# N12924: 2000 Embraer EMB-145LR, registration cancelled 2017-04-03 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: April 3, 2017 - Exported to: Cameroon - Status when cancelled: Valid registration - Airframe: [Embraer EMB-145LR](https://openairdocs.org/model/embraer-emb-145lr) (registry code 3260212) - Engine: [Allison AE-3007A](https://openairdocs.org/engine/allison-ae-3007a) (registry code 03030) - Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (OpenAirDocs) - Serial number: 145311 - Year built: 2000 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 24, 2000 - Certificate issued: March 24, 2017 - Last registry action: March 24, 2017 - Mode S code: A077DC - Owner when cancelled: [Southern Aircraft Consultancy Inc Trustee](https://openairdocs.org/faa-owner/SOUTHERN%20AIRCRAFT%20CONSULTANCY%20INC%20TRUSTEE) - Location: Bungay Suffolk, United Kingdom - Owner type: Corporation - The mark today: https://openairdocs.org/aircraft/N12924 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=12924 - Page: https://openairdocs.org/deregistered/N12924-2017-04-03 From the FAA registry file of October 29, 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 (55, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASOA201610270625](https://openairdocs.org/sdr/ASOA201610270625), Oct 27, 2016: CONTROL MODULE. ODOR. F/A REPORTS A BURNING SMELL COMING FROM BEHIND SPEAKER IN GALLEY. MX REMOVED AND REPLACED GALLEY LIGHTING CONTROL MODULE POWERED A/C WITH NO BURNING SMELL FOUND - [SDR ASOA20160510022R](https://openairdocs.org/sdr/ASOA20160510022R), May 10, 2016: CONTROL MODULE. SHORTED. CREW REPORTED THE RIGHT SIDEWALL PASSENGER LIGHTS WOULD NOT TURN ON AND PRODUCED A BURNING ODOR. MAINTENANCE R & R THE LIGHTS CONTROL MODULE WITH OPS CHECK GOOD - [SDR ASOA20150609057](https://openairdocs.org/sdr/ASOA20150609057), Jun 9, 2015: PACKING. TORN. THE CREW REPORTED THAT THE ACFT HAD A VERY STRONG ODOR ASSOCIATED WITH THE PACKS. THE AIRCRAFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE ACFT, R & - [SDR ASOA20150602125](https://openairdocs.org/sdr/ASOA20150602125), Jun 2, 2015: DOOR FRAME. CORRODED. DURING C-CHECK THE MAIN CABIN DOOR LOWER FRAME WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5210-01348. THE - [SDR ASOA20150602124](https://openairdocs.org/sdr/ASOA20150602124), Jun 2, 2015: STRINGER. CORRODED. DURING C-CHECK STRINGER 20R WAS FOUND TO BE CORRODED BETWEEN FRAMES 13-14. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A SPLICE REPAIR IAW SRM 53-00-03. THE - [SDR ASOA20150602123V](https://openairdocs.org/sdr/ASOA20150602123V), Jun 2, 2015: SKIN. CRACKED. DURING C-CHECK, THE RT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AROUND 3 FASTENERS BETWEEN FRAMES 78-79, STRINGERS 2R-5R. MAINTENANCE PERFORMED 3 BUSHING REPAI - [SDR ASOA20150602122V](https://openairdocs.org/sdr/ASOA20150602122V), Jun 2, 2015: SKIN. CRACKED. DURING C-CHECK, THE LT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AROUND 4 FASTENERS BETWEEN FRAMES 77-78, STRINGERS 3L-4L. MAINTENANCE PERFORMED 4 BUSHING REPAI - [SDR ASOA20150528121](https://openairdocs.org/sdr/ASOA20150528121), May 28, 2015: FIREWALL. CANNING. DURING C-CHECK THE APU FIREWALL AT FRAME 81 WAS FOUND TO BE OIL-CANNING BY THE LT SIDE STIFFENER BELOW THE BLEED DUCT. MAINTENANCE PERFORMED A DOUBLER REPAIR IA - [SDR ASOA20150528120](https://openairdocs.org/sdr/ASOA20150528120), May 28, 2015: FLOOR SUPPORT. CORRODED. DURING C-CHECK THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 23. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5320-02044. THE AC - [SDR ASOA20150528119](https://openairdocs.org/sdr/ASOA20150528119), May 28, 2015: SKIN. CRACKED. DURING C-CHECK THE RT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75, STRINGERS 1R-2R. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5330-03019. THE ACFT - [SDR ASOA20130917109](https://openairdocs.org/sdr/ASOA20130917109), Sep 17, 2013: LIGHT. INOPERATIVE. DURING MX INSPECTION THE AISLE FLOOR EMERGENCY LIGHT AT ROW 16 WAS DISCOVERED INOPERATIVE. MX R & R LIGHT, OPS CHECKED SUCCESSFUL. ACFT APPROVED FOR RETURN TO S - [SDR ASOA20130703071](https://openairdocs.org/sdr/ASOA20130703071), Jul 3, 2013: ACM. SEIZED. CREW REPORTED SMOKE IN COCKPIT AND CABIN IN FLIGHT. MX PERFORMED ABNORMAL SMOKE INSPECTION OF CABIN & COCKPIT AND FOUND NR 1 ACM DAMAGED. R & R NR 1 ACM WITH OP - [SDR ASOA20130616090](https://openairdocs.org/sdr/ASOA20130616090), Jun 16, 2013: FLAPPER BEARING. LEAKING. DURING CLIMB, THE CREW REPORTED FUEL LEAKING FROM THE RT WING. THE ACFT RETURNED TO AIRPORT WHERE IT LANDED WITHOUT INCIDENT. MX R & R THE OTBD FLAPPER VALVE IN - [SDR ASOA20121025084](https://openairdocs.org/sdr/ASOA20121025084), Oct 25, 2012: CHARGER. FAULTY. DURING ROUTINE MX, AFT ASILE EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MX REPLACED THE BATTERY POWER SUPPLY CHARGER. OPS CHECKED GOOD. - [SDR ASOA20121012082](https://openairdocs.org/sdr/ASOA20121012082), Oct 12, 2012: BATTERY PACK. INOPERATIVE. DURING ROUTINE MX, THE REAR INTERIOR AND EXTERIOR EMERGENCY LIGHTS WOULD NOT TEST. MX REPLACED THE NR 4 EMERGENCY LIGHT BATTERY PACK. OPS CHECKS WERE GOOD. - [SDR ASOA20120923084R](https://openairdocs.org/sdr/ASOA20120923084R), Sep 23, 2012: BATTERY PACK. INOPERATIVE. DURING MX INSPECTION, FOUND NR 4 EMERGENCY LIGHT BATTERY WILL NOT CHARGE. MX R & R NR 4 EMERGENCY LIGHT BATTERY PACK WITH OPS CHECKED SUCCESSFUL. ACFT WAS APPRO - [SDR ASOA20120824064](https://openairdocs.org/sdr/ASOA20120824064), Aug 24, 2012: CHARGER. INOPERATIVE. DURING MX INSPECTION, THE LT AND RT EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MX R & R THE NR 4 BATTERY CHARGING TRAY WITH OPS CHECK SUCCESSFUL - [SDR C2XA11RI091](https://openairdocs.org/sdr/C2XA11RI091), May 24, 2011: CONTROLLER. DEFECTIVE. FLIGHT 6165 - IAD - FLIGHT CREW REPORTED AUTO PRESS ERRACTIC. IAD MX MEL`ED THE SYSTEM. RIC MX PERFORMED OPERATIONAL CHECK OF AUTO PRESSURIZATION AND COULD NOT - [SDR C2XA11RI090](https://openairdocs.org/sdr/C2XA11RI090), May 24, 2011: CONTROLLER. DEFECTIVE. FLIGHT 5790 - ORF - FLIGHT CREW REPORTED PRESSURIZATION FAIL IN AUTO AND MANUAL MODE. RIC MX PERFORMED OPERATIONAL CHECK OF AUTO PRESSURIZATION AND COULD NOT DU - [SDR C2XA11IA088](https://openairdocs.org/sdr/C2XA11IA088), May 8, 2011: FLOW DIVIDER. LEAKING. FLIGHT 2557 FROM IND THE CREW REPORTED A STRONG FUEL ODOR IN THE COCKPIT DURING TAKEOFF. THE AIRCRAFT CONTINUED, WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE I - [SDR C2XA10CL112](https://openairdocs.org/sdr/C2XA10CL112), Jul 12, 2010: O-RING. DETERIORATED. THE CREW REPORTED A "BLEED 1 LEAK" MESSAGE ON CLIMB. THE AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE BLEED DUCT O-RING - [SDR C2XA10TY058](https://openairdocs.org/sdr/C2XA10TY058), Apr 18, 2010: LIGHT. INOPERATIVE. TYS - EMERGENCY LIGHT ABOVE RT PACK PANEL INOP. REMOVED AND REPLACED BULB. - [SDR C2XA10RI036](https://openairdocs.org/sdr/C2XA10RI036), Mar 12, 2010: UNKNOWN. ODOR. FLIGHT 3073 - EWR - FLIGHT CREW REPORTED STRONG SMELL NOTICEABLE IN PAST HALF OF ACFT CABIN. EWR MX PERFORMED OPERATIONAL CHECK OF THE PACKS AND PERFORMED CABIN - [SDR C2XA09TY249](https://openairdocs.org/sdr/C2XA09TY249), Sep 29, 2009: ATTACH BRACKET. CORRODED. FRETTING AT FRM 75 STR 1R AT FUSELAGE TO STAB ATTACH BRACKET AS MARKED. REMOVED FITTING AT FRM 75, BLENDED CORROSION, PERFORMED DYE-PEN, REPAIRED FITTING AND IN - [SDR C2XA09TY248](https://openairdocs.org/sdr/C2XA09TY248), Sep 29, 2009: FITTING. DAMAGED. FRM 75 UPPER FITTING HAS OVERSIZED HOLE ON RT O/B HOLE. REMOVED, REPAIRED AND INSTALLED FITTING IAW EC5530-01187, EMB 145 SRM 51-40-02 AND EC5310-01317. - [SDR C2XA09TY237](https://openairdocs.org/sdr/C2XA09TY237), Sep 17, 2009: STRUCTURE. CORRODED. TYS - A/C CURRENTLY IN C-CHECK AND INSPECTION FOUND CORROSION IN TWO HOLES ON THE NR 2 ENGINE INLET. MAINTENANCE REAMED THE HOLES AND INSTALL BUSHINGS TO REMOVE - [SDR C2XA09RI158](https://openairdocs.org/sdr/C2XA09RI158), Sep 7, 2009: TUBE. LEAKING. FLIGHT CREW REPORTED ENGINE BLEED NR 2 LEAK AFTER TAKEOFF. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED NR 2 BLEED SYSTEM TUBE - [SDR C2XA09IA193](https://openairdocs.org/sdr/C2XA09IA193), Jul 29, 2009: O-RING. BLOWN. IAH - FLIGHT 2695, THE CREW REPORTED A BLD 2 LK INDICATION ON EICAS. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AI - [SDR C2XA09IA105](https://openairdocs.org/sdr/C2XA09IA105), Apr 22, 2009: AHRS. INOPERATIVE. IAH - FLIGHT 2027, THE CREW REPORTED AN AHRS1 FAIL / ATT FAIL 1, AND SPS ADVANCE ON CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTE - [SDR C2XA08CL021](https://openairdocs.org/sdr/C2XA08CL021), Feb 18, 2008: RELAY. FAULTY. CLE FLIGHT 2793 - THE CREW REPORTED MULTIPLE WARNINGS DURING CLIMB E1 FUEL LO LEVEL, AMBER DASHES ON FUEL TOTAL + TANK 2 FUEL LEVELS, RMU NR 2 BLANK, APU SHUTOF - [SDR C2XA07IA252](https://openairdocs.org/sdr/C2XA07IA252), Dec 20, 2007: LANDING GEAR. MALFUNCTIONED. FLIGHT 2412 - DGO - IAH, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO DGO AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS R - [SDR C2XA07BT012](https://openairdocs.org/sdr/C2XA07BT012), Jan 26, 2007: UNKNOWN. ODOR. FLT NR 2312 - SMELLED BURNING ODOR 20 MINUTES AND 5 MINUTES BEFORE LANDING. NO SMOKE OBSERVED. FLT ATTENDANT SMELLED IT FIRST IN FWD CABIN. INSP COCKPIT AREA OV - [SDR C2XA06IA068](https://openairdocs.org/sdr/C2XA06IA068), May 2, 2006: BATTERY PACK. LOOSE. STL - DURING MAINTENANCE INSPECTION BOTH OVERWING EMERGENCY EXITS WERE FOUND TO BE INOPERATIVE. MAINTENANCE RESECURED THE NUMBER THREE EMERGENCY LIGHT BATTERY P - [SDR C2XA06IA041](https://openairdocs.org/sdr/C2XA06IA041), Mar 12, 2006: BALLAST. MALFUNCTIONED. IAH - FLIGHT 2732, A BURNING SMELL WAS NOTICED IN THE GALLEY. MAINTENANCE REMOVED AND REPLACED TWO LIGHT BALLASTS, OPERATIONALLY CHECKED WITH NO DEFECTS, AND TH - [SDR C2XA03SH510](https://openairdocs.org/sdr/C2XA03SH510), Dec 22, 2003: STRIP. INOPERATIVE. SHV- DURING C-CHECK THE NR 4 AND NR 5 EMERGENCY PROXIMITY AISLE LIGHTS WOULD NOT ILLUMINATE DURING FUNCTIONAL CHECK. MAINTENANCE REMOVED AND REPLACED THE NR 5 P - [SDR C2XA03SH507](https://openairdocs.org/sdr/C2XA03SH507), Dec 18, 2003: SILL. CORRODED. SHV- DURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRC - [SDR C2XA03SH502](https://openairdocs.org/sdr/C2XA03SH502), Dec 18, 2003: BUTTSTRAP. CORRODED. SHV- DURING C-CHECK THE FORWARD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED AT FRAME 15. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR EMB - [SDR C2XA03SH508](https://openairdocs.org/sdr/C2XA03SH508), Dec 18, 2003: ANGLE. CORRODED. SHV- DURING C-CHECK THE LEFT HAND RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. - [SDR C2XA03SH506](https://openairdocs.org/sdr/C2XA03SH506), Dec 18, 2003: FLOORBEAM. CORRODED. SHV- DURING C-CHECK THE LEFT HAND OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 1 - [SDR C2XA03SH505](https://openairdocs.org/sdr/C2XA03SH505), Dec 18, 2003: FLOORBEAM. CORRODED. SHV- DURING C-CHECK THE LEFT HAND OMEGA BEAM BETWEEN FRAMES 23 AND 25 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REP - [SDR C2XA03SH504](https://openairdocs.org/sdr/C2XA03SH504), Dec 18, 2003: FLOORBEAM. CORRODED. SHV- DURING C-CHECK THE CENTER OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR - [SDR C2XA03SH503](https://openairdocs.org/sdr/C2XA03SH503), Dec 18, 2003: SILL. CORRODED. SHV- DURING C-CHECK THE LEFT HAND SILL BETWEEN FRAME 18 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-4 - [SDR C2XA03SH501](https://openairdocs.org/sdr/C2XA03SH501), Dec 17, 2003: ANGLE. CORRODED. SHV- DURING C-CHECK THE CENTER RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. TH - [SDR C2XA03SH500](https://openairdocs.org/sdr/C2XA03SH500), Dec 17, 2003: BUTTSTRAP. CORRODED. SHV-DURING C CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 20 AND 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 S - [SDR C2XA03SH499](https://openairdocs.org/sdr/C2XA03SH499), Dec 17, 2003: BUTTSTRAP. CORRODED. SHV- DURING C-CHECK THE AFT DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AI - [SDR C2XA03SH498](https://openairdocs.org/sdr/C2XA03SH498), Dec 17, 2003: FLOORBEAM. CORRODED. SHV-DURING C CHECK THE CENTER OMEGA BEAM BETWEEN FRAMES 16 AND 24 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 5 - [SDR C2XA03SH497](https://openairdocs.org/sdr/C2XA03SH497), Dec 13, 2003: BUTTSTRAP. CORRODED. SHV- DURUNG C-CHECK THE LEFT OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. TH - [SDR C2XA03SH496](https://openairdocs.org/sdr/C2XA03SH496), Dec 13, 2003: BUTTSTRAP. CORRODED. SHV- DURING C-CHECK THE RIGHT OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE RIGHT OMEGA BEAM BUTTSTRAP IAW EMB 145 SRM 51- - [SDR C2XA03SH494](https://openairdocs.org/sdr/C2XA03SH494), Dec 13, 2003: SILL. CORRODED. SHV- DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE - [SDR C2XA03SH493](https://openairdocs.org/sdr/C2XA03SH493), Dec 13, 2003: SUPPORT. CORRODED. SHV- DURING C-CHECK THE MAIN PASSENGER DOOR SILL SUPPORT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE MAIN PASSENGER DOOR SILL SUPPORT IAW EMB All 55: https://openairdocs.org/deregistered/N12924-2017-04-03/reports.md ## Other aircraft with N12924 - [Cancelled 1975-01-22](https://openairdocs.org/deregistered/N12924-1975-01-22): Cessna 172M, S/N 17262376, built 1973. Exported to Canada. Owner: [Tag Flight Inc](https://openairdocs.org/faa-owner/TAG%20FLIGHT%20INC), [Spring Valley, NY](https://openairdocs.org/faa-place/NY/Spring%20Valley) --- 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.