# N12967: 1999 Embraer EMB-145LR, registration cancelled 2017-01-05 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: January 5, 2017 - Status when cancelled: Valid registration - Airframe: [Embraer EMB-145LR](https://openairdocs.org/model/embraer-emb-145lr) (registry code 3260212) - Engine: [Allison AE3007C series](https://openairdocs.org/engine/allison-ae3007c-series) (registry code 03028) - Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (OpenAirDocs) - Serial number: 145133 - Year built: 1999 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: May 8, 1999 - Certificate issued: June 18, 1999 - Last registry action: February 3, 2015 - Mode S code: A0786B - Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%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/N12967 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=12967 - Page: https://openairdocs.org/deregistered/N12967-2017-01-05 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 (101, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASOA20141204144](https://openairdocs.org/sdr/ASOA20141204144), Dec 4, 2014: DISPLAY. MALFUNCTIONED. THE CREW REPORTED THAT AFTER PFD2 WENT BLANK THERE WAS SMOKE IN THE COCKPIT. MAINTENANCE R & R THE NR 2 PFD, OPERATIONALLY TESTED WITH NO DEFECTS AND THE ACFT W - [SDR ASOA20140410033C](https://openairdocs.org/sdr/ASOA20140410033C), Apr 10, 2014: WIRE HARNESS. BURNED. THE CREW REPORTED BURNING ODOR IN THE CABIN AND GALLEY AREA. MAINTENANCE INSPECTED AND FOUND THE OVERHEAD LIGHT AT 5A TO BE BURNED. MAINTENANCE R & R THE CABIN - [SDR ASOA20140304027](https://openairdocs.org/sdr/ASOA20140304027), Mar 4, 2014: LIGHT. MALFUNCTIONED. PILOT REPORTED NOT ALL THE EMERGENCY LIGHTS WORKING. MAINTENANCE RESET EMERGENCY LIGHT SYSTEM AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20131208278](https://openairdocs.org/sdr/ASOA20131208278), Dec 8, 2013: SILL. CORRODED. SERVICE DOOR SILL CORRODED. R & R SERVICE DOOR SILL IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20131208277](https://openairdocs.org/sdr/ASOA20131208277), Dec 8, 2013: SKIN. CRACKED. SKIN CRACKS AROUND RIVETS, FR 77, STR 8R. REPAIRED SKIN CRACKS IAW SRM 53-32-02. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20131208276](https://openairdocs.org/sdr/ASOA20131208276), Dec 8, 2013: DOOR FRAME. CORRODED. CARGO DOOR LOWER CUT OUT CORRODED BETWEEN FR 65-68. RT CARGO DOOR LOWER CUT OUT IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20131208275](https://openairdocs.org/sdr/ASOA20131208275), Dec 8, 2013: STRINGER. CRACKED. STRINGER 6R CRACKED AT FR 13. R & R STRINGER IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20130409052](https://openairdocs.org/sdr/ASOA20130409052), Apr 9, 2013: INVERTER. INOPERATIVE. DURING A SCHEDULED INSP, THE AFT OVERWING EMERGENCY EXIT LOCATER LIGHT WAS FOUND TO BE INOPERATIVE. THE NR 4 EMERGENCY LIGHT INVERTER WAS REPLACED, OPS CHECKS P - [SDR ASOA20121108103](https://openairdocs.org/sdr/ASOA20121108103), Nov 8, 2012: WIRE. UNSECURE. DURING MX INSPECTION, ROW 12 AISLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX RESECURED LOOSE WIRE ON ROW 12 EMERGENCY LIGHT ASSY WITH OPS CHECK SUCCESSFUL. ACFT - [SDR ASOA20120809110](https://openairdocs.org/sdr/ASOA20120809110), Aug 9, 2012: BATTERY PACK. DISCHARGED. DURING MX INSPECTION, VARIOUS OVERWING EMERGENCY EXIT LIGHTS/SIGNS WERE FOUND TO BE INOPERATIVE. MX R & R THE NR 3 EMERGENCY LIGHT BATTERY PACK, OPS TESTED WITH - [SDR ASOA20120722062C](https://openairdocs.org/sdr/ASOA20120722062C), Jul 22, 2012: DUCT. CONTAMINATED. THE CREW REPORTED A SMOKE ODOR IN COCKPIT. THE ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MX DETERMINED ODOR TO BE COMING FROM 1 ENGINE 14TH STAGE - [SDR ASOA20120627058C](https://openairdocs.org/sdr/ASOA20120627058C), Jun 27, 2012: INVERTER. INOPERATIVE. DURING ROUTINE MX, THE RT OVERWING EMERGENCY LIGHT MARKER IN CABIN WAS FOUND TO BE INOPERATIVE. MX REPLACED THE NR 5 EMERGENCY LIGHT INVERTER. OPS CHECKED GOOD. - [SDR ASOA20120326047](https://openairdocs.org/sdr/ASOA20120326047), Mar 26, 2012: INVERTER. INOPERATIVE. THE CREW REPORTED THAT THE NR 3 AISLE PATH LIGHT STRIP WAS INOP, COMES ON INTERMITTENTLY AFTER ABOUT 10 MINUTES. MX R & R THE EMERGENCY LIGHT INVERTER IN THE GA - [SDR ASOA20120325046](https://openairdocs.org/sdr/ASOA20120325046), Mar 25, 2012: BATTERY PACK. DISCHARGED. THE CREW REPORTED THE NR 2 AND 3 AISLE PATH LIGHT STRIPS TO BE INOPERATIVE. MX R & R THE NR 2 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS - [SDR ASOA20120325045](https://openairdocs.org/sdr/ASOA20120325045), Mar 25, 2012: LIGHT. INOPERATIVE. FLIGHT 5900 THE CREW REPORTED THAT THE NUMBER 5 AISLE PATH LIGHT WAS INOPERATIVE. MX R & R THE NR 5 LIGHT, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED - [SDR ASOA20120325044](https://openairdocs.org/sdr/ASOA20120325044), Mar 25, 2012: LIGHT. INOPERATIVE. THE CREW REPORTED THE NR 2 AISLE PATH LIGHT STRIP TO BE INOPERATIVE. MX PLACED THE AFFECTED LIGHT STRIP ON MEL 33-50-00-2 CAT C, AND THE ACFT WAS APPROVED FOR R - [SDR ASOA20120316025](https://openairdocs.org/sdr/ASOA20120316025), Mar 16, 2012: WIRE HARNESS. FAULTY. SMOKE WAS REPORTED COMING OUT OF THE CEILING LIGHT ABOVE SEAT 1A. MX INSPECTED AND ISOLATED THE LIGHT HARNESS FOR THE LIGHT ABOVE SEAT 1A TO BE FAULTY. MX REMOV - [SDR ASOA20120109008](https://openairdocs.org/sdr/ASOA20120109008), Jan 9, 2012: SKIN. CRACKED. DURING C-CK. SKIN CRACKS AT FR 75, STR 1R-3R. REPAIRED SKIN IAW EC5330-02353. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20120109007](https://openairdocs.org/sdr/ASOA20120109007), Jan 9, 2012: SKIN. CRACKED. DURING C-CHECK. SKIN CRACKED AROUND RIVETS AT FR 75, STR 2L-3L. REPAIRED SKIN IAW EC5330-02353. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA11CL160](https://openairdocs.org/sdr/C2XA11CL160), Jul 5, 2011: O-RING. BLOWN. MKE FLT2000 THE CREW REPORTED A HYDRAULIC SYSTEM NR 2 FAIL MESSAGE IN FLIGHT. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED - [SDR C2XA11RI056](https://openairdocs.org/sdr/C2XA11RI056), Apr 16, 2011: BATTERY. OVERTEMP. FLIGHT 6129 - IAD - DURING APPROACH MAIN BATTERY NR 2 OVERTEMP. CREW LANDED WITH BATTERY TEMP AT 61 C, IT REACHED 81 C BY THE TIME TO DEPOWER ACFT. CREW EVACUAT - [SDR C2XA11CL048](https://openairdocs.org/sdr/C2XA11CL048), Feb 13, 2011: HOSE. WORN. FLT 6002 - THE CREW REPORTED A SMOKE SMELL WHEN THE NR 1 PACK WAS SELECTED. MAINTENANCE PLACED THE NR 1 PACK ON MEL. MAINTENANCE REPLACED THE HOSES AT THE DUAL - [SDR C2XA10IA299](https://openairdocs.org/sdr/C2XA10IA299), Nov 17, 2010: LIGHT. OVERHEATED. IAH - FLIGHT 2090, THE CREW REPORTED A STRONG ELECTRIC BURNING SMELL AROUND SEAT 1A AND THE GALLEY. MAINTENANCE REMOVED AND REPLACED THE FIRST FOUR LIGHT ASSEMB - [SDR C2XA10IA298](https://openairdocs.org/sdr/C2XA10IA298), Nov 17, 2010: LIGHT. OVERHEATED. IAH - FLIGHT 2090, THE CREW REPORTED A STRONG ELECTRIC BURNING SMELL AROUND SEAT 1A AND THE GALLEY. MAINTENANCE REMOVED AND REPLACED THE FIRST FOUR LIGHT ASSEMB - [SDR C2XA10IA297](https://openairdocs.org/sdr/C2XA10IA297), Nov 17, 2010: LIGHT. OVERHEATED. IAH - FLIGHT 2090 THE CREW REPORTED A STRONG ELECTRIC BURNING SMELL AROUND SEAT 1A AND THE GALLEY. MAINTENANCE REMOVED AND REPLACED THE FIRST FOUR CABIN LIGHT A - [SDR C2XA10CL156](https://openairdocs.org/sdr/C2XA10CL156), Oct 11, 2010: CONTROL UNIT. INTERMITTENT. THE CREW REPORTED DURING TAXI THE BRAKES SEEMED INTERMITTANT AND THEN GRAB HARD. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE BRAKE - [SDR C2XA10IA105](https://openairdocs.org/sdr/C2XA10IA105), Mar 25, 2010: BALLAST. OVERHEATED. IAH - DURING MAINTENANCE INSPECTION A BURNING SMELL WAS NOTICED AT SEAT 1A. MAINTENANCE REMOVED AND REPLACED THE LIGHTING BALLAST ABOVE SEAT 1A, OPERATIONALLY C - [SDR C2XA10IA101](https://openairdocs.org/sdr/C2XA10IA101), Mar 25, 2010: BALLAST. MALFUNCTIONED. CREW REPORTED BURNING SMELL AT FLIGHT ATTENDANT WINDSCREEN AREA. MAINTENANCE REMOVED AND REPLACED LIGHT BALLAST AT ROW NUMBER ONE. OPERATIONALLY CHECKED LIGHTS. - [SDR C2XA10IA046](https://openairdocs.org/sdr/C2XA10IA046), Jan 30, 2010: UNKNOWN. ODOR. IAH - FLIGHT 3047, THE CREW REPORTED A POSSIBLE LIGHTNING STRIKE DUE TO A BRIGHT FLASH AND A BURNING SMELL. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MA - [SDR C2XA09SH504](https://openairdocs.org/sdr/C2XA09SH504), Dec 17, 2009: SKIN. CORRODED. SHV - DURING C-CHECK CORROSION (LEVEL 2 LOCAL) ON FUSELAGE SKIN STRINGERS 18L-18R FRAMES 59-60. MAINTENANCE PERFORMED REPAIR ON FUSELAGE SKIN STRINGERS 18L-18R - [SDR C2XA09SH501](https://openairdocs.org/sdr/C2XA09SH501), Dec 14, 2009: SKIN. CORRODED. SHV - DURING C-CHECK CORROSION (LEVEL 3 LOCAL) UNDER SEALANT AT FRAME 58 WATER HEATERS. MAINTENANCE PERFORMED ALL WORK IAW EC5330-02032. THE AIRCRAFT WAS APPROV - [SDR C2XA09SH498](https://openairdocs.org/sdr/C2XA09SH498), Dec 14, 2009: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK RT OMEGA BEAM CORRODED (LEVEL 3 LOCAL) AROUND NUT PLATE HOLE AT FRAME 18. MAINTENANCE INSTALLED REPAIRED RT OMEGA BEAM AT FRAME 18 IAW EMB- - [SDR C2XA09SH497](https://openairdocs.org/sdr/C2XA09SH497), Dec 14, 2009: SKIN. CORRODED. SHV - DURING C-CHECK CORROSION (LEVEL 3) ON FUSELAGE SKIN STRINGERS 18L-18R FRAMES 57-58. MAINTENANCE REPAIRED AREA OF CORRODED FUSELAGE SKIN AT STRINGERS 18L-1 - [SDR C2XA09SH496](https://openairdocs.org/sdr/C2XA09SH496), Dec 14, 2009: SKIN. CORRODED. SHV - DURING C-CHECK CORROSION (LEVEL 3 LOCAL) ON FUSELAGE SKIN STRINGERS 18L-18R FRAMES 58-59. MAINTENANCE REPAIRED FUSELAGE SKIN WHERE CORROSION WAS FOUND AT - [SDR C2XA09SH495](https://openairdocs.org/sdr/C2XA09SH495), Dec 14, 2009: SKIN. CRACKED. SHV - DURING C-CHECK CRACKS AROUND RIVETS AT FRAME 75, 77 AND 79 RT SIDE. MAINTENANCE REPAIRED FUSELAGE SKIN AT MARKED RIVETS AT FRAME 75, 77 AND 79 RT SIDE IAW - [SDR C2XA09SH494](https://openairdocs.org/sdr/C2XA09SH494), Dec 14, 2009: SKIN. CRACKED. SHV - DURING C-CHECK CRACKS AROUND RIVETS AT FRAME 77-78 LT SIDE. MAINTENANCE REPAIRED THE FUSELAGE SKIN AT MARKED RIVETS AT FRAMES 77-78 LT SIDE IAW EC 5330-02 - [SDR C2XA09SH491](https://openairdocs.org/sdr/C2XA09SH491), Dec 11, 2009: SKIN. CORRODED. SHV - DURING C-CHECK, FUSELAGE SKIN CORRODED AT FR 58. REPAIRED SKIN IAW EC5330-02032. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09SH489](https://openairdocs.org/sdr/C2XA09SH489), Dec 8, 2009: SHEAR TIE. CRACKED. SHV - DURING C-CHECK SHEAR CLIP CRACKED AT FRAME 24 STRINGER 15R-16R. MAINTENANCE REMOVED AND REPLACED SHEAR CLIP AT FRAME 24 STRINGER 15R-16R IAW EMB-145 SRM 5 - [SDR C2XA09SH488](https://openairdocs.org/sdr/C2XA09SH488), Dec 8, 2009: FITTING. CRACKED. SHV - DURING C-CHECK SHEAR CLIP CRACKED AT FRAME 26 STRINGER 14R-15R. MAINTENANCE REMOVED AND REPLACED SHEAR CLIP AT FRAME 26 STRINGER 14R-15R IAW EMB-145 SRM 5 - [SDR C2XA09SH487](https://openairdocs.org/sdr/C2XA09SH487), Dec 8, 2009: FITTING. CRACKED. SHV - DURING C-CHECK SHEAR CLIP CRACKED AT FRAME 24 STRINGER 16R-17R. MAINTENANCE REMOVED AND REPLACED SHEAR CLIP AT FRAME 24 STRINGER 16R-17R IAW EMB-145 SRM 5 - [SDR C2XA09SH486](https://openairdocs.org/sdr/C2XA09SH486), Dec 8, 2009: FITTING. CRACKED. SHV - DURING C-CHECK SHEAR CLIP CRACKED AT FRAME 25 STRINGER 15R-16R. MAINTENANCE REMOVED AND REPLACED SHEAR CLIP AT FRAME 25 STRINGER 15R-16R IAW EMB-145 SRM 5 - [SDR C2XA09SH485](https://openairdocs.org/sdr/C2XA09SH485), Dec 8, 2009: BEAM. CORRODED. SHV - DURING C-CHECK CARGO DOOR CUTOUT, INTERNAL, LOWER L-SHAPE CORRODED. MAINTENANCE REMOVED AND REPLACED CARGO DOOR, INTERNAL, LOWER L-SHAPE CORRODED LEVEL 3 - [SDR C2XA09SH484](https://openairdocs.org/sdr/C2XA09SH484), Dec 8, 2009: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK, CENTER OMEGA BEAM CORRODED AT FR 33-34. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09SH483](https://openairdocs.org/sdr/C2XA09SH483), Dec 8, 2009: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK, CENTER OMEGA BEAM CORRODED AT FR 24. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09SH482](https://openairdocs.org/sdr/C2XA09SH482), Dec 8, 2009: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK, CENTER OMEGA BEAM CORRODED AT FR 20. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09SH481](https://openairdocs.org/sdr/C2XA09SH481), Dec 8, 2009: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK, LT OMEGA BEAM CORRODED AT FR 20. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09SH480](https://openairdocs.org/sdr/C2XA09SH480), Dec 8, 2009: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK, LT OMEGA BEAM CORRODED AT FR 29. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09SH479](https://openairdocs.org/sdr/C2XA09SH479), Dec 8, 2009: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK, LT OMEGA BEAM CORRODED AT FR 33-34. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09SH478](https://openairdocs.org/sdr/C2XA09SH478), Dec 8, 2009: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK, LT OMEGA BEAM CORRODED AT FR 38. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09SH477](https://openairdocs.org/sdr/C2XA09SH477), Dec 8, 2009: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK, LT OMEGA BEAM CORRODED AT FR 44. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. All 101: https://openairdocs.org/deregistered/N12967-2017-01-05/reports.md ## Other aircraft with N12967 - [Cancelled 1993-09-20](https://openairdocs.org/deregistered/N12967-1993-09-20): Cessna 552, S/N 5520013. Owner: [The Cessna Aircraft Company](https://openairdocs.org/faa-owner/THE%20CESSNA%20AIRCRAFT%20COMPANY), [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita) - [Cancelled 1973-11-30](https://openairdocs.org/deregistered/N12967-1973-11-30): Cessna 172M, S/N 17262412, built 1973. Exported to Canada. Owner: [Fontana Aviation Inc](https://openairdocs.org/faa-owner/FONTANA%20AVIATION%20INC), [Iron Mountain, MI](https://openairdocs.org/faa-place/MI/Iron%20Mountain) --- 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.