# N12996: 2000 Embraer EMB-145LR, registration cancelled 2018-12-17 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 17, 2018 - Exported to: Libya - 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: 145296 - Year built: 2000 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: August 13, 2000 - Certificate issued: May 21, 2018 - Last registry action: November 19, 2018 - Mode S code: A078D3 - Owner when cancelled: [Tvpx Aircraft Solutions Inc Trustee](https://openairdocs.org/faa-owner/TVPX%20AIRCRAFT%20SOLUTIONS%20INC%20TRUSTEE) - Location: [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake) - Owner type: Corporation - Owner's area on the map: 40.8386° N, 111.9179° W: Placed by OpenAirDocs at the center of ZIP code 84054, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N12996 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=12996 - Page: https://openairdocs.org/deregistered/N12996-2018-12-17 From the FAA registry file of November 7, 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 (59, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASOA20150828165](https://openairdocs.org/sdr/ASOA20150828165), Aug 28, 2015: FRAME. CORRODED. DURING C-CHECK THE SERVICE DOOR LOWER FRAME WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5240-01102. THE ACF - [SDR ASOA20150828164V](https://openairdocs.org/sdr/ASOA20150828164V), Aug 28, 2015: 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 EC5210-01036. THE - [SDR ASOA20150828163](https://openairdocs.org/sdr/ASOA20150828163), Aug 28, 2015: SKIN. CRACKED. DURING C-CHECK THE RT AFT SKIN WAS FOUND TO BE CRACKED AROUND 5 FASTENER LOCATIONS BETWEEN FRAMES 77-78, STR 3R-6R. MAINTENANCE PERFORMED BUSHING REPAIRS IAW EC - [SDR ASOA20150828162](https://openairdocs.org/sdr/ASOA20150828162), Aug 28, 2015: FITTING. CRACKED. DURING C-CHECK THE RT OTBD FLAP INBD ROLLER FITTING WAS FOUND TO BE CRACKED AND VERIFIED WITH EDDY CURRENT. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5750-01 - [SDR ASOA20150219014](https://openairdocs.org/sdr/ASOA20150219014), Feb 19, 2015: ENGINE. LEAKING. THE CREW REPORTED LAVATORY SMOKE WARNING MESSAGE AND SMOKE IN THE CABIN. MAINTENANCE REPLACED THE NR 2 ENGINE. OPS CHECKED WERE GOOD. - [SDR ASOA20150207009](https://openairdocs.org/sdr/ASOA20150207009), Feb 7, 2015: SMOKE DETECTOR. FALSE INDICATION. THE CREW REPORTED A LAVATORY SMOKE WARNING INDICATION ON THE EICAS ON CLIMBOUT. MAINTENANCE INSPECTED AND REPLACED THE LAVATORY SMOKE SENSOR. OPS CHECKED GOOD. - [SDR ASOA20141111091](https://openairdocs.org/sdr/ASOA20141111091), Nov 11, 2014: SMOKE DETECTOR. FALSE ACTIVATION. THE CREW REPORTED A MOMENTARY LAVATORY SMOKE MESSAGE DURING FLIGHT. MAINTENANCE INSPECTED AND R & R SMOKE DETECTOR. OPS CHECKS WERE GOOD. - [SDR ASOA20141021118](https://openairdocs.org/sdr/ASOA20141021118), Oct 21, 2014: SMOKE DETECTOR. FALSE INDICATION. PILOT REPORTED A LAVATORY SMOKE WARNING INDICATION ON EICAS WITH NO INDICATION OF SMOKE OR FIRE. MAINTENANCE INSPECTED LAVATORY FOR SMOKE AND EVIDENCE OF FIRE W - [SDR ASOA20140930121](https://openairdocs.org/sdr/ASOA20140930121), Sep 30, 2014: SMOKE WARNING. FALSE ACTIVATION. CREW REPORTED A LAVATORY SMOKE MESSAGE ON EICAS AFTER TAKE OFF. THE ACFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE ACFT, LAV WIRING WITH NO DEFECT - [SDR ASOA20140916113](https://openairdocs.org/sdr/ASOA20140916113), Sep 16, 2014: STRUCTURE. DAMAGED. DURING 1A INSPECTION, A SMALL HOLE WAS FOUND IN THE CARGO DOOR LOWER FWD CORNER. MAINTENANCE PERFORMED AN INTERNAL DOUBLER REPAIR TO THE CARGO DOOR, OPS TESTED - [SDR ASOA20140608066](https://openairdocs.org/sdr/ASOA20140608066), Jun 8, 2014: BRAKE ASSY. SLIPPED. PILOT REPORTED THE BRAKES SLIPPING ON LANDING AND VERY NOISE DURING SLOW TAXI. MX R & R 1 BRAKE ASSY OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE - [SDR ASOA20131114127](https://openairdocs.org/sdr/ASOA20131114127), Nov 14, 2013: DISPLAY. SHORTED. NR 2 PFD CIRCUIT BREAKER TRIPPED WITH BURNING ODOR IN COCKPIT. MAINTENANCE R & R THE NR 2 PFD, OPS CHECKED SUCCESSFUL. ACFT APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20130901218V](https://openairdocs.org/sdr/ASOA20130901218V), Sep 1, 2013: BUSHING. MIGRATED. DURING C-CHECK, LT AILERON OTBD PCA ATTACHMENT FITTING OTBD LUG, OTBD HAT BUSHING MIGRATED. MX R & R THE LT AILERON OTBD PCA ATTACHMENT FITTING IAW EC5750-01177 - [SDR ASOA20130622062R](https://openairdocs.org/sdr/ASOA20130622062R), Jun 22, 2013: LIGHT. INOPERATIVE. DURING SCHEDULED MX INSPECTION, THE CABIN FLOOR EMERGENCY LIGHTS AT ROW 6 AND 7 WERE INOPERATIVE. MX R & R THE FLOOR STRIP LIGHT WITH OPS CHECK SUCCESSFUL. ACFT - [SDR C2XA11SH162](https://openairdocs.org/sdr/C2XA11SH162), Oct 25, 2011: DOOR FRAME. CORRODED. SHV - DURING C-CHECK PAX DOOR FRAME LOWER SECTION HAS CORRODED NUT PLATE HOLES (NEAR DOOR SEAL). MAINTENANCE PERFORMED REPAIR AT PAX DOOR LOWER NUT PLATE AREAS - [SDR C2XA11SH161](https://openairdocs.org/sdr/C2XA11SH161), Oct 25, 2011: SKIN. GOUGED. SHV - DURING C-CHECK BAGGAGE DOOR INNER FRAME SKIN GOUGED AT LOWER, FWD AND CENTER AREAS. MAINTENANCE PERFORMED REPAIR ON BAGGAGE DOOR INNER SKIN IAW EC5230-012 - [SDR C2XA11SH160](https://openairdocs.org/sdr/C2XA11SH160), Oct 25, 2011: FRAME. CORRODED. SHV - DURING C-CHECK CORROSION PRESENT IN AREA WHERE THE SHUNT CONNECTION BAR COMES IN CONTACT WITH STRUCTURE. MAINTENANCE PERFORMED REPAIR AT APU SHUNT FRAME 8 - [SDR C2XA11SH159](https://openairdocs.org/sdr/C2XA11SH159), Oct 25, 2011: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM SUPPORT FLANGE AT FRAME 21-25 NUT PLATE CORRODED. MAINTENANCE PERFORMED REPAIR AND INSTALLED FABRICATED DOUBLER AT LT OMEGA B - [SDR C2XA11SH158](https://openairdocs.org/sdr/C2XA11SH158), Oct 25, 2011: SKIN. CANNING. SHV - DURING C-CHECK STRINGER 11 EXTERNAL FUSELAGE PATCH JUST AFT OF PAX DOOR IS OIL CANNING. MAINTENANCE PERFORMED REPAIR AT STRINGER 11L JUST AFT OF PAX DOOR - [SDR C2XA11IA085](https://openairdocs.org/sdr/C2XA11IA085), May 7, 2011: COMPUTER. FAILED. IAH - FLIGHT 2695, DURING TAKEOFF THE CREW REPORTED THAT THE NUMBER ONE AHRS COMPUTER FAILED. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAI - [SDR C2XA10CL107](https://openairdocs.org/sdr/C2XA10CL107), Jul 8, 2010: ELECTRONIC UNIT. FAULTY. CLE FLT 2209 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE LGEU. OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA10IA163](https://openairdocs.org/sdr/C2XA10IA163), May 28, 2010: O-RING. LEAKING. IAH - FLIGHT 2948, THE CREW REPORTED A BLEED ONE LEAK IN CLIMB OUT THAT CLEARED UPON CLOSING BLEED ONE WITH NO APU. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED - [SDR C2XA09SH503](https://openairdocs.org/sdr/C2XA09SH503), Dec 17, 2009: FLOOR SKIN. CORRODED. SHV - DURING C-CHECK FUSELAGE FLOOR SKIN CORRODED (LEVEL 2 LOCAL) BETWEEN FRAMES 61-62 STRINGERS 21L-21R. MAINTENANCE PERFORMED REPAIR ON FUSELAGE SKIN BETWEEN - [SDR C2XA09SH490](https://openairdocs.org/sdr/C2XA09SH490), Dec 11, 2009: FRAME. CRACKED. SHV - DURING C-CHECK, FR 10 CRACKED AT STR 10L. REMOVED AND REPLACED FRAME IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09SH473](https://openairdocs.org/sdr/C2XA09SH473), Dec 7, 2009: FRAME. CRACKED. SHV - DURING C-CHECK RT HALF FRAME AT FRAME 10 IS CRACKED AT DV WINDOW. MAINTENANCE REMOVED AND REPLACED RT HALF FRAME AT FRAME 10 AT DV WINDOW. THE AIRCRAFT WA - [SDR C2XA09SH469](https://openairdocs.org/sdr/C2XA09SH469), Dec 7, 2009: SUPPORT. CORRODED. SHV - DURING C-CHECK LT UPPER SEAT TRACK SUPPORT CORRODED (LEVEL 3 LOCAL) AT FRAME 46 ATTACHMENT. MAINTENANCE REPAIRED LT UPPER SEAT TRACK SUPPORT AT FRAME 46 I - [SDR C2XA09SH468](https://openairdocs.org/sdr/C2XA09SH468), Dec 7, 2009: SUPPORT. CORRODED. SHV - DURING C-CHECK LT UPPER SEAT TRACK SUPPORT CORRODED (LEVEL 3 LOCAL) AT FRAME 50 ATTACHMENT. MAINTENANCE REPAIRED LT UPPER SEAT TRACK SUPPORT AT FRAME 50 I - [SDR C2XA09SH467](https://openairdocs.org/sdr/C2XA09SH467), Dec 7, 2009: SUPPORT. CORRODED. SHV - DURING C-CHECK RT UPPER SEAT TRACK SUPPORT CORRODED (LEVEL 2 LOCAL) AT FRAME 50 IAW EC5320-01512. MAINTENANCE REPAIRED RT UPPER SEAT TRACK SUPPORT AT FRAM - [SDR C2XA09SH466](https://openairdocs.org/sdr/C2XA09SH466), Dec 7, 2009: SUPPORT. CORRODED. SHV - DURING C-CHECK RT UPPER SEAT TRACK SUPPORT CORRODED (LEVEL 2 LOCAL) AT FRAME 46. MAINTENANCE REPAIRED RT UPPER SEAT TRACK SUPPORT AT FRAME 46 IAW EC5320-0 - [SDR C2XA09RI187](https://openairdocs.org/sdr/C2XA09RI187), Oct 30, 2009: SIGN. INOPERATIVE. RIC MX - DURING ROUTINE MAINTENANCE, MX FOUND EXIT SIGN IN FRONT OF SEAT 3B INOPERATIVE. MX REMOVED AND REPLACED EXIT SIGN AND PERFORMED OPERATIONAL CHECK SUCCE - [SDR C2XA09RI133](https://openairdocs.org/sdr/C2XA09RI133), Aug 3, 2009: POWER SUPPLY. NOT SEATED. RIC - MX - DURING ROUTINE MAINTENANCE, MX FOUND RIGHT WING AFTERWARD EMERGENCY LIGHT AND EMERGENCY LIGHT IN FRONT OF SEAT 3B INOPERATIVE. MX RESEATED NR 3 EMERG - [SDR C2XA09RI054](https://openairdocs.org/sdr/C2XA09RI054), Mar 24, 2009: BATTERY. DISCHARGED. EWR MX - DURING ROUTINE MAINTENANCE, MX FOUND EMERGENCY EXIT LIGHT AT OVERWING CEILING INOPERATIVE. MX REMOVED AND REPLACED NR 3 BATTERY AND PERFORMED OPERATION - [SDR C2XA09RI053](https://openairdocs.org/sdr/C2XA09RI053), Mar 24, 2009: BATTERY. DISCHARGED. EWR MX - DURING ROUTINE MAINTENANCE, MX FOUND EMERGENCY EXIT LIGHT ON AFT GALLEY WALL INOPERATIVE. MX REMOVED AND REPLACED NR 2 BATTERY AND PERFORMED OPERATIONA - [SDR C2XA09CL028](https://openairdocs.org/sdr/C2XA09CL028), Mar 12, 2009: TRIM SWITCH. INTERMITTENT. CLE FLIGHT 2080 - THE CREW REPORTED THE PITCH TRIM WAS INOPERATIVE AFTER TAKEOFF. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTE - [SDR C2XA09IA028](https://openairdocs.org/sdr/C2XA09IA028), Jan 31, 2009: WINDSHIELD. CRACKED. OKC - FLIGHT 2205 - THE CREW REPORTED THAT THE FIRST OFFICERS WINDSHIELD CRACKED ON CLIMBOUT BLOCKING VISIBILITY. THE AIRCRAFT RETURNED TO OKC WHERE IT LANDED W - [SDR C2XA09IA031](https://openairdocs.org/sdr/C2XA09IA031), Jan 24, 2009: INVERTER. INOPERATIVE. MCI - DURING MAINTENANCE INSPECTION THE RIGHT OVERWING EMERGENCY EXIT MARKER LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FIVE - [SDR C2XA08IA038](https://openairdocs.org/sdr/C2XA08IA038), Jan 23, 2008: INVERTER. INOPERATIVE. MCI - DURING MAINTENANCE INSPECTION THE FORWARD OVERWING CEILING EXIT LOCATOR SIGN WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER 6 EM - [SDR C2XA07BT024](https://openairdocs.org/sdr/C2XA07BT024), Mar 5, 2007: CONNECTOR. DIRTY. EWR LOG SQUAWK FLT 2347 FORWARD OVERHEAD EMERGENCY EXIT LOCATER SIGN AT ROW 11 OUT. CLEANED CONNECTOR AND RESECURED FORWARD EMERGENCY EXIT LOCATER AT ROW 11 IAW - [SDR C2XA05BT071](https://openairdocs.org/sdr/C2XA05BT071), Oct 7, 2005: SIGN. FAULTY. DURING SERVICE ROUTINE CHECK ON OVERNIGHT, MAINTENANCE FOUND ROW 12 OVERHEAD EMERGENCY EXIT SIGN NOT WORKING. REMOVED AND REPLACED ROW 12 OVERHEAD EMERGENCY EXI - [SDR C2XA05CL046](https://openairdocs.org/sdr/C2XA05CL046), Jun 15, 2005: WARNING LIGHT. FALSE ACTIVATION. MHT FLIGHT 3054, THE CREW REPORTED A BAGGAGE COMPARTMENT SMOKE INDICATION ON THE EICAS THAT WOULD NOT CLEAR. MAINTENANCE INSPECTED AND RESET AIRCRAFT POWER. OPE - [SDR C2XA04RI016](https://openairdocs.org/sdr/C2XA04RI016), Nov 28, 2004: AMPLIFIER. FAILED. ORF - FLT 2017, DURING PREFLIGHT CHECK THE CREW FOUND CABIN AND CABIN EMERGENCY LIGHTS IN OVERHEAD PANEL ILLUMINATED AND CABIN INTERPHONE AND PA INOP. MAINTENAN - [SDR C2XA04CL061](https://openairdocs.org/sdr/C2XA04CL061), Jun 4, 2004: LIGHT. INOPERATIVE. CLE FLIGHT 2266, THE CREW REPORTED THAT THE SECOND TO AFT EMERGENCY LIGHT STRIP WAS INOP WHEN TESTED. MAINTENANCE INSPECTED, REMOVED AND REPLACED THE LIGHT STRI - [SDR C2XA04CL018](https://openairdocs.org/sdr/C2XA04CL018), Mar 7, 2004: TRIM SYSTEM. MALFUNCTIONED. IAH FLIGHT 2390 CREW REPORTED, ROLL TRIM RUN-AWAY AFTER TAKEOFF FROM IAH. CREW FOLLOWED QRH AND RESET CIRCUIT BREAKER FOR AILERON TRIM. SYSTEM OPS CHECKED GOOD. - [SDR CX2A04SH012](https://openairdocs.org/sdr/CX2A04SH012), Jan 9, 2004: ANGLE. CHAFED. SHV-DURING C CHECK THE NR 2 ENGINE LOWER COWLING AFT OB EDGE MEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR - [SDR C2XA04SH006](https://openairdocs.org/sdr/C2XA04SH006), Jan 4, 2004: BUTTSTRAP. CORRODED. SHV- DURING C-CHECK THE FWD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 53-21-10. THE AI - [SDR C2XA04SH005](https://openairdocs.org/sdr/C2XA04SH005), Jan 4, 2004: BUTTSTRAP. CORRODED. SHV- DURING C-CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 20 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 - [SDR C2XA04SH004](https://openairdocs.org/sdr/C2XA04SH004), Jan 4, 2004: STIFFENER. CHAFED. SHV- DURING C-CHECK THE NUMBER 2 ENGINE LOWER COWLING AFT STIFFENER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 - [SDR C2XA03SH526](https://openairdocs.org/sdr/C2XA03SH526), Dec 31, 2003: RIB. GOUGED. DURING C CHECK THE AFT EDGE MEMBER WAS FOUND TO BE GOUGED AT THE SIX O'CLOCK POSITION. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW E - [SDR C2XA03SH524](https://openairdocs.org/sdr/C2XA03SH524), Dec 30, 2003: BEAM. CORRODED. SHV-DURING C-CHECK THE LOWER CARGO DOOR CUT OUT BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE - [SDR C2XA03SH523](https://openairdocs.org/sdr/C2XA03SH523), Dec 30, 2003: FLOORBEAM. CORRODED. SHV-DURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 19. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE A All 59: https://openairdocs.org/deregistered/N12996-2018-12-17/reports.md ## Other aircraft with N12996 - [Cancelled 1936-03-15](https://openairdocs.org/deregistered/N12996-1936-03-15): Ray Besasie BESASIE, S/N 2, built 1933. Owner: [Besasie Ray](https://openairdocs.org/faa-owner/BESASIE%20RAY), [Milwaukee, WI](https://openairdocs.org/faa-place/WI/Milwaukee) --- 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.