# N17115: 2002 Embraer EMB-145XR, registration cancelled 2026-09-23 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 23, 2026 - Status when cancelled: Sale reported - Airframe: [Embraer EMB-145XR](https://openairdocs.org/model/embraer-emb-145xr) (registry code 3260214) - Engine: [Rolls-Royce AE3007 series](https://openairdocs.org/engine/rolls-royce-ae3007-series) (registry code 54582) - Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (OpenAirDocs) - Serial number: 145666 - Year built: 2002 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: February 25, 2005 - Last registry action: June 17, 2026 - Mode S code: A11F7D - Location: [Kingman, AZ](https://openairdocs.org/faa-place/AZ/Kingman) - Owner type: Individual - Owner's area on the map: 35.0799° N, 113.7486° W: Placed by OpenAirDocs at the center of ZIP code 86401, within about 20 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N17115 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=17115 - Page: https://openairdocs.org/deregistered/N17115-2026-09-23 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-145XR: https://openairdocs.org/model/embraer-emb-145xr.md ## Service difficulty reports (58, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASOA2019080795091](https://openairdocs.org/sdr/ASOA2019080795091), Jul 29, 2019: BATTERY PACK. INOPERATIVE. DURING MX THE WING EMERGENCY LIGHTS AND REAR CEILING SIGN WAS DISCOVERED INOP. MX RESECURED PINS AT PLUG J8031 AND REMOVED AND REPLACED BATTERY PACK #3 WITH OPE - [SDR ASOA2019041955057](https://openairdocs.org/sdr/ASOA2019041955057), Apr 5, 2019: DOOR. CRACKED. DURING MX INSPECTION THE BAGGAGE DOOR WAS FOUND TO HAVE A GOUGE 1/2" IN LENGTH. MX REPAIRED GOUGE ON DOOR IAW EMB145 SRM 52-30-01. - [SDR ASOA201805187085](https://openairdocs.org/sdr/ASOA201805187085), May 18, 2018: BATTERY. DISCHARGED. TYS A/C WAS IN FOR A SERVICE CHECK WHEN THEY FOUND EMERGENCY MAIN DOOR LIGHT AND MAIN DOOR EXTERIOR LIGHT INOP. MAINTENANCE RE-LAMPED THE MAIN DOOR EXTERIOR LIG - [SDR ASOA201710055117](https://openairdocs.org/sdr/ASOA201710055117), Oct 5, 2017: CHARGER. INOPERATIVE. DURING INSPECTION, THE MAIN CABIN DOOR EMERGENCY LIGHT WAS DISCOVERED INOPERATIVE. REMOVED AND REPLACED THE BATTERY CHARGER, OPS CHECKED GOOD. ACFT WAS APPROVED - [SDR ASOA20160926050R](https://openairdocs.org/sdr/ASOA20160926050R), Sep 26, 2016: SWITCH. STUCK. CREW REPORTED NOSE UP PITCH TRIM(UNCOMMANDED) RIGHT AFTER TAKEOFF. POSSIBLE PITCH TRIM RUNAWAY. AURAL WARNING"TRIM, TRIM" BUT NO EICASE MESSAGE. SMOOTH LANDING - [SDR ASOA20160718064](https://openairdocs.org/sdr/ASOA20160718064), Jul 18, 2016: SMOKE DETECTOR. DEFECTIVE. IAH - FLIGHT 4438, THE CREW REPORTED A LAV SMOKE INDICATION ON SHORT FINAL. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT - [SDR ASOA20160427039](https://openairdocs.org/sdr/ASOA20160427039), Apr 27, 2016: POWER SUPPLY. INOPERATIVE. DURING MAINTENANCE INSPECTION THE LT AND RT OVERWING AND EMERGENCY EXIT AISLE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 3 EMERGENC - [SDR ASOA20160427038](https://openairdocs.org/sdr/ASOA20160427038), Apr 27, 2016: BATTERY PACK. DISCHARGED. DURING MAINTENANCE INSPECTION THE LT AND RT OVERWING AND EMERGENCY EXIT AISLE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 3 EMERGENC - [SDR ASOA20150421037](https://openairdocs.org/sdr/ASOA20150421037), Apr 21, 2015: BULB. INOPERATIVE. DURING 3A INSPECTION THE EMERGENCY EXIT LIGHT ON THE SERVICE DOOR LOWER WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE AFFECTED LIGHT BULB, OPERATIONALLY TE - [SDR ASOA20141114336](https://openairdocs.org/sdr/ASOA20141114336), Nov 14, 2014: SKIN. CORRODED. DURING C-CHECK CARGO DOOR UPPER INTERNAL SKIN CORRODED AT NUTPLATE. MAINTENANCE PERFORMED REPAIR ON CARGO DOOR UPPER INTERNAL SKIN IAW EC5230-01349. THE ACFT WA - [SDR ASOA20141114335](https://openairdocs.org/sdr/ASOA20141114335), Nov 14, 2014: DOOR FRAME. CORRODED. DURING C-CHECK CARGO DOOR FWD FRAME CORRODED. MAINTENANCE PERFORMED REPAIR ON CARGO DOOR FWD FRAME IAW SRM 51-40-02 AND EC5230-01349. THE ACFT WAS APPROVED FOR - [SDR ASOA20141114334V](https://openairdocs.org/sdr/ASOA20141114334V), Nov 14, 2014: DOOR FRAME. CORRODED. DURING C-CHECK, CARGO DOOR AFT FRAME CORRODED, LOCAL LEVEL 2 AT NUTPLATE. MAINTENANCE PERFORMED REPAIR OF CARGO DOOR AFT FRAME AT NUTPLATE IAW EC5230-01349 UP T - [SDR ASOA20141114333](https://openairdocs.org/sdr/ASOA20141114333), Nov 14, 2014: FRAME. CRACKED. DURING C-CHECK, CRACK AT RIVET FRAME 10 UNDER RT DV WINDOW CUTOUT. MAINTENANCE R & R FRAME 10 UNDER RT DV WINDOW CUTOUT IAW SRM 51-40-02. THE ACFT WAS APPROVED - [SDR ASOA20141114332V](https://openairdocs.org/sdr/ASOA20141114332V), Nov 14, 2014: FLOOR SUPPORT. CORRODED. DURING C-CHECK, RT OMEGA BEAM IS CORRODED, LOCAL LEVEL 2 AT FASTENER HOLE AT FRAME 23. MAINTENANCE PERFORMED REPAIR OF RT OMEGA BEAM AT FRAME 23 IAW SRM 53-21-1 - [SDR ASOA20141114331](https://openairdocs.org/sdr/ASOA20141114331), Nov 14, 2014: SHEAR TIE. DAMAGED. DURING C-CHECK SHEAR TIE AT FRAME 19, STRINGER 14L IS MISSING RIVETS. MAINTENANCE INSTALLED 2 RIVETS IN SHEAR CLIP AT FRAME 19, STRINGER 14L IAW SRM 51-40-02. T - [SDR ASOA20141114330](https://openairdocs.org/sdr/ASOA20141114330), Nov 14, 2014: SUPPORT. CORRODED. DURING C-CHECK, GALLEY FWD DIGITAL BUTTSTRAP IS CORRODED, AT VARIOUS FASTENER HOLES. MAINTENANCE PERFORMED REPAIR OF GALLEY FWD DIGITAL LT IAW EC5320-01987. THE - [SDR ASOA20141110327](https://openairdocs.org/sdr/ASOA20141110327), Nov 10, 2014: BRACKET. DAMAGED. DURING C-CHECK CARGO DOOR LOWER FRAME BRACKET DAMAGED. MAINTENANCE R & R CARGO DOOR LOWER FRAME "L" BRACKET IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN T - [SDR ASOA20141110326](https://openairdocs.org/sdr/ASOA20141110326), Nov 10, 2014: SKIN. GOUGED. DURING C-CHECK CARGO DOOR LOWER INTERNAL SKIN GOUGED. MAINTENANCE PERFORMED REPAIR ON CARGO DOOR LOWER INTERNAL SKIN IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR - [SDR ASOA20140410034](https://openairdocs.org/sdr/ASOA20140410034), Apr 10, 2014: LIGHT. INOPERATIVE. DURING ROUTINE MAINTENANCE, THE LT AFT EXTERNAL EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSY, OPS CHECKED GOOD. - [SDR ASOA20131119202](https://openairdocs.org/sdr/ASOA20131119202), Nov 19, 2013: BULB. LOOSE. DURING SCHEDULED MAINTENANCE THE PASSENGER DOOR LOWER EMERGENCY EXIT LIGHT FAILED TO ILLUMINATE WHEN TESTED. MAINTENANCE RESECURED THE BULB IN THE LIGHT FIXTURE - [SDR ASOA20130702070](https://openairdocs.org/sdr/ASOA20130702070), Jul 2, 2013: WARNING MESSAGE. ILLUMINATED. PILOT REPORTED A BRAKE DEGRADED EICAS MESSAGE AFTER SELECTING GEAR DOWN AND THE RT BRAKE WAS LESS EFFECTIVE ON LANDING ROLL. CREW RESET SYS WITH MX CONTROL. MES - [SDR ASOA20121217118](https://openairdocs.org/sdr/ASOA20121217118), Dec 17, 2012: CHARGER. INOPERATIVE. DURING MX INSPECTION, THE AFT AISLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX R & R THE NR 3 EMERGENCY LIGHT BATTERY CHARGER WITH OPS CHECK SUCCESSFUL. ACFT WAS - [SDR ASOA20120410038C](https://openairdocs.org/sdr/ASOA20120410038C), Apr 10, 2012: CONNECTOR. LOOSE. DURING ROUTINE MX, EMERGENCY EXIT SIGN AT RT OVERWING EXIT DOOR WAS FOUND INOPERATIVE. MX RESECURED LOOSE CONNECTION AT THE EXIT MARKER. OPS CHECKED GOOD. - [SDR ASOA2011TY005](https://openairdocs.org/sdr/ASOA2011TY005), Nov 18, 2011: WARNING SYSTEM. FALSE INDICATION. REJECTED TAKEOFF. THE TAKEOFF CONFIGURATION FLAPS AURAL WARNING MESSAGE CAME ON. CREW RESET AND PERFORMED OPS CHECK OF FLAPS AND TRIM SYSTEMS WERE ALL GOOD. ACF - [SDR C2XA11IA253](https://openairdocs.org/sdr/C2XA11IA253), Nov 7, 2011: PROBE. MALFUNCTIONED. FLIGHT 4455 THE CREW REPORTED A FUEL TANK NR 2 FUEL LEVEL ERROR IN FLIGHT, FUEL FLUCTUATING BETWEEN 4100LBS CAUSING IMBALANCE. THE AIRCRAFT RETURNED TO IAH WHER - [SDR C2XA11IA086](https://openairdocs.org/sdr/C2XA11IA086), May 7, 2011: LIGHT. OVERHEATED. FLIGHT 2532, THE CREW REPORTED A BURNING ODOR AT ROW 4A. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE - [SDR C2XA11CL089](https://openairdocs.org/sdr/C2XA11CL089), Apr 3, 2011: BUTTON. FAULTY. EWR - FLT 2370 THE CREW REPORTED THE NR 2 BLEED VALVE CLOSED AFTER TAKEOFF AND WAS UNABLE TO CLEAR THE MESSAGE. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOU - [SDR C2XA11IA009](https://openairdocs.org/sdr/C2XA11IA009), Jan 7, 2011: BLEED VALVE. LOCKED. IAH - FLIGHT 3004, THE CREW REPORTED A BLEED VALVE TWO FAIL. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT A - [SDR C2XA10CL129](https://openairdocs.org/sdr/C2XA10CL129), Aug 8, 2010: WARNING SYSTEM. ACTIVATED. CLE FLT 2777 THE CREW REPORTED A ENGINE 2 ANTI-ICE FAIL MESSAGE ON THE EICAS DURING CLIMBOUT. MAINTENANCE INSPECTED AND RELEASED THE AIRCRAFT IAW MEL 30-21-01-1 - [SDR C2XA10IA076](https://openairdocs.org/sdr/C2XA10IA076), Feb 22, 2010: ACCUMULATOR. DISCHARGED. IAH - FLIGHT 2412, THE CREW REPORTED THAT THE LANDING GEAR TOOK LONGER THAN NORMAL TO RETRACT, AND RECEIVED A LANDING GEAR LEVER DISAGREE MESSAGE ON EICAS. THE - [SDR C2XA09IA316](https://openairdocs.org/sdr/C2XA09IA316), Dec 15, 2009: CONTROL LEVER. DEFECTIVE. IAH - FLIGHT 2198, THE CREW REPORTED THAT THE MLG DID NOT INITIALLY RETRACT, AFTER QRH RECYCLED GEAR AND RETRACTED NORMALLY. THE AIRCRAFT LANDED AT IAH WITHOUT - [SDR C2XA09IA301](https://openairdocs.org/sdr/C2XA09IA301), Dec 3, 2009: PROXIMITY SENSOR. INOPERATIVE. IAH - FLIGHT 2272, THE CREW REPORTED A LANDING GEAR LEVER DISAGREE MESSAGE AND THE GEAR FAILED TO RETRACT ON TAKEOFF, AND FINALLY RETRACTED AFTER SEVERAL ATTEMP - [SDR C2XA09IA300](https://openairdocs.org/sdr/C2XA09IA300), Dec 1, 2009: CONTROL LEVER. MALFUNCTIONED. IAH - FLIGHT 2135, DURING CLIMB THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT ON TAKE OFF. THE CREW PERFORMED THE QRH, CYCLED THE GEAR WHICH THEN RE - [SDR C2XA09IA299](https://openairdocs.org/sdr/C2XA09IA299), Nov 29, 2009: ELECTRONIC UNIT. MALFUNCTIONED. IAH - FLIGHT 2953, ON CLIMBOUT THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE CREW FOLLOWED THE QRH, CYCLED THE GEAR AND THE GEAR RETRACTED. THE - [SDR C2XA09CL154](https://openairdocs.org/sdr/C2XA09CL154), Nov 24, 2009: ACTUATOR. FAULTY. CLE FLT 2781 THE CREW REPORTED AN AIR/GROUND FAIL MESSAGE WHILE GEAR WAS IN TRANSIT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT NOSE GEAR DOOR ACTUATOR. OPERA - [SDR C2XA09RI196](https://openairdocs.org/sdr/C2XA09RI196), Nov 18, 2009: CONTROL LEVER. INOPERATIVE. FLIGHT 2508 - EWR - FLIGHT CREW REPORTED L/G AND AIR/GRND DISAGREE MESSAGE ON EICAS. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND - [SDR C2XA09RI195](https://openairdocs.org/sdr/C2XA09RI195), Nov 18, 2009: ELECTRONIC UNIT. INOPERATIVE. FLIGHT 2508 - EWR - FLIGHT CREW REPORTED L/G AND AIR/GRND DISAGREE MESSAGE ON EICAS. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND - [SDR C2XA09IA262](https://openairdocs.org/sdr/C2XA09IA262), Oct 16, 2009: WARNING SYSTEM. MALFUNCTIONED. IAH - FLIGHT 2771, THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE ON APPROACH. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED - [SDR C2XA09IA227](https://openairdocs.org/sdr/C2XA09IA227), Sep 9, 2009: THERMOSTAT. MALFUNCTIONED. ATL - FLIGHT 3128 - THE CREW REPORTED AN ELECTRIC BURNING SMELL IN THE COCKPIT AND FORWARD CABIN DURING CRUISE, WITH A BLEED TWO OVERHEAT WARNING ON EICAS. THE - [SDR C2XA09IA226](https://openairdocs.org/sdr/C2XA09IA226), Sep 9, 2009: THERMOSTAT. FAULTY. ATL - FLIGHT 3128 - THE CREW REPORTED AN ELECTRIC BURNING SMELL IN THE COCKPIT AND FORWARD CABIN DURING CRUISE, WITH A BLEED TWO OVERHEAT WARNING ON EICAS. THE - [SDR C2XA09IA214](https://openairdocs.org/sdr/C2XA09IA214), Aug 25, 2009: SKIN. CORRODED. IAH - FLIGHT 2140, DURING POST FLIGHT INSPECTION THE CREW REPORTED A PIECE OF THE LT WING LEADING EDGE TWO TO BE CORRODED AND MISSING. IAH MAINTENANCE INSPECTED - [SDR C2XA09TY124](https://openairdocs.org/sdr/C2XA09TY124), Jun 23, 2009: BUSHING. MIGRATED. DURING C-CHECK, A MIGRATED HAT BUSHING WAS FOUND ON THE LT AILERON OTBD PCA FITTING INBD LUG. THE AILERON PCA BRACKET WAS REMOVED AND REPLACED IAW EC 5750-01177 - [SDR C2XA09TY122](https://openairdocs.org/sdr/C2XA09TY122), Jun 21, 2009: FUEL TANK. CHAFED. TYS - DURING C-CHECK THE VENTRAL TANK WAS FOUND CHAFED FROM CONTACT WITH PANEL 197BB. THE VENTRAL TANK WAS REPAIRED IAW EC 2810-01053. A/C STILL IN C-CHECK. - [SDR C2XA09TY118](https://openairdocs.org/sdr/C2XA09TY118), Jun 18, 2009: SKIN. DENTED. THE LT CENTER FUSELAGE I SKIN HAS TWO DENTS, ONE BETWEEN FRM 20 & 21 AND A PREVIOUSLY BLENDED AREA BETWEEN FRM 18 & 19 WITH A REMAINING THICKNESS OF .014 INCH. - [SDR C2XA09TY117](https://openairdocs.org/sdr/C2XA09TY117), Jun 18, 2009: SKIN. DAMAGED. THE RT REAR FUSELAGE I SKIN HAS A DENT WITH A GOUGE BETWEEN FRM 65 & 66, STR 14 & 15R. MAX DEPTH OF DENT AND GOUGE IS .034 INCH. CUT OUT GOUGED AREA OF SKIN, FA - [SDR C2XA07SH102](https://openairdocs.org/sdr/C2XA07SH102), Dec 5, 2007: ATTACH FITTING. DAMAGED. SHV - DURING C-CHECK RIGHT AILERON PCA HAS PLAY WHEN HYD ARE PRESSURIZED. MAINTENANCE REMOVED AND REPLACED RIGHT AILERON PCA FITTING AND PAINTED IAW EC5750-0117 - [SDR C2XA07SH100](https://openairdocs.org/sdr/C2XA07SH100), Dec 5, 2007: AXLE. CORRODED. SHV - DURING C-CHECK LT MLG STRUT LOWER ATTACH AXLE CORRODED. MAINTENANCE REMOVED AND REPLACED LT MLG STRUT LOWER ATTACH AXLE IAW EMB 145XR AMM 32-10-02. THE AI - [SDR C2XA07SH101](https://openairdocs.org/sdr/C2XA07SH101), Dec 5, 2007: AXLE. CORRODED. SHV - DURING C-CHECK RT MLG SHOCK STRUT LOWER ATTACH AXLE CORRODED. MAINTENANCE REMOVED AND REPLACED RT MLG SHOCK STRUT LOWER ATTACH AXLE IAW EMB AMM 32-10-02. - [SDR C2XA07SH099](https://openairdocs.org/sdr/C2XA07SH099), Dec 5, 2007: BEAM. CORRODED. SHV - DURING C-CHECK BAGGAGE DOOR CUTOUT LOWER CENTER BEAM HAS CORROSION. MAINTENANCE REMOVED AND REPLACED LOWER BEAM FOR BAGGAGE DOOR CUTOUT IAW EMB 145 SRM 51 - [SDR C2XA07SH098](https://openairdocs.org/sdr/C2XA07SH098), Dec 5, 2007: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LEFT OMEGA BEAM HAS CORROSION BETWEEN FR 19-21. MAINTENANCE REPAIRED LEFT OMEGA BEAM BETWEEN FRS 19-21 IAW EC 5320-01229. THE AIRCRAFT WAS All 58: https://openairdocs.org/deregistered/N17115-2026-09-23/reports.md ## Other aircraft with N17115 - [Cancelled 1991-01-30](https://openairdocs.org/deregistered/N17115-1991-01-30): Grumman E-2C, S/N 160415. Administratively canceled. Owner: [US Customs Service](https://openairdocs.org/faa-owner/US%20CUSTOMS%20SERVICE), [Washington, DC](https://openairdocs.org/faa-place/DC/Washington) --- 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.