# N17108: 2002 Embraer EMB-145XR, registration cancelled 2026-07-28 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 28, 2026 - Exported to: Chad - Status when cancelled: Valid registration - 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: 145655 - Year built: 2002 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: February 25, 2005 - Certificate issued: June 30, 2025 - Last registry action: June 30, 2025 - Mode S code: A11F5D - 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/N17108 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=17108 - Page: https://openairdocs.org/deregistered/N17108-2026-07-28 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-145XR: https://openairdocs.org/model/embraer-emb-145xr.md ## Service difficulty reports (56, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASOA201812313080](https://openairdocs.org/sdr/ASOA201812313080), Dec 21, 2018: COFFEEMAKER. FAULTY. THE CREW REPORTED STRONG ELECTRICAL SMELL IN GALLEY. MAINTENANCE INSPECTED AND REPLACED BOTH GALLEY COFFEE MAKERS. - [SDR ASOA201812024069](https://openairdocs.org/sdr/ASOA201812024069), Dec 2, 2018: BULB. INOPERATIVE. IAH - FLIGHT 4035, THE CREW REPORTED THAT THE REAR OVERHEAD EMERGENCY LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, OPER - [SDR ASOA2018091944048](https://openairdocs.org/sdr/ASOA2018091944048), Sep 14, 2018: COFFEEMAKER. FAULTY. IAH - FLIGHT 4340, THE FLIGHT ATTENDANT REPORTED A BIT OF SMOKE OR SOME KIND OF BURNING WHEN NR 1 COFFEE POT SELECTED ON. MAINTENANCE REMOVED AND REPLACED THE N - [SDR ASOA201706265091](https://openairdocs.org/sdr/ASOA201706265091), Jun 26, 2017: STRIP. MISSING. DURING MX INSPECTION TWO EMERGENCY EXIT FLOOR PROXIMITY STRIPS WERE FOUND MISSING. MX INSTALLED FLOOR PROXIMITY TERMINATING STRIPS. A/C WAS APPROVED FOR RETURN - [SDR ASOA201704230076V](https://openairdocs.org/sdr/ASOA201704230076V), Apr 23, 2017: BEAM. CORRODED. SHV. DURING C-CK. CARGO DOOR LOWER BEAM CORRODED. REMOVED AND REPLACED CARGO DOOR LOWER BEAM IAW SRM 51-40-02. A/C WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20140729091](https://openairdocs.org/sdr/ASOA20140729091), Jul 28, 2014: RIB. CRACKED. LEFT WING RIB 7 CRACKED IN SEVERAL AREAS SURROUNDING THE REFUELING SHUTOFF VALVE AND DIFFUSER. CUT OUT THE CRACKED AREA. PERFORMED NDI OF CUTOUT SURROUND. FABRI - [SDR ASOA20140725090T](https://openairdocs.org/sdr/ASOA20140725090T), Jul 25, 2014: MOUNT. CRACKED. DURING C-CHECK, FOUND THE LT LOWER NR 1 ENGINE MOUNT CRACKED AND WAS VERIFIED BY VISUAL AND EDDY CURRENT MEANS. MAINTENANCE R & R THE NR 1 ENGINE YOKE IAW EC 54 - [SDR ASOA20140706093](https://openairdocs.org/sdr/ASOA20140706093), Jul 6, 2014: LIGHT. DISLODGED. DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE AFT CEILING EMERGENCY EXIT LIGHT WAS COMING OUT OF ITS CASING AND WAS NOT FULLY LIT. MAINTENANCE SECURRED - [SDR ASOA20130926175](https://openairdocs.org/sdr/ASOA20130926175), Sep 26, 2013: LIGHT. MALFUNCTIONED. DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT SIGNS WOULD NOT ILLUMINATE. THE SYS WAS RESET, AND THE LIGHTS OPERATED WITH NO DEFECTS NO - [SDR ASOA20130515069](https://openairdocs.org/sdr/ASOA20130515069), May 12, 2013: SKIN. CRACKED. DURING 4A INSPECTION THE RT AFT FUSELAGE II SKIN WAS FOUND TO HAVE A SINGLE CRACK EMINATING FROM A RIVET AT FR 78 STR 5R. MX REMOVED THE DAMAGE, AND PERFORMED A - [SDR ASOA20130512068](https://openairdocs.org/sdr/ASOA20130512068), May 12, 2013: SKIN. CRACKED. DURING 4A INSPECTION THE LT AFT FUSELAGE SKIN WAS FOUND TO HAVE THREE CRACKS EMINATING FROM A SINGLE RIVET NEAR FR 78 STRINGERS 4L & 5L. MX REMOVED THE DAMAGED - [SDR ASOA20130329046H](https://openairdocs.org/sdr/ASOA20130329046H), Mar 29, 2013: FLAPPER VALVE. LEAKING. THE CREW REPORTED FUEL LEAKING FROM THE LT WING. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT, R & R THE FLAPPER VALVE - [SDR ASOA20121231125](https://openairdocs.org/sdr/ASOA20121231125), Dec 31, 2012: SMOKE DETECTOR. FAULTY. CREW REPORTED A LAVATORY SMOKE INDICATION ON EICAS DURING DESCENT. MESSAGE CLEARED AFTER QRH PROCEDURE. R & R LAVATORY SMOKE DETECTOR, OPS CHECKED SUCCESSFUL. A - [SDR ASOA20120126014](https://openairdocs.org/sdr/ASOA20120126014), Jan 26, 2012: BATTERY. DISCHARGED. DURING MX INSPECTION, THE NR 2 EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MX R & R THE AFFECTED EMERGENCY LIGHT, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, A - [SDR ASOA20111119002](https://openairdocs.org/sdr/ASOA20111119002), Nov 19, 2011: BATTERY PACK. DISCHARGED. DURING ROUTINE MX THE RT AND LT FORWARD EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MX INSPECTED AND REPLACED THE NR 3 EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD. - [SDR C2XA11IA218](https://openairdocs.org/sdr/C2XA11IA218), Sep 6, 2011: WARNING SYSTEM. FALSE ACTIVATION. DEN - FLIGHT 5862 THE CREW REPORTED LANDING GEAR AURAL WARNING IN FLIGHT AT 13,000 FEET WITH NO OTHER INDICATIONS. THE AIRCRAFT LANDED AT DEN WITHOUT INCIDENT W - [SDR C2XA11SH113](https://openairdocs.org/sdr/C2XA11SH113), Aug 2, 2011: COMPUTER. DEFECTIVE. FLIGHT 2476 A/C N17108 FROM EWR AFTER TAKEOFF AND DURING CLIMB HAD SPS 1 INOP, AIR RETURNED TO EWR. MAINTENANCE REMOVED AND REPLACED STALL PROTECTION COMPUTER I - [SDR C2XA11TY058](https://openairdocs.org/sdr/C2XA11TY058), May 9, 2011: INVERTER. INOPERATIVE. RT EMERGENCY EXIT FWD EMERGENCY LIGHT INOP. REMOVED AND REPLACED NR 3 INVERTER IAW EMB 145AMM 33-50-01. OPS CHECK GOOD. - [SDR C2XA11RI037](https://openairdocs.org/sdr/C2XA11RI037), Mar 5, 2011: ANTI-ICE VALVE. INOPERATIVE. FLIGHT 2199 - BTV - FLIGHT CREW REPORTED WING ANTI-ICE FAIL ON EICAS. CREW DIVERTED TO BTV AND LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED LT WING ANTI-ICE - [SDR C2XA10TY162](https://openairdocs.org/sdr/C2XA10TY162), Oct 8, 2010: PANEL. CORRODED. CARGO DOOR LT SIDE PANEL HAS MULTIPLE CORRODED NUT PLATE HOLES. FOUND SIX DAMAGED HOLES, BLENDED MINOR CORROSION ON FOUR HOLES. TWO OF THE SIX HOLES WERE OUT OF - [SDR C2XA10TY160](https://openairdocs.org/sdr/C2XA10TY160), Oct 8, 2010: PROXIMITY SWITCH. OUT OF ADJUST. TYS - A/C WENT OUT ON A TEST FLIGHT AFTER COMPLETING A C-CHECK INSPECTION. THE CREW GOT A LDG AIR/GND FAIL MESSAGE ON THE EICAS AND RETURN BACK TO THE HANGAR WH - [SDR C2XA10TY157](https://openairdocs.org/sdr/C2XA10TY157), Sep 28, 2010: BUSHING. DAMAGED. TYS - A/C IS IN C-CHECK NOW. INSPECTION FOUND THE HORIZONTAL STAB RT INBOARD HINGE STATIONARY BUSHING PITTED. MAINTENANCE REMOVED AND REPLACED THE BUSHING IAW E - [SDR C2XA10CL150](https://openairdocs.org/sdr/C2XA10CL150), Sep 20, 2010: CABLE. OUT OF ADJUST. THE CREW REPORTED THE MAIN CABIN DOOR WAS VERY HARD TO OPEN. MAINTENANCE INSPECTED AND ADJUSTED THE MAIN CABIN DOOR CABLES. OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA10IA256](https://openairdocs.org/sdr/C2XA10IA256), Sep 17, 2010: BATTERY PACK. DISCHARGED. IAH - DURING POST FLIGHT INSPECTION THE CREW REPORTED THE OVERHEAD EMERGENCY EXIT LIGHT AT ROW 12A WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER - [SDR C2XA10IA252](https://openairdocs.org/sdr/C2XA10IA252), Sep 12, 2010: UNKNOWN. ODOR. IAH - FLIGHT 2194, THE CREW REPORTED A BURNING SMELL ORIGINATING FROM THE COFFEE POT AREA WITH BOTH POTS TURNED ON. MAINTENANCE INSPECTED BOTH COFFEEMAKERS & WI - [SDR C2XA10CL071](https://openairdocs.org/sdr/C2XA10CL071), May 12, 2010: ADC. FAULTY. MSP FLT 2816 THE CREW REPORTED, THE FIRST OFFICER'S AIRSPEED INDICATION IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 AIR DATA COMPUTER, OPERATIONAL CH - [SDR C2XA10RI056](https://openairdocs.org/sdr/C2XA10RI056), Apr 19, 2010: FIRE LOOP. FAILED. FLIGHT 2601 - EWR - FLIGHT CREW REPORTED E1 FIRE DETECTION FAIL AT 35000 FT, ALL OTHER INDICATION NORMAL. EWR MX REMOVED AND REPLACED E1 FIRE LOOP AND PERFORMED - [SDR C2XA09CL167](https://openairdocs.org/sdr/C2XA09CL167), Dec 22, 2009: INVERTER. FAULTY. CLE FLT 2095 THE CREW REPORTED THE EMERGENCY LIGHT AT THE FLIGHT ATTENDANT STATION DID NOT TEST. MAINTENANCE INSPECTED AND REPLACED THE FORWARD LIGHT INVERTER. - [SDR C2XA09RI162](https://openairdocs.org/sdr/C2XA09RI162), Sep 16, 2009: CONTROLLER. INOPERATIVE. FLIGHT 2447 - EWR - DURING LANDING, FLIGHT CREW REPORTED AUTO PRESSURIZATION FAIL. EWR MX REMOVED AND REPLACED DIGITAL AUTO PRESSURIZATION CONTROLLER AND PERFOR - [SDR C2XA09RI161](https://openairdocs.org/sdr/C2XA09RI161), Sep 16, 2009: CONTROLLER. INOPERATIVE. FLIGHT 2447 - EWR - DURING LANDING, FLIGHT CREW REPORTED AUTO PRESSURIZATION FAIL. EWR MX REMOVED AND REPLACED DIGITAL AUTO PRESSURIZATION CONTROLLER AND PERFOR - [SDR C2XA09IA066](https://openairdocs.org/sdr/C2XA09IA066), Feb 25, 2009: ELECTRONIC UNIT. MALFUNCTIONED. IAH - FLIGHT 3048, THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE ON CLIMB. THE AIRCRAFT RETURNED TO IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REP - [SDR C2XA09TY033](https://openairdocs.org/sdr/C2XA09TY033), Feb 22, 2009: BATTERY. DISCHARGED. EMERGENCY LIGHTS AT ROW 12 SIDEWALL PANELS & OVERHEAD PANEL INOP. REMOVED AND REPLACED NR 3 EMERGENCY LIGHT BATTERY IAW EMB 145XR AMM 33-50-04. OPS CHECK GOOD. - [SDR C2XA09IA034](https://openairdocs.org/sdr/C2XA09IA034), Feb 3, 2009: SIGN. INOPERATIVE. IAH - DURING MX INSPECTION THE RT LOWER EMERGENCY EXIT IDENTIFIER WAS FOUND TO BE INOPERATIVE. MX R&R THE AFFECTED EMERGENCY EXIT SIGN, OPS TESTED WITH NO DEFEC - [SDR C2XA09SH045](https://openairdocs.org/sdr/C2XA09SH045), Jan 25, 2009: FLOORBEAM. CORRODED. SHV DURING C-CHECK. LT OMEGA BEAM HAS CORROSION AT FR. 29. REPAIRED LT OMEGA BEAM AT FR. 29 IAW EMB 145 SRM 53-00-10. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09SH044](https://openairdocs.org/sdr/C2XA09SH044), Jan 25, 2009: FLOORBEAM. CORRODED. SHV DURING C-CHECK. LT OMEGA BEAM CORROSION BTW. FR. 23-24. REPAIRED LT OMEGA BEAM BTW FR. 23-24 IAW EMB 145 SRM 53-00-10. ACFT WAS APPROVED FOR RETURN TO SERVI - [SDR C2XA09SH041](https://openairdocs.org/sdr/C2XA09SH041), Jan 24, 2009: STRUCTURE. MISSING. SHV-DURING C-CHECK RT ELEVATOR TIP FAIRING AFT UPPER NUT PLATE MISSING. (DAMAGED RIVET HOLES) MX REPAIRED RT ELEVATOR TIP ATTACHMENT AT AFT O/B END UPPER AREA A - [SDR C2XA09SH043](https://openairdocs.org/sdr/C2XA09SH043), Jan 24, 2009: SKIN. CORRODED. SHV-DURING C-CHECK LT HORIZONTAL STAB L?E UPPER SURFACE HAS MULTIPLE RIVETS WITH CORROSION. MX REMOVED CORROSION IAW EC5510-01199 ORIG. THE ACFT WAS APPROVED FO - [SDR C2XA09SH042](https://openairdocs.org/sdr/C2XA09SH042), Jan 24, 2009: STRUCTURE. CORRODED. SHV-DURING C-CHECK RT HORIZONTAL STAB L/E UPPER SURFACE HAS MULTIPLE RIVETS WITH CORROSION. (MARKED) MX REMOVED CORROSION IAW EC5510-01199 ORIG. THE ACFT WAS AP - [SDR C2XA09SH040](https://openairdocs.org/sdr/C2XA09SH040), Jan 24, 2009: STRUCTURE. DAMAGED. SHV-DURING C-CHECK RT HORIZONTAL STAB L/E AT LOWER I/B CORNER HAS 1 TOOLING MARK. MX BLENDED OUT TOOLING MARKS IAW SRM 51-10-03 PER EC5510-01199 ORIG. THE ACFT - [SDR C2XA09SH013](https://openairdocs.org/sdr/C2XA09SH013), Jan 20, 2009: INTAKE. CORRODED. RT ENGINE AIR INTAKE HAS VARIOUS MOUNTING BOLT HOLES THAT ARE CORRODED. REPAIRED RT ENGINE AIR INTAKE MOUNT HOLES IAW EC5420-01158. ACFT WAS APPROVED TO RETURN - [SDR C2XA081A176](https://openairdocs.org/sdr/C2XA081A176), Jul 26, 2008: CONTROLLER. MALFUNCTIONED. IAH - FLIGHT 2259 - DURING CRUISE, THE CREW REPORTED THAT THE AIRCRAFT CABIN RATE OF CHANGE BECAME ERRATIC. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT - [SDR C2XA08RI073](https://openairdocs.org/sdr/C2XA08RI073), May 15, 2008: LAMP. INOPERATIVE. DURING ROUTINE MAINTENANCE, MX FOUND RIGHT HAND LOWER EMERGENCY LIGHT AT ESCAPE HATCH INOPERATIVE. MX REMOVED AND REPLACED EMERGENCY LIGHT IAW EMB AMM 33-50-13 - [SDR C2XA08IA109](https://openairdocs.org/sdr/C2XA08IA109), Apr 9, 2008: INVERTER. INOPERATIVE. IAH - FLIGHT 2832 DURING POST FLIGHT INSPECTION THE CREW REPORTED THE MID CABIN CEILING EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE - [SDR C2XA08TY038](https://openairdocs.org/sdr/C2XA08TY038), Mar 22, 2008: WIRE. BROKEN. EWR/CLT- FLT 3068 - UNCOMMANDED SPOILER INDICATION IN FLIGHT. CLT MX REPAIRED A BROKEN WIRE AT C/P P1167 PIN A. OPS CHECKS WERE GOOD IAW EMB 145 AMM 27-63-01. A - [SDR C2XA08TY029](https://openairdocs.org/sdr/C2XA08TY029), Feb 12, 2008: LIGHT. INOPERATIVE. TYS - DURING ROUTINE MX THE FWD CEILING EMERGENCY LIGHT WAS FOUND INOP. MX REMOVED AND REPLACED THE LAMPS IAW 145XR AMM 33-50-06 AND OPS CHECKED GOOD. A/C WAS R - [SDR C2XA08IA047](https://openairdocs.org/sdr/C2XA08IA047), Jan 19, 2008: WIRE. BROKEN. IAH - FLIGHT 2392, THE CREW REPORTED A SPOILER FAIL WITH A SPOILER OPEN INDICATION WITH THE SPOILERS CLOSED. THE CREW PERFORMED AN EMERGENCY DESCENT, AND LANDED - [SDR C2XA07CL104](https://openairdocs.org/sdr/C2XA07CL104), Dec 18, 2007: SIGN. MALFUNCTIONED. DURING ROUTINE MAINTENANCE, THE SMALL EMERGENCY EXIT SIGN ON THE RIGHT OVERWING EXIT WOULD NOT TEST. MAINTENANCE PERFORMED A ELECTRICAL RESET AND OPERATIONAL CH - [SDR C2XA07TY046](https://openairdocs.org/sdr/C2XA07TY046), Aug 29, 2007: BULB. INOPERATIVE. EMERGENCY LIGHT IN CEILING BY ROW 17A INOP. REPLACED LIGHT BULB IAW EMB 145 AMM 33-50-04, OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE. - [SDR C2XA07IA168](https://openairdocs.org/sdr/C2XA07IA168), Jul 18, 2007: LIGHT. INOPERATIVE. IAH - FLIGHT 2713, DURING PREFLIGHT INSPECTION, THE GALLEY EMERGENCY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGH - [SDR C2XA07IA034](https://openairdocs.org/sdr/C2XA07IA034), Feb 9, 2007: BATTERY. DISCHARGED. IAH - DURING PREFLIGHT INSPECTION, A CABIN EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY, O All 56: https://openairdocs.org/deregistered/N17108-2026-07-28/reports.md ## Other aircraft with N17108 - [Cancelled 1960-01-12](https://openairdocs.org/deregistered/N17108-1960-01-12): Stinson SR-8E, S/N 9788, built 1936. Owner: [Davis Melvin C](https://openairdocs.org/faa-owner/DAVIS%20MELVIN%20C), [Cincinnati, OH](https://openairdocs.org/faa-place/OH/Cincinnati) --- 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.