# N13956: 1998 Embraer EMB-145LR, registration cancelled 2015-12-10 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 10, 2015 - Exported to: Mexico - 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: 145078 - Year built: 1998 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 12, 1998 - Certificate issued: December 10, 2015 - Last registry action: December 10, 2015 - Mode S code: A09FC6 - 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/N13956 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=13956 - Page: https://openairdocs.org/deregistered/N13956-2015-12-10 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 (73, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASOA20141130141](https://openairdocs.org/sdr/ASOA20141130141), Nov 30, 2014: UNKNOWN. ODOR. THE CREW REPORTED AN OIL BURNING ODOR WITH THE PACKS RUNNING DURING TAKE OFF AND LANDING. MAINTENANCE INSPECTED THE ACFT AND PERFORMED HIGH POWER RUNS AND IDLE - [SDR ASOA20141128354V](https://openairdocs.org/sdr/ASOA20141128354V), Nov 28, 2014: SHEAR TIE. CRACKED. DURING C-CHECK LOWER SHEAR CLIP OTBD OF LT WING VENT VALVE CRACKED. MAINTENANCE R & R NEW SHEAR CLIP OTBD OF LT WING VENT VALVE IAW SRM 51-40-02. THE ACFT WAS A - [SDR ASOA20141128353V](https://openairdocs.org/sdr/ASOA20141128353V), Nov 28, 2014: BUSHING. MIGRATED. DURING C-CHECK, LT SECOND FROM OB ELEVATOR FITTING ASSY LOWER OTBD HAT BUSHING MIGRATED. MAINTENANCE R & R LT 2ND FROM OTBD ELEVATOR FITTING ASSY IAW SRM 51-40- - [SDR ASOA20141128352](https://openairdocs.org/sdr/ASOA20141128352), Nov 28, 2014: BUSHING. MIGRATED. DURING C-CHECK, RT ELEVATOR OTBD HINGE LOWER HAT BUSHING MIGRATED. MAINTENANCE R & R RT ELEVATOR OB HINGE FITTING ASSY IAW SRM 51-40-02. THE ACFT WAS APPROVED F - [SDR ASOA20141128351V](https://openairdocs.org/sdr/ASOA20141128351V), Nov 28, 2014: FRAME. CRACKED. DURING C-CHECK, COPILOTS FRAME 10 CRACKED BELOW DV WINDOW. MAINTENANCE R & R THE FRAME IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20140601061](https://openairdocs.org/sdr/ASOA20140601061), Jun 1, 2014: LIGHT. INOPERATIVE. THE CEILING EMERGENCY EXIT LIGHT ABOVE OVERWING EXIT WAS REPORTED INOPERATIVE. THE SYSTEM WAS RESET AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVIC - [SDR ASOA20130808061](https://openairdocs.org/sdr/ASOA20130808061), Aug 8, 2013: ACM. FAULTY. THE CREW REPORTED A PACK 1, OVERHEAT ON EICAS WITH BAD ODOR IN COCKPIT. MX REPLACED THE NR 1 ACM. OPS CHECKED GOOD. - [SDR ASOA20121203137](https://openairdocs.org/sdr/ASOA20121203137), Dec 3, 2012: SMOKE DETECTOR. NO TEST. DURING PREFLIGHT, LAVATORY SMOKE DETECTOR WILL NOT TEST. MX R & R LAVATORY SMOKE DETECTOR IAW AMM 26-14-01, OPS CHECKED GOOD. THE ACFT WAS APPROVED FOR RETURN T - [SDR ASOA20121118142](https://openairdocs.org/sdr/ASOA20121118142), Nov 18, 2012: FIREWALL. CRACKED. DURING A-CHECK INSPECTION, THE APU FIREWALL WAS FOUND TO BE CRACKED IN 2 LOCATIONS AS VIEWED FROM INSIDE THE AFT RIGGING BAY. MX INSPECTED THE FIREWALL AND FOUN - [SDR ASOA20120315038](https://openairdocs.org/sdr/ASOA20120315038), Mar 9, 2012: CHARGER. INOPERATIVE. DURING TEST, OVERWING EMERGENCY LIGHTS FOUND TO BE INOPERATIVE. MX REPLACED THE BATTERY CHARGER, TESTED SYSTEM AND CLEARED THE DISCREPANCY. - [SDR ASOA20120229019](https://openairdocs.org/sdr/ASOA20120229019), Feb 29, 2012: UNKNOWN. ODOR. PAX SITTING IN EXIT ROW REPORTED DETECTING AN ELECTRICAL BURNING ODOR TWO TIMES DURING DESCENT. MX PERFORMED OPS CHECKS OF BOTH PACKS, INSPECTED PACK COMPARTEME - [SDR ASOA20120220021H](https://openairdocs.org/sdr/ASOA20120220021H), Feb 20, 2012: UNKNOWN. ODOR. THE CREW REPORTED THAT AFTER LANDING, THERE WAS A BURNING ODOR IN THE CABIN AND COCKPIT. MAINTENANCE INSPECTED THE AIRCRAFT AND WERE UNABLE TO DETECT ANY BURNIN - [SDR C2XA11TY087](https://openairdocs.org/sdr/C2XA11TY087), Jun 14, 2011: SKIN. DAMAGED. TYS - A/C WAS EN ROUTE FROM PVD TO IAD WHEN A BIRD STRIKE TO THE LEFT AVIONICS BAY. MAINTENANCE PERFORMED A GVI INSPECTION TYO THE LT AVIONIC AREA AND AVIOIC RA - [SDR C2XA11CL115](https://openairdocs.org/sdr/C2XA11CL115), May 3, 2011: DAU. FAULTY. EWR FLT 2476 THE CREW REPORTED A DAU 2 FAIL MESSAGE IN FLIGHT. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED TH - [SDR C2XA10SH430](https://openairdocs.org/sdr/C2XA10SH430), Dec 19, 2010: HINGE FITTING. WORN. SHV - DURING C-CHECK RT AILERON O/B HINGE POINT I/B BUSHING MIGRATED. MAINTENANCE REPAIRED RT AILERON O/B HINGE POINT I/B HAT BUSHING IAW EC5740-01152 REV B. TH - [SDR C2XA10SH429](https://openairdocs.org/sdr/C2XA10SH429), Dec 14, 2010: WINDOW FRAME. CORRODED. SHV - DURING C-CHECK FASTENER HOLE ON LT COCKPIT WINDSHIELD FRAME BOTTOM LT CORNER HAS CORROSION. MAINTENANCE PERFORMED REPAIR ON LT WINDSHIELD BOTTOM LT CORNER - [SDR C2XA10IA166](https://openairdocs.org/sdr/C2XA10IA166), May 29, 2010: HOSE. CLOGGED. IAH - FLIGHT 2203, THE CREW REPORTED SMOKE ODOR IN THE FRONT OF THE CABIN IN FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND R - [SDR C2XA10TY061](https://openairdocs.org/sdr/C2XA10TY061), Apr 17, 2010: LIGHT. DEFECTIVE. TYS - A/C WAS TAXIING FROM THE GATE WHEN CREW SMELL SMOKE IN THE CABIN AND RETURNED BACK TO THE GATE. MAINTENANCE REMOVED THE SIDEWALL PANEL AT SEAT 8A AND PLAC - [SDR C2XA10IA092](https://openairdocs.org/sdr/C2XA10IA092), Mar 10, 2010: LIGHT. INOPERATIVE. IAH - DURING MAINTENANCE INSPECTION THE LEFT FORWARD OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LI - [SDR C2XA09CL137](https://openairdocs.org/sdr/C2XA09CL137), Oct 18, 2009: POWER SUPPLY. DISCHARGED. DURING ROUTINE MAINTENANCE THE AFT EMERGENCY AISLE PATH LIGHT STRIP WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 4 EMERGENCY LIGHT POWER SUP - [SDR C2XA09CL072](https://openairdocs.org/sdr/C2XA09CL072), May 21, 2009: TURBINE WHEEL. CRACKED. DURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 2 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASO - [SDR C2XA09RI080](https://openairdocs.org/sdr/C2XA09RI080), Apr 27, 2009: LIGHT. INOPERATIVE. RIC - DURING ROUTINE MAINTENANCE, RIC MX FOUND SEAT 12C OVERHEAD EMERGENCY LIGHT INOPERATIVE. MX REMOVED AND REPLACED LIGHT BULB AND PERFORMED OPERATIONAL CHECK - [SDR C2XA09IA037](https://openairdocs.org/sdr/C2XA09IA037), Feb 6, 2009: INVERTER. INOPERATIVE. MCI - DURING MX INSPECTION THE LT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MX R&R THE NR 4 EMERGENCY LIGHT INVERTER, OPS TESTED WITH NO DEFECT - [SDR C2XA09IA013](https://openairdocs.org/sdr/C2XA09IA013), Jan 8, 2009: BALLAST. FAULTY. DURING PREFLIGHT INSP, CREW REPORTED A BURNED SMELL IN THE CABIN AROUND ROWS 5 AND 6. MX INSPECTED THE ACFT, AND R&R (2) LIGHT BALLASTS, OPS TESTED WITH NO DEFE - [SDR C2XA09SH002](https://openairdocs.org/sdr/C2XA09SH002), Jan 5, 2009: STRUCTURE. CORRODED. DURING C-CHECK. CORROSION AROUND RIVETS ON RT HORZ STAB L/E. REPAIRED RT HORZ STAB L/E IAW EC5510-01196. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09SH001](https://openairdocs.org/sdr/C2XA09SH001), Jan 5, 2009: SKIN. CORRODED. DURING C-CHECK, CORROSION AROUND RIVETS ON LT HORZ STAB L/E. REPAIRED LT HOR. STAB L/E IAW EC5510-01196. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA08RI158](https://openairdocs.org/sdr/C2XA08RI158), Oct 18, 2008: BULB. BURNED OUT. RIC MX DURING ROUTINE MX, FOUND LT OVER WING EMERGENCY LIGHT TO BE INOPERATIVE. MX R&R EMERGENCY BULB AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED FO - [SDR C2X2008F00042](https://openairdocs.org/sdr/C2X2008F00042), Aug 30, 2008: LIGHT. INOPERATIVE. DURING PREFLIGHT INSPECTION, THE CREW REPORTED (2) EMERGENCY LIGHT STRIPS TO BE INOPERATIVE. MAINT REMOVED AND REPLACED THE AFFECTED LIGHT STRIPS, OPERATIONALLY - [SDR C2X2008F00003](https://openairdocs.org/sdr/C2X2008F00003), Jun 28, 2008: INVERTER. INOPERATIVE. FWD EMERGENCY PROX LIGHT STRIP INOPERATIVE. REMOVED AND REPLACED NR 2 EMERGENCY LIGHT INVERTER IAW AMM 33-50-11. OPS CHECK GOOD. (K) - [SDR C2XA08XL069](https://openairdocs.org/sdr/C2XA08XL069), Jun 12, 2008: WIRE. LOOSE. CLE FLIGHT 3060, THE CREW REPORTED THE FORWARD EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPAIRED WIRE TO SERVICE DOOR EMERGENCY LIGHT. OPERATI - [SDR C2XA08CL069](https://openairdocs.org/sdr/C2XA08CL069), Jun 12, 2008: WIRE. LOOSE. CLE FLIGHT 3060. THE CREW REPORTED THE FORWARD EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPAIRED WIRE TO SERVICE DOOR EMERGENCY LIGHT. OPERATI - [SDR C2XA08RI064](https://openairdocs.org/sdr/C2XA08RI064), May 9, 2008: LIGHT. INOPERATIVE. FLIGHT 3098 - EWR - FLIGHT CREW REPORTED BAG SMOKE DETECT TEST LIGHT WAS INOPERATIVE. EWR MX RESET THE SYSTEM AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRC - [SDR C2XA08IA114](https://openairdocs.org/sdr/C2XA08IA114), Apr 17, 2008: PROXIMITY SWITCH. INOPERATIVE. IAH - FLIGHT 2643, THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE ON TAKEOFF. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENAN - [SDR C2XA08IA113](https://openairdocs.org/sdr/C2XA08IA113), Apr 17, 2008: PROXIMITY SENSOR. INOPERATIVE. IAH - FLIGHT 2264, AFTER LANDING THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE ON EICAS. MAINTENANCE REMOVED AND REPLACED THE LEFT SHOCK ABSORBER PRO - [SDR C2XA08IA112](https://openairdocs.org/sdr/C2XA08IA112), Apr 16, 2008: ELECTRONIC UNIT. INOPERATIVE. IAH - FLIGHT 2037, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED - [SDR C2XA08IA075](https://openairdocs.org/sdr/C2XA08IA075), Mar 6, 2008: LIGHT. MALFUNCTIONED. IAH - FLIGHT 3019, DURING PREFLIGHT INSPECTION THE CREW REPORTED AN EMERGENCY EXIT LIGHT INOP. MAINTENANCE INSPECTED THE AIRCRAFT, RESET THE EMERGENCY LIGHTS, O - [SDR C2XA07CL094](https://openairdocs.org/sdr/C2XA07CL094), Nov 6, 2007: LIGHT. INOPERATIVE. CLE FLIGHT 2038 THE CREW REPORTED THE EMERGENCY EXIT PATH LIGHTING STRIP WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED EMERGENCY LIGHT STRIP. OPERATIONAL - [SDR C2XA07RI090](https://openairdocs.org/sdr/C2XA07RI090), Oct 15, 2007: LIGHT. INOPERATIVE. FLT 2216 - EWR - CREW REPORTED EMERGENCY EXIT LIGHT BY MAIN CABIN DOOR INOPERATIVE. EWR MX PERFORMED OPERATIONAL TEST SUCCESSFULLY AND NO FAULT FOUND. ACFT WAS - [SDR C2XA07TY009](https://openairdocs.org/sdr/C2XA07TY009), Mar 4, 2007: PROXIMITY SWITCH. OUT OF ADJUST. JAX-CLE FLT NR 2050- LANDING GEAR/AIR GROUND FAIL MESSAGE ANNUNCIATED DURING FLIGHT. DIVERTED TO TYS WITHOUT INCIDENT. THE LT MLG TRAILING ARM PROX SWITCH WAS A - [SDR C2XA07CL027](https://openairdocs.org/sdr/C2XA07CL027), Mar 2, 2007: WARNING HORN. FAULTY. CLE FLIGHT NR 2485 THE CREW REPORTED DESCENDING THRU 25000 FEET THEY HAD A AUDIBLE LANDING GEAR WARNING UNTIL LANDING GEAR WAS DOWN AND LOCKED. MAINTENANCE INSP - [SDR C2XA07IA033](https://openairdocs.org/sdr/C2XA07IA033), Feb 11, 2007: SIGN. LOOSE. IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHT AT THE FLIGHT ATTENDANT STATION WAS INOPERATIVE. MAINTENANCE RESET THE CONNECTOR O - [SDR C2XA06CL064](https://openairdocs.org/sdr/C2XA06CL064), Jun 28, 2006: TERMINAL BLOCK. MELTED. CLE FLIGHT 3094 THE CREW REPORTED THE CAPTAINS WINDSHIELD EMITTED A SMALL AMOUNT OF SMOKE WHEN THE HEAT WAS TURNED ON. MAINTENANCE INSPECTED AND FOUND THE -P- T - [SDR C2XA05SH026](https://openairdocs.org/sdr/C2XA05SH026), Apr 21, 2005: SKIN. DENTED. SHV - DURING C-CHECK, LT SIDE EXTERNAL FUSELAGE HAS A DENT BETWEEN FR 7 & 8 JUST AFT OF GPU CONNECTION. MAINTENANCE REPAIRED LEFT SIDE EXTERNAL FUSELAGE DENT BE - [SDR C2XA05SH025](https://openairdocs.org/sdr/C2XA05SH025), Apr 15, 2005: RIB. CRACKED. SHV - DURING C-CHECK, THE LT WINGS NR 1 FLAP TORQUE BOX HAS CRACK INDICATION ON FASTENERS O/B FWD AND AFT. MAINTENANCE OVERSIZED LT TORQUE BOX NR 1 O/B HOLE FWD - [SDR C2XA04BT068](https://openairdocs.org/sdr/C2XA04BT068), Jun 22, 2004: LEVER. FAULTY. CREW REPORTED, LANDING GEAR WOULD NOT RETRACT. AIR RETURNED TO NEWARK. MAINTENANCE TROUBLESHOT LANDING GEAR SYSTEM, SWUNG LANDING GEAR SEVERAL TIMES, SERVICED N - [SDR C2XA04BT027](https://openairdocs.org/sdr/C2XA04BT027), Mar 2, 2004: PROXIMITY SWITCH. FAULTY. CREW REPORTED, EXPERIENCED SEVERAL UNUSUAL THUMPS WHILE INFLIGHT. NOISES SEEM TO BE COMING FROM THE NOSE OF THE AIRCRAFT. MAINTENANCE TROUBLESHOT AND FOUND RIGH - [SDR C2XA03CL200](https://openairdocs.org/sdr/C2XA03CL200), Dec 15, 2003: APU. FAILED. EWR FLIGHT 2526 THE CREW REPORTED SMOKE IN THE COCKPIT AND CABIN AFTER PUSHBACK. MAINTENANCE INSPECTED AND REPLACED THE APU. THE APU WAS SEIZED AND CAUSED BURNI - [SDR C2XA03BT103](https://openairdocs.org/sdr/C2XA03BT103), Oct 24, 2003: BALLAST. DEFECTIVE. CREW REPORTED ON TAXI, ELECTRICAL BURNING SMELL IN (THE VICINITY OF) ROW FOUR IN THE CABIN. MAINTENANCE REMOVED AND REPLACED LIGHT BALLAST AND WIRING FOR SEAT 4 - [SDR C2XA03CL169](https://openairdocs.org/sdr/C2XA03CL169), Sep 18, 2003: ANTENNA. FAULTY. CLE FLIGHT NR 2068 THE CREW REPORTED A LANDING GEAR WARNING AT 10,000 FT. MAINTENANCE INSPECTED AND REPLACED BOTH NR 2 RADIO ALTIMETER ANTENNAS. OPERATIONAL CHE - [SDR C2XA03TY139](https://openairdocs.org/sdr/C2XA03TY139), Aug 24, 2003: HOUSING. CORRODED. TYS DURING A SCHEDULED INSPECTION THE HORIZONTAL SATB SPHERICAL BEARING HOUSING WAS FOUND TO BE WORN AND PITTED. MAINTENANCE ACCOMPLISHED A BLEND-OUT AND REAM R All 73: https://openairdocs.org/deregistered/N13956-2015-12-10/reports.md ## Other aircraft with N13956 - [Cancelled 1990-09-25](https://openairdocs.org/deregistered/N13956-1990-09-25): Piper PA-23-250, S/N 274571. N-number assigned, not yet registered --- 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.