# N14943: 1998 Embraer EMB-145EP, registration cancelled 2015-05-26

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 26, 2015
- Exported to: South Africa
- Status when cancelled: Valid registration
- Airframe: [Embraer EMB-145EP](https://openairdocs.org/model/embraer-emb-145ep) (registry code 3260221)
- 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: 145040
- Year built: 1998
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 27, 2005
- Certificate issued: May 6, 2015
- Last registry action: May 6, 2015
- Mode S code: A0C71F
- 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/N14943
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14943
- Page: https://openairdocs.org/deregistered/N14943-2015-05-26

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-145EP: https://openairdocs.org/model/embraer-emb-145ep.md

## Service difficulty reports (108, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR ASOA20131029193H](https://openairdocs.org/sdr/ASOA20131029193H), Oct 29, 2013: DRAG ANGLE. CRACKED. DURING 2A INSPECTION THE LT VERTICLE STAB TO FUSELAGE LT DRAG ANGLE WAS FOUND TO HAVE A 20MM CRACK AT FRAME 76. MAINTENANCE R & R THE AFFECTED LT DRAG ANGLE, AN
- [SDR ASOA20131019188](https://openairdocs.org/sdr/ASOA20131019188), Oct 19, 2013: LIGHT. INOPERATIVE. DURING MAINTENANCE INSPECTION, LEFT FWD EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE AFFECTED EMERGENCY LIGHT, OPS TESTED WITH NO
- [SDR ASOA20130226089](https://openairdocs.org/sdr/ASOA20130226089), Mar 7, 2013: SKIN. CORRODED. DURING C-CHECK THE COCKPIT BELLY SKIN WAS FOUND TO BE CORRODED BETWEEN FRAMES 13-14 AND STRINGERS 18R-19L. MX R & R THE SKIN IAW SRM 51-40-02. THE ACFT WAS APPR
- [SDR ASOA20130226088](https://openairdocs.org/sdr/ASOA20130226088), Feb 26, 2013: BEAM. CORRODED. DURING C-CHECK THE CARGO DOOR CUT-OUT LOWER BEAM WAS FOUND TO BE CORRODED FROM FRAMES 65-68 BETWEEN STRINGERS 15L-16L. MX R & R THE BEAM IAW SRM 51-40-02. THE A
- [SDR ASOA20130226087](https://openairdocs.org/sdr/ASOA20130226087), Feb 26, 2013: SHEAR TIE. CORRODED. DURING C-CHECK THE SHEAR CLIP AT FRAME 65 BETWEEN STRINGERS 15L-16L WAS FOUND TO BE CORRODED. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5330
- [SDR ASOA20130226086](https://openairdocs.org/sdr/ASOA20130226086), Feb 26, 2013: SHEAR ANGLE. CORRODED. DURING C-CHECK THE SHEAR CLIP AT FRAME 68 BETWEEN STRINGERS 15L-16L WAS FOUND TO BE CORRODED. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5330
- [SDR ASOA20130226085](https://openairdocs.org/sdr/ASOA20130226085), Feb 26, 2013: SHEAR ANGLE. CRACKED. DURING C-CHECK THE RIB 1 SHEAR CLIP FROM FRAMES 40-45 WAS FOUND TO BE CRACKED. MX R & R THE SHEAR CLIP IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SER
- [SDR ASOA20121126147](https://openairdocs.org/sdr/ASOA20121126147), Nov 26, 2012: SKIN. CRACKED. DURING MX INSPECTION, THE FUSELAGE SKIN AT FR 75 ON EITHER SIDE OF STRINGER 2R WAS FOUND TO HAVE TWO CRACKS ONE APPROX .039" AND 1 APPROX .157" LONG. MX PERFORM
- [SDR ASOA20121126146](https://openairdocs.org/sdr/ASOA20121126146), Nov 26, 2012: SKIN. CRACKED. DURING MX INSPECTION, FUSELAGE SKIN WAS FOUND TO BE CRACKED ACROSS A RIVET HOLE APPROX 16MM IN LENGTH BETWEEN FRAME 77-78 JUST ABOVE STR 6R. MX INSTALLED A REPA
- [SDR ASOA20121126145](https://openairdocs.org/sdr/ASOA20121126145), Nov 26, 2012: SKIN. CRACKED. DURING MX INSPECTION, THE FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75, STRINGER 02L. MX PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA, AND THE ACFT WAS 
- [SDR ASOA20120824076](https://openairdocs.org/sdr/ASOA20120824076), Aug 23, 2012: ENGINE. SMOKE. GROUND CREW REPORTED FLAMES FROM NR 1 ENGINE. ENGINE SMOKING 15 MIN AFTER SHUTDOWN. R & R 1 ENGINE IAW AMM 71-00-00. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120503066](https://openairdocs.org/sdr/ASOA20120503066), May 3, 2012: SMOKE DETECTOR. DEFECTIVE. THE CREW REPORTED A BAGGAGE SMOKE WARNING ON EICAS. THE CREW DISCHARGED THE BAGGAGE FIRE EXTINGUISHERS AND THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOU
- [SDR C2XA11IA238](https://openairdocs.org/sdr/C2XA11IA238), Oct 17, 2011: UNKNOWN. ODOR. IAH - FLIGHT 4586, THE CREW REPORTED WEIRD SMELL DURING ENGINE START. MAINTENANCE INSPECTED THE AIRCRAFT, PERFORMED ENGINE STARTS, OPERATIONALLY CHECKED BLEED S
- [SDR C2XA10IA287](https://openairdocs.org/sdr/C2XA10IA287), Nov 9, 2010: ENGINE. MALFUNCTIONED. FLIGHT 2561 THE CREW REPORTED A BURNING SMOKE SMELL IN THE CABIN WITH THE NUMBER TWO ENGINE, NUMBER 2 BLEED, AND NUMBER TWO PACK RUNNING. THE AIRCRAFT LANDED AT
- [SDR C2XA10IA286](https://openairdocs.org/sdr/C2XA10IA286), Nov 9, 2010: ACM. SEIZED. IAH - FLIGHT 2561, THE CREW REPORTED SMOKE IN THE COCKPIT AND CABIN ON SHORT FINAL. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND RE
- [SDR C2XA10SH275](https://openairdocs.org/sdr/C2XA10SH275), Aug 16, 2010: FITTING. CORRODED. SHV - DURING C-CHECK THE SHEAR CLIP AT FRAME 65 WAS FOUND TO BE CORRODED BETWEEN STRINGERS 16-17L. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A SPLICE REPA
- [SDR C2XA10SH274](https://openairdocs.org/sdr/C2XA10SH274), Aug 16, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 33-34. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW E
- [SDR C2XA10SH273](https://openairdocs.org/sdr/C2XA10SH273), Aug 16, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24-25. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW E
- [SDR C2XA10SH272](https://openairdocs.org/sdr/C2XA10SH272), Aug 16, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAMES 22-23. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5320-012
- [SDR C2XA10SH266](https://openairdocs.org/sdr/C2XA10SH266), Aug 11, 2010: BEAM. CORRODED. SHV - DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT
- [SDR C2XA10IA117](https://openairdocs.org/sdr/C2XA10IA117), Apr 11, 2010: CONTROLLER. INOPERATIVE. MEM - FLIGHT 2249, DURING DESCENT THE CREW REPORTED THAT AUTO PRESSURIZATION FAILED. THE AIRCRAFT LANDED AT MEM WITHOUT INCIDENT WHERE THE CREW PLACED THE AUTO 
- [SDR C2XA10IA104](https://openairdocs.org/sdr/C2XA10IA104), Mar 25, 2010: SIGN. MALFUNCTIONED. IAH - FLIGHT 2132, DURING POST FLIGHT INSPECTION THE CREW REPORTED THE EXIT SIGN AT SEAT 12C TO BE INOPERATIVE. MAINTENANCE RESET THE EMERGENCY LIGHTS, OPERATIO
- [SDR C2XA10SH106](https://openairdocs.org/sdr/C2XA10SH106), Mar 23, 2010: RELAY. FAILED. FLT 2159 MEM-IAH DIVERT TO AEX - BLEED 1 LOW TEMP/ENG OPEN LIGHT NOT ILLUM IN ICING - SHV RECOVERY. MAINTENANCE PERFORMED ANTI-ICE OPERATIONAL CHECKS IAW EMB-14
- [SDR C2XA10TY030](https://openairdocs.org/sdr/C2XA10TY030), Mar 2, 2010: LIGHT. INOPERATIVE. SEAT 12BC OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED BULB IAW EMB145 AMM 33-50-07, OPS CHECK GOOD.
- [SDR C2XA10IA055](https://openairdocs.org/sdr/C2XA10IA055), Feb 5, 2010: CLAMP. DEFECTIVE. IAH - FLIGHT 2069 THE CREW REPORTED A BLEED ONE LEAK DURING CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLAC
- [SDR C2XA10IA047](https://openairdocs.org/sdr/C2XA10IA047), Feb 1, 2010: DUCT. LEAKING. IAH - FLIGHT 2277, THE CREW REPORTED A BLEED ONE LEAK MESSAGE DURING CRUISE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED 
- [SDR C2XA10IA041](https://openairdocs.org/sdr/C2XA10IA041), Jan 28, 2010: THERMOSTAT. INOPERATIVE. IAH - FLIGHT 2413 - THE CREW REPORTED A BLEED 1 LOW TEMP DURING ICING TEST. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED A
- [SDR C2XA09IA313](https://openairdocs.org/sdr/C2XA09IA313), Dec 9, 2009: INVERTER. INOPERATIVE. IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED AISLE PATH EMERGENCY LIGHTS TO BE INOPERATIVE IN THE REAR OF THE AIRCRAFT. MAINTENANCE REMOVED AND REPLACED 
- [SDR C2XA09IA180](https://openairdocs.org/sdr/C2XA09IA180), Jul 15, 2009: PROXIMITY SWITCH. INOPERATIVE. IAH - FLIGHT 2703 - DURING CLIMB THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTE
- [SDR C2XA09IA080A](https://openairdocs.org/sdr/C2XA09IA080A), Jul 15, 2009: PROXIMITY SENSOR. INOPERATIVE. DURING CLIMB THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE. ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX REMOVED AND REPLACED THE 
- [SDR C2XA09IA022](https://openairdocs.org/sdr/C2XA09IA022), Jan 23, 2009: BATTERY PACK. DISCHARGED. IAH - DURING A-CK INSPECTION THE LT FORWARD WING BOX EMERGENCY LIGHT, PAX DOOR EMERGENCY LIGHT, AND EMERGENCY LIGHT ABOVE THE FORWARD F/A SEAT WERE FOUND TO BE 
- [SDR C2XA08IA173](https://openairdocs.org/sdr/C2XA08IA173), Jul 21, 2008: UNKNOWN. ODOR. IAH - FLIGHT 2372 - THE FLIGHT ATTENDANT REPORTED A BURNING ODOR COMING FROM ROWS 8-10. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED 
- [SDR C2XA08CL012](https://openairdocs.org/sdr/C2XA08CL012), Jan 24, 2008: BLEED VALVE. FAULTY. BWI FLIGHT 2247 - THE CREW REPORTED A NR 1 ENGINE BLEED VALVE FAIL MESSAGE ON THE EICAS. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED T
- [SDR C2XAO8RI007](https://openairdocs.org/sdr/C2XAO8RI007), Dec 26, 2007: GENERATOR. INOPERATIVE. FLT 3142 - EWR - CREW REPORTED APU GENERATOR AND GENERATOR NR 1 OFF BUSS. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED AP
- [SDR C2XA08RI006](https://openairdocs.org/sdr/C2XA08RI006), Dec 26, 2007: GCU. INOPERATIVE. FLT 3142 - EWR - CREW REPORTED APU GENERATOR AND GENERATOR NR 1 OFF BUSS. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED AP
- [SDR C2XA07RI104](https://openairdocs.org/sdr/C2XA07RI104), Dec 8, 2007: WIRE. CHAFED. FLT 2616 - RIC - CREW REPORTED PAX DETECTED ELECTRIC TYPE OF SMOKE. RIC MX FOUND ELECTRIC EMERGENCY SIGN AT ROW 3BC WITH BARE WIRE EXPOSED. MX REPAIRED WIRE AND
- [SDR C2XA07RI101](https://openairdocs.org/sdr/C2XA07RI101), Nov 21, 2007: RELAY. FAILED. FLIGHT 2929 - EWR - CREW REPORTED BAGG SMOKE LIGHT ON, BUT NO VISUAL SMOKE IN CARGO BAY. EWR MX REMOVED AND REPLACED BAGG SMOKE TEST RELAY AND PERFORMED OPERATI
- [SDR C2XA07SH083](https://openairdocs.org/sdr/C2XA07SH083), Oct 13, 2007: FLOORBEAM. CORRODED. SHV - DURING C-CHECK LEFT OMEGA BEAM HAS CORROSION ON FR 20. MX REPAIRED LEFT OMEGA BEAM AT FR 20 IAW EMB 145 SRM 53-00-13. THE AIRCRAFT WAS APPROVED TO RETURN 
- [SDR C2XA07IA093](https://openairdocs.org/sdr/C2XA07IA093), Apr 20, 2007: CONNECTOR. LOOSE. IAH - FLIGHT 2277, THE CREW REPORTED THAT THE EMERGENCY EXIT SIGN ABOVE THE F/A SEAT WORKED INTERMITTENTLY. MAINTENANCE INSPECTED THE AIRCRAFT AND RESECURED THE
- [SDR C2XA06IA127](https://openairdocs.org/sdr/C2XA06IA127), Jul 31, 2006: POWER SUPPLY. DISCHARGED. IAH - FLIGHT 2415, THE CREW REPORTED THAT THE LT FUSELAGE EXTERIOR LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY, O
- [SDR C2XA05IA116](https://openairdocs.org/sdr/C2XA05IA116), Oct 18, 2005: INVERTER. INOPERATIVE. IAH - FLIGHT 2418, DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE LOWER AFT LEFT EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLAC
- [SDR C2XA05SH088](https://openairdocs.org/sdr/C2XA05SH088), Jul 21, 2005: HINGE. WORN. SHV-DURING C-CHECK MAINTENANCE FOUND HAT BUSHING HOUSING AT ATTACHMENT FITTING FOR UPPER HYDRAULIC ACTUATOR ON RUDDER I IS WORN. MAINTENANCE REPAIRED HAT BUSHIN
- [SDR C2XA05SH087](https://openairdocs.org/sdr/C2XA05SH087), Jul 21, 2005: HINGE. CRACKED. SHV-DURING C-CHECK MAINTENANCE FOUND RUDDER II UPPER MIDDLE ATTACHMENT BRACKET CRACKED. MAINTENANCE REMOVED AND REPLACED RUDDER II UPPER MIDDLE ATTACHMENT BRACK
- [SDR C2XA05SH086](https://openairdocs.org/sdr/C2XA05SH086), Jul 21, 2005: FLOOR SUPPORT. CORRODED. SHV-DURING C-CHECK MAINTENANCE FOUND LT OMEGA BEAM FLOOR SUPPORT FLANGE HAS CORROSION BETWEEN FRAMES 20-24. MAINTENANCE REMOVED & REPLACED LT OMEGA BEAM FROM FR
- [SDR C2XA05SH085](https://openairdocs.org/sdr/C2XA05SH085), Jul 21, 2005: FLOOR SUPPORT. CORRODED. SHV-DURING C-CHECK MAINTENANCE FOUND LT OMEGA BEAM LOWER FLANGE IS CORRODED BETWEEN FRAMES 53-59. MAINTEANACE REPAIRED LOWER FLANGE AT FRAME 54 I/A/W EMB 145 SR
- [SDR C2XA05SH084](https://openairdocs.org/sdr/C2XA05SH084), Jul 21, 2005: FLOOR SUPPORT. CORRODED. SHV-DURING C-CHECK MAINTENANCE FOUND CENTER OMEGA BEAM HAS CORROSION AT FRAME 20. MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM FROM FRAMES 11-23 I/A/W EMB
- [SDR C2XA05SH083](https://openairdocs.org/sdr/C2XA05SH083), Jul 21, 2005: FLOOR SUPPORT. CORRODED. SHV-DURING C-CHECK MAINTENANCE FOUND LT OMEGA BEAM HAS CORROSION AT VARIOUS AREAS BETWEEN FRAMES 38-46. MAINTENANCE REPAIRED LT OMEGA BEAM BETWEEN FRAMES 38 & 4
- [SDR C2XA05SH082](https://openairdocs.org/sdr/C2XA05SH082), Jul 21, 2005: SKIN PANEL. LIGHTNING STRIKE. SHV-DURING C-CHECK MAINTENANCE FOUND LIGHTNING STRIKES AT LOWER RT WING, NEAR PNL 631 AB. MAINTENANCE REPAIRED LIGHTNING STRIKES AT LOWER RT WING, NEAR PNL 631 
- [SDR C2XA05SH081](https://openairdocs.org/sdr/C2XA05SH081), Jul 21, 2005: SKIN PANEL. LIGHTNING STRIKE. SHV-DURING C-CHECK MAINTENANCE FOUND LIGHTNING STRIKE AT FRAME 23 STR 17R. MAINTENANCE REPAIRED LIGHTNING STRIKE AT FRAME 23 STR 17R I/A/W EC 5330-01480, REPAIR
- [SDR C2XA05SH080](https://openairdocs.org/sdr/C2XA05SH080), Jul 21, 2005: SKIN PANEL. LIGHTNING STRIKE. SHV-DURING C-CHECK MAINTENANCE FOUND LIGHTENING STRIKE AT FRAMES 21-22, STR 18R. MAINTENANCE REPAIRED LIGHTENING STRIKES AT FRAMES 21-22, STR 18R I/A/W EC 5330-

All 108: https://openairdocs.org/deregistered/N14943-2015-05-26/reports.md

## FAA accident and incident reports (2)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20000122003369I](https://openairdocs.org/incident/20000122003369I), Jan 22, 2000: Emb EMB145ER (N14943), Cleveland, OH. Continental express 4107 taxed across rny 23L after acknowledging ATCT clearance to hold short. See form 8020-18[privacy data omitted]for details. [privacy…
- [Incident 19990124013839I](https://openairdocs.org/incident/19990124013839I), Jan 24, 1999: Emb EMB145 (N14943), Newark, NJ. Pilot had smoke in cabin lav area after landing at ewr. During taxi to parking, egressed 48 passengers. No passenger injuries. Co exp pax buss dispatched to…

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