2009: FRAME. CORRODED. TYS - DURING C-CHECK CORROSION WAS FOUND AROUND THE SERVICE DOOR LOWER FRAME NUT PLATES. THE AREA WAS CUT OUT AND REPAIRED IAW EC 5310-01373. A/C STILL IN C-CHE - [SDR C2XA09TY065](https://openairdocs.org/sdr/C2XA09TY065), Apr 21, 2009: YOKE. CRACKED. TYS - DURING C-CHECK THE NR 1 ENGINE FWD LOWER YOKE WAS FOUND CRACKED AT THE FWD ATTACH POINT. A DYE PEN TEST WAS PERFORMED IAW EMB NDT PTO 1 AND PTO 2 AND THE - [SDR C2XA08CL038](https://openairdocs.org/sdr/C2XA08CL038), Mar 24, 2008: LIGHT. INOPERATIVE. DURING ROUTINE MAINTENANCE THE MAIN CABIN DOOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE LAMP. OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA08IA020](https://openairdocs.org/sdr/C2XA08IA020), Jan 9, 2008: WHEEL. WORN. IAH - FLIGHT 2431, THE CREW REPORTED AN EXCESSIVE NW VIBRATION ON T/O. MAINTENANCE REMOVED AND REPLACED BOTH NOSE WHEEL ASSEMBLIES, AND THE AIRCRAFT WAS APPROVE - [SDR C2XA08IA019](https://openairdocs.org/sdr/C2XA08IA019), Jan 9, 2008: WHEEL. WORN. IAH - FLIGHT 2431, THE CREW REPORTED AN EXCESSIVE NW VIBRATION ON T/O. MAINTENANCE REMOVED AND REPLACED BOTH NOSE WHEEL ASSEMBLIES, AND THE AIRCRAFT WAS APPROVE - [SDR C2XA07SH043](https://openairdocs.org/sdr/C2XA07SH043), Aug 4, 2007: CASE. CORRODED. SHV - DURING C-CHECK MAINTENANCE FOUND NR 1 ENGINE FAN CASE ASSY & ENGINE INLET MOUNTING ATTACHMENT BOLTS HOLES WITH CORROSION. MAINTENANCE REPAIRED NR 1 ENGINE - [SDR C2XA06CL086](https://openairdocs.org/sdr/C2XA06CL086), Oct 16, 2006: INVERTER. INOPERATIVE. DURING ROUTINE MAINTENANCE THE EMERGENCY EXIT LIGHTS BELOW EMERGENCY EXIT DOOR WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 5 EMERGENCY LIGHT INVE - [SDR C2XA06IA159](https://openairdocs.org/sdr/C2XA06IA159), Sep 28, 2006: CONTROL UNIT. MALFUNCTIONED. IAH-2394, ON TAXI OUT OF BNA, THE CREW REPORTED A PACK TWO OVERHEAT ON TAXI OUT. THE SYSTEM WAS RESET SUCCESSFULLY, AND ON TAKEOFF HAD A STRONG ELECTRICAL ODOR - [SDR C2XA06CL043](https://openairdocs.org/sdr/C2XA06CL043), Apr 15, 2006: PROXIMITY SWITCH. FAULTY. CLE FLIGHT 3233, THE CREW REPORTED A VIBRATION FROM THE NOSE AREA AFTER TAKEOFF. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED - [SDR C2XA06IA030](https://openairdocs.org/sdr/C2XA06IA030), Mar 6, 2006: CONNECTOR. LOOSE. IAH - ON TAKEOFF FROM SDF THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT WITHOUT PRESSING THE DOWNLOCK RELEASE BUTTON. THE AIRCRAFT CONTINUED TO IAH - [SDR C2XA06BT011](https://openairdocs.org/sdr/C2XA06BT011), Mar 2, 2006: CONTROL LEVER. FAULTY. CREW REPORTED AFTER TAKEOFF IN YYZ, -DOWNLOCK RELEASE- BUTTON HAD TO BE PUSHED TO GET THE GEAR HANDLE TO COME UP, NO EICAS MESSAGE NOTED. FLIGHT CONTINUE TO NEW - [SDR C2XA06IA028](https://openairdocs.org/sdr/C2XA06IA028), Feb 27, 2006: BATTERY PACK. DISCHARGED. IAH - DURING MAINTENANCE INSPECTION THE RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EM All 63: https://openairdocs.org/deregistered/N21537-2022-08-16/reports.md ## Other aircraft with N21537 - [Cancelled 1984-07-13](https://openairdocs.org/deregistered/N21537-1984-07-13): Piper PA-28-181, S/N 28-7990053. Administratively canceled. Owner: [American Aviation Inc](https://openairdocs.org/faa-owner/AMERICAN%20AVIATION%20INC), [Brooksville, FL](https://openairdocs.org/faa-place/FL/Brooksville) - [Cancelled 1965-07-12](https://openairdocs.org/deregistered/N21537-1965-07-12): Piper J3C-65, S/N 2388, built 1938. Owner: [Suffolk County Afb Aero Club](https://openairdocs.org/faa-owner/SUFFOLK%20COUNTY%20AFB%20AERO%20CLUB), [West Hampton Beach, NY](https://openairdocs.org/faa-place/NY/West%20Hampton%20Beach) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.