# N12567: 2002 Embraer EMB-145LR, registration cancelled 2020-10-20 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 20, 2020 - Exported to: Nigeria - Status when cancelled: Sale reported - 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: 145623 - Year built: 2002 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: August 2, 2002 - Last registry action: October 16, 2020 - Mode S code: A0698F - Location: [Xxx, OK](https://openairdocs.org/faa-place/OK/Xxx) - Owner type: Individual - The mark today: https://openairdocs.org/aircraft/N12567 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=12567 - Page: https://openairdocs.org/deregistered/N12567-2020-10-20 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 (60, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASOA201901214003](https://openairdocs.org/sdr/ASOA201901214003), Jan 21, 2019: SKIN. DAMAGED. IAH - DURING MAINTENANCE INSPECTION A PREVIOUS REPAIR ON THE CARGO DOOR LOWER FORWARD CORNER WAS FOUND TO HAVE A CREASE ON THE SKIN. MAINTENANCE REMOVED THE DOU - [SDR ASOA201804167062](https://openairdocs.org/sdr/ASOA201804167062), Apr 16, 2018: WIRE. BROKEN. INSPECTION FOUND A BROKEN WIRE ON THE EMERGENCY LIGHT STRIP. MAINTENANCE REPLACED THE LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD. - [SDR ASOA201804167061](https://openairdocs.org/sdr/ASOA201804167061), Apr 16, 2018: SKIN. DAMAGED. FOUND THE RT HORIZONTAL STAB LEADING EDGE DAMAGE AT THE LOWER SIDE SCREW HOLES. MAINTENANCE REPAIRED THE LOWER HORIZONTAL STAB LEADING EDGE IAW ETD 2018-145-037 - [SDR ASOA201804137060](https://openairdocs.org/sdr/ASOA201804137060), Apr 11, 2018: SKIN. DAMAGED. RIGHT HORIZONTAL STAB LEADING EDGE HAS DAMAGE AT THE SCREW HOLES ON LOWER SIDE. CONTOURED THE AREA BY COLD FORMING. INSTALLED DIMPLED WASHER IAW ETD2018-145-037 - [SDR ASOA201804057052](https://openairdocs.org/sdr/ASOA201804057052), Apr 4, 2018: DOOR FRAME. CORRODED. DOOR FRAME HAS CORROSION ON AFT LOWEST DOOR STOP ON SERVICE DOOR. REMOVED DAMAGED SECTION OF THE DOOR FRAME 22. DRILLED AND FABRICATED A DOUBLER SECTION OF THE - [SDR ASOA201804057051](https://openairdocs.org/sdr/ASOA201804057051), Apr 4, 2018: SKIN. CRACKED. CRACKED SKIN AT FRAME 75. CUT OUT A 2 X 2 INCH SECTION OF THE SKIN AND INSTALLED FILLER AND DOUBLER. - [SDR ASOA201803247036](https://openairdocs.org/sdr/ASOA201803247036), Mar 24, 2018: YOKE. CRACKED. #1 ENGINE PYLON LOWER FORWARD YOKE CRACKED. REMOVED AND REPLACED FORWARD YOKE. AIRCRAFT STILL IN C CHECK. - [SDR ASOA201706055083](https://openairdocs.org/sdr/ASOA201706055083), Jun 5, 2017: CONTROL UNIT. FAULTY. PILOT REPORTED RIGHT BRAKE PEDAL WHEN COMMANDED RESULTS IN ALMOST NO BRAKING ACTION. ADDITIONALLY THE RIGHT IB BRAKE TEMP ALWAYS STAYED AT ZERO DESPITE THE RIGH - [SDR ASOA201612225092](https://openairdocs.org/sdr/ASOA201612225092), Dec 22, 2016: LIGHT. INOPERATIVE. CREW REPORTED MOST AFT CABIN EMERGENCY LIGHTS ARE INOPERATIVE. MX REMOVED AND REPLACED THE LIGHT AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20160611028](https://openairdocs.org/sdr/ASOA20160611028), Jun 11, 2016: CONTROL MODULE. ODOR. HEAVY ELECTRICAL SMOKE ODOR REPORTED FROM MAIN CABIN DOOR AREA SPREAD TO THE GALLEY. R & R CABIN LIGHT CONTROL MODULE WITH OPS CHECK GOOD. ACFT APPROVED FOR RET - [SDR ASOA20150626033](https://openairdocs.org/sdr/ASOA20150626033), Jun 26, 2015: CHARGER. INOPERATIVE. DURING MAINTENANCE INSPECTION, THE LT FWD FUSELAGE EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE R & R NR 4 EMERGENCY LIGHT BATTERY CHARGER AND REPAIRED WI - [SDR ASOA20150520029](https://openairdocs.org/sdr/ASOA20150520029), May 20, 2015: CHARGER. FAULTY. DURING ROUTINE MAINTENANCE THE LT FWD EXTERNAL EMERGENCY LIGHT AND AISLE CEILING LIGHT WOULD NOT TEST. MAINTENANCE REPLACED THE NR 1 EMERGENCY LIGHT BATTERY CHA - [SDR ASOA20150304023](https://openairdocs.org/sdr/ASOA20150304023), Mar 4, 2015: CHARGER. INOPERATIVE. DURING A-CK INSPECTION, THE LT WING FWD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 1 BATTERY CHARGER, OPERATIONALLY TESTED WITH NO DE - [SDR ASOA20130806350T](https://openairdocs.org/sdr/ASOA20130806350T), Aug 6, 2013: BEARING. WORN. ACFT LT AND RT HORIZONTAL STABILIZER SPHERICAL BEARINGS HAD PLAY IN THE HOUSING. MX REAMED BOTH HOUSINGS AND REPAIRED AND INSTALLED SPHERICAL BEARINGS IAW SRM 5 - [SDR ASOA20130702069](https://openairdocs.org/sdr/ASOA20130702069), Jul 2, 2013: TRANSDUCER. FAULTY. PILOT REPORTED DURING BRAKE APPLICATION (RT ONLY) CLUNKING NOISE COMES FROM FWD OF COCKPIT UNTIL HARD BRAKE APPLICATION. BRAKING ACTION REDUCED UNTIL HARD APPLI - [SDR ASOA20130412035](https://openairdocs.org/sdr/ASOA20130412035), Apr 12, 2013: LIGHT. INOPERATIVE. DURING MX INSPECTION THE EMERGENCY LIGHT PROXIMITY STRIP BETWEEN ROW 4 AND 7 WAS FOUND INOPERATIVE. MX RESET SYS AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS - [SDR ASOA20121010081](https://openairdocs.org/sdr/ASOA20121010081), Oct 10, 2012: DUCT. DISCONNECTED. THE CREW REPORTED ODOR OF SMOKE AT SEATS 6-7. MX INSPECTED AND FOUND DUCT AT NR 2 RECIRCULATION FAN OFF UNDER FLOOR. MX REINSTALLED DUCT AT NR 2 RECIRCULATION F - [SDR ASOA20120812109](https://openairdocs.org/sdr/ASOA20120812109), Aug 12, 2012: BATTERY PACK. DISCHARGED. DURING PREFLIGHT INSP THE CREW REPORTED TAHT THE FIRST 3 AISLE PATH EMERGENCY LIGHTS WOULD ONLY STAY ILLUMINATED FOR 15 SECONDS AND THEN GO IFF, AND THAT THE EM - [SDR ASOA20120812108](https://openairdocs.org/sdr/ASOA20120812108), Aug 12, 2012: BATTERY PACK. DISCHARGED. DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE FIRST 3 AISLE PATH EMERGENCY LIGHTS WOULD ONLY STAY ILLUMINATED FOR 15 SECONDS AND THEN GO OFF, AND THAT - [SDR ASOA20120525108](https://openairdocs.org/sdr/ASOA20120525108), May 24, 2012: SILL. CORRODED. CORROSION ON REPAIR DOUBLER RT SILL FRAME 20. BLENDED CORROSION, WITHIN LIMITS. TREATED, PRIMED, PAINTED. - [SDR ASOA20120519106T](https://openairdocs.org/sdr/ASOA20120519106T), May 19, 2012: SHEAR TIE. CRACKED. SHEAR CLIP FOUND CRACKED AT FRAME 61 BETWEEN STR 6L AND 7L. MX R & R THE SHEAR CLIP IAW SRM 51-20-03 AND 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT - [SDR ASOA20120519105](https://openairdocs.org/sdr/ASOA20120519105), May 19, 2012: SHEAR TIE. CRACKED. SHEAR CLIP CRACKED AT FRAME 80 AT THE APU FIRE BOTTLE. MX R & R THE SHEAR CLIP IAW SRM 51-20-03 AND 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE - [SDR ASOA20120519104](https://openairdocs.org/sdr/ASOA20120519104), May 19, 2012: CROSSBEAM. CORRODED. CORROSION WAS FOUND IN THE ISLE AT FRAME 20 CROSS-MEMBER THAT WAS BLENDED OUT OF LIMITS. MX R & R THE CROSS-MEMBER IAW SRM 51-20-03 AND 51-40-02. ALL WORK ACCOM - [SDR ASOA20120519103](https://openairdocs.org/sdr/ASOA20120519103), May 19, 2012: FLOOR SUPPORT. CRACKED. THE RT OTBD OMEGA BEAM SUPPORT WAS FOUND CRACKED AT FRAME 47 TO 48. MX R & R THE SUPPORT IAW SRM 51-20-03 AND 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEAS - [SDR ASOA20120519102](https://openairdocs.org/sdr/ASOA20120519102), May 19, 2012: SKIN. CANNING. DENT ON THE CARGO DOOR. MX RECONTOURED DENT, SKIN HAD A OIL CAN, SO THEY CUT OUT DAMAGE, FABRICATED A FILLER AND DOUBLER, THEN INSTALL FILLER AND DOUBLER IAW SR - [SDR ASOA20120519101](https://openairdocs.org/sdr/ASOA20120519101), May 19, 2012: SEAT TRACK. CORRODED. THE LEFT OTBD SEAT TRACK WAS FOUND CORRODED BEYOND LIMITS AT FRAME 50. MX R & R THE SUPPORT AT FRAME 50 IAW SRM 51-20-03 AND 51-40-02. ALL WORK ACCOMPLISHED AND - [SDR ASOA20120525110](https://openairdocs.org/sdr/ASOA20120525110), May 12, 2012: FLOOR SUPPORT. CORRODED. CORROSION IN GUSSET CENTER OMEGA BEAM FRAME 20. BLENDED CORROSION, WITHIN LIMITS. TREATED, PRIMED AND PAINTED. - [SDR ASOA20120525109](https://openairdocs.org/sdr/ASOA20120525109), May 12, 2012: BRACKET. CORRODED. CORROSION ON BRACKET AT PAX DOOR ENTRANCE BELOW FLOOR. BLENDED CORROSION, WITHIN LIMITS. TREATED, PRIMED AND PAINTED. - [SDR C2XA11CL064](https://openairdocs.org/sdr/C2XA11CL064), Mar 3, 2011: SMOKE WARNING. FALSE ACTIVATION. ICT FLT 6056 THE CREW REPORTED A LAV SMOKE EICAS MESSAGE IN FLIGHT. MAINTENANCE INSPECTED AND PERFORMED LAV SMOKE SYSTEM OPERATIONAL CHECKS. NO DEFECTS WERE FOU - [SDR C2XA10SH248](https://openairdocs.org/sdr/C2XA10SH248), Jul 21, 2010: SKIN. CRACKED. SHV - DURING C-CHECK THE LT AFT SKIN WAS FOUND TO BE CRACKED AROUND FASTENERS BETWEEN FRAMES 77-79 AND STRINGERS 2-10L. MAINTENANCE REMOVED THE CRACKS AND PERFO - [SDR C2XA10SH247](https://openairdocs.org/sdr/C2XA10SH247), Jul 21, 2010: SKIN. CRACKED. SHV - DURING C-CHECK THE RT AFT SKIN WAS FOUND TO BE CRACKED AROUND FASTENERS BETWEEN FRAMES 78-79 AND STRINGERS 2-10R. MAINTENANCE REMOVED THE CRACKS AND PERFO - [SDR C2XA10SH246](https://openairdocs.org/sdr/C2XA10SH246), Jul 21, 2010: FRAME. CRACKED. SHV - DURING C-CHECK FRAME 10 AT STRINGER 10L (RIGHT BELOW THE LT DV WINDOW) WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE CRACKED FRAME SEGMENT - [SDR C2XA10SH245](https://openairdocs.org/sdr/C2XA10SH245), Jul 21, 2010: FRAME. CRACKED. SHV - DURING C-CHECK FRAME 10 AT STRINGER 10R (RIGHT BELOW THE RT DV WINDOW) WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE CRACKED FRAME SEGMENT - [SDR C2XA10TY022](https://openairdocs.org/sdr/C2XA10TY022), Feb 5, 2010: FUSE. BLOWN. TYS - A/C IN FOR A 3A CHECK WHEN INSPECTION FOUND THE LT FWD OVERWING EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE FUSE IN BATTERY TRAY 1. OPS CHE - [SDR C2XA10IA003](https://openairdocs.org/sdr/C2XA10IA003), Jan 3, 2010: LIGHT. INOPERATIVE. IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED THE LEFT FORWARD EMERGENCY EXIT LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT - [SDR C2XA09IA332](https://openairdocs.org/sdr/C2XA09IA332), Dec 30, 2009: LINE. CONTAMINATED. IAH - FLIGHT 2263, THE CREW REPORTED AN ALTITUDE AND IAS ERROR WITH A BURNING SMELL. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE DRAINED THE W - [SDR C2XA09IA069](https://openairdocs.org/sdr/C2XA09IA069), Feb 28, 2009: CHARGER. INOPERATIVE. LCH - DURING MAINTENANCE INSPECTION THE COCKPIT CEILING AND NR 1 AISLE PATH, CEILING, AND WING TO FUSELAGE FRONT FAIRING LEFT EMERGENCY LIGHTS WERE FOUND TO BE - [SDR C2XA09TY035](https://openairdocs.org/sdr/C2XA09TY035), Feb 24, 2009: SKIN. DENTED. AIRCRAFT HAD TWO DENTS BETWEEN FRM 20/21 AND STR14L/16L. REPAIRED DENTED AREA BY FABRICATING L-ANGLE IAW IC2009-145/01434A. RE-CONTOURED SKIN, PERFORMED NDT, IN - [SDR C2XA09TY024](https://openairdocs.org/sdr/C2XA09TY024), Jan 27, 2009: BATTERY PACK. FAILED. ACFT WAS FOUND WITH THE AFT CEILING EMERGENCY LIGHT INOP. MX R&R THE NR 4 EMERGENCY LIGHT POWER SUPPLY IAW AMM 145 33-50-04. OPS CHECK GOOD AND WAS RELEASED TO - [SDR C2XA08RI065](https://openairdocs.org/sdr/C2XA08RI065), May 9, 2008: LIGHT. INOPERATIVE. FLIGHT 2648 - EWR - FLIGHT CREW REPORTED BAG SMOKE DETECT WOULD NOT ILLUMINATED ON TEST. EWR MX RESET THE SYSTEM AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. A - [SDR C2XA08RI017](https://openairdocs.org/sdr/C2XA08RI017), Feb 11, 2008: PROXIMITY SWITCH. INTERMITTENT. FLIGHT 2761 - EWR - CREW REPORTED THAT AFTER ROTATION, LDG/AIR GRD FAIL MESSAGE AND REV DISAGREE MESSAGE APPEARED ON EICAS. MESSAGES CLEARED UPON GEAR EXTENSION - [SDR C2XA07RI100](https://openairdocs.org/sdr/C2XA07RI100), Nov 25, 2007: CONTROL LEVER. DEFECTIVE. FLT 2490 - EWR - CREW REPORTED THAT LANDING GEAR WILL NOT RETRACT AFTER TAKEOFF. CREW PROCEEDED WITH AIR RETURN AND LANDED UNEVENTFULLY. EWR MX REMOVED AND REPL - [SDR C2XA07IA075](https://openairdocs.org/sdr/C2XA07IA075), Mar 24, 2007: INVERTER. INOPERATIVE. MCI - DURING MAINTENANCE INSPECTION AISLE PATH LIGHTS 6, 7 & 8 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER SIX EMERGENCY LIGHT INV - [SDR C2XA06BT056](https://openairdocs.org/sdr/C2XA06BT056), Dec 10, 2006: SOCKET. LOOSE. BTV 2A CHECK FOUND RIGHT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED LAMP BASE IAW EMB145 AMM 33-50-10. OPS CHECK GOOD. - [SDR C2XA06IA110](https://openairdocs.org/sdr/C2XA06IA110), Jul 15, 2006: BATTERY. DISCHARGED. IAH - FLIGHT 3225, DURING PREFLIGHT INSPECTION, THE CREW REPORTED EMERGENCY AISLE PATH LIGHT WAS INOPERATIVE. MAINTENANCE RECHARGED THE AISLE PATH LIGHTING, OPE - [SDR C2XA06IA101](https://openairdocs.org/sdr/C2XA06IA101), Jun 18, 2006: INVERTER. INOPERATIVE. STL - DURING MAINTENANCE INSPECTION, THE FORWARD EMERGENCY FLOOR LIGHT STRIPS 2 & 3 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TW - [SDR C2XA06SH047](https://openairdocs.org/sdr/C2XA06SH047), Apr 19, 2006: DOOR FRAME. CORRODED. SHV - DURING C-CHECK THE AFT LOWER SERVICE DOOR CUTOUT FRAME WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW E - [SDR C2XA06SH046](https://openairdocs.org/sdr/C2XA06SH046), Apr 19, 2006: SKIN. GOUGED. SHV - DURING C-CHECK THE FUSELAGE SKIN AT FRAME 7 WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A PATCH REPAIR IAW EMB 145 SRM 53-1 - [SDR C2XA04CL119](https://openairdocs.org/sdr/C2XA04CL119), Nov 20, 2004: CONTACTOR. FAILED. CREW REPORTED A BURNING ODOR AND CRACKING SOUND BEHIND THE CAPTAINS SEAT AFTER THE APU FAILED. REPLACED THE APU LINE CONTACTOR. AIRCRAFT RETURNED TO SERVICE. - [SDR C2XA04TY085](https://openairdocs.org/sdr/C2XA04TY085), May 23, 2004: SILL. CORRODED. DURING A SCHEDULED 1C INSPECTION THE SERVICE DOOR SILL WAS FOUND CORRODED. MAINT. REMOVED THE REPLACED THE SERVICE DOOR SILL IAW EMB 135/145 SRM 51-40-02 AND IC All 60: https://openairdocs.org/deregistered/N12567-2020-10-20/reports.md ## 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 20050426007729I](https://openairdocs.org/incident/20050426007729I), Apr 26, 2005: Emb EMB145LR (N12567), Omaha, NE. (-23) N12567, operated by express jet as Continental express flight 2594, aborted takeoff after a report by another aircraft of possible smoke in the area of… ## Other aircraft with N12567 - [Cancelled 1994-11-29](https://openairdocs.org/deregistered/N12567-1994-11-29): Cessna 172M, S/N 17262078. Exported to Spain. Owner: [Knight Flight Limited Inc](https://openairdocs.org/faa-owner/KNIGHT%20FLIGHT%20LIMITED%20INC), [Sanford, FL](https://openairdocs.org/faa-place/FL/Sanford) --- 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.