# N14939: 1997 Embraer EMB-145EP, registration cancelled 2015-08-13 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 13, 2015 - 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: 145030 - Year built: 1997 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 27, 2005 - Certificate issued: February 23, 1998 - Last registry action: January 29, 2015 - Mode S code: A0C702 - Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%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/N14939 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14939 - Page: https://openairdocs.org/deregistered/N14939-2015-08-13 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 (135, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASOA20140801100](https://openairdocs.org/sdr/ASOA20140801100), Aug 1, 2014: LIGHT. INOPERATIVE. DURING PREFLIGHT INSPECTION, THE CREW REPORTED EXIT ROW EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE R & R THE AFFECTED LIGHT ASSEMBLY, OPERATIONALLY TESTED W - [SDR ASOA20140318066](https://openairdocs.org/sdr/ASOA20140318066), Mar 18, 2014: FRAME. CRACKED. DOOR 123BL CRACKED UNDER HINGE POINT MOUNT. REMOVED CRACKED FRAME AND INSTALLED NEW HALF FRAME ON DOOR 123BL IAW SRM 51-40-02. - [SDR ASOA20140318065T](https://openairdocs.org/sdr/ASOA20140318065T), Mar 18, 2014: CHANNEL. CORRODED. CORROSION ON RT OMEGA BEAM AT NUTPLATE JUST AFT OF FRAME 59. REMOVED CORROSION, REPAIRED OMEGA BEAM IAW EC5320-01910. - [SDR ASOA20140318064](https://openairdocs.org/sdr/ASOA20140318064), Mar 18, 2014: FLOORBEAM. CRACKED. FLOORBEAM FRAME 61 NUTPLATE HOLE CRACKED. R & R TEE ON FLOORBEAM IAW SRM 51-40-02. - [SDR ASOA20140318063](https://openairdocs.org/sdr/ASOA20140318063), Mar 18, 2014: SHEAR TIE. CRACKED. SHEAR TIE CRACKED AT FRAME 24 BETWEEN STRINGERS 15 & 16R. R & R SHEAR TIE IAW SRM 51-40-02. - [SDR ASOA20140318062](https://openairdocs.org/sdr/ASOA20140318062), Mar 18, 2014: SHEAR TIE. CRACKED. CRACK AT RIVET IN SHEAR TIE AT FRAME 81, APU FIREWALL, BETWEEN S1 & 2R. REMOVED CRACKED SHEAR TIE AND INSTALLED NEW IAW SRM 51-40-02. - [SDR ASOA20140318061](https://openairdocs.org/sdr/ASOA20140318061), Mar 18, 2014: ATTACH ANGLE. CRACKED. CRACK IN ANGLE JOINING FRAME 46 TO WING BOX ON RT SIDE AT FLOOR LEVEL. R & R ANGLE IAW SRM 51-40-02. - [SDR ASOA20140318060T](https://openairdocs.org/sdr/ASOA20140318060T), Mar 18, 2014: CHANNEL. CRACKED. LEFT OMEGA GUSSET OTBD SPLICE CRACKED BETWEEN FRAMES 16 & 17. R & R OMEGA GUSSET IAW 51-40-02. - [SDR ASOA20140318059](https://openairdocs.org/sdr/ASOA20140318059), Mar 18, 2014: CHANNEL. CORRODED. RIGHT OMEGA BEAM CORROSION AROUND NUTPLATE FRAME 23. REMOVED CORROSION AND FABRICATED REPAIR IAW EC5320-01443, REV C. - [SDR ASOA20140318058](https://openairdocs.org/sdr/ASOA20140318058), Mar 18, 2014: FLOOR SUPPORT. CHAFED. LEFT FLOOR SUPPORT AT FRAME 72 HAS CHAFED METAL IN MULTIPLE AREAS WITH EXPOSED BARE METAL. R & R FLOOR SUPPORT IAW 51-40-02. - [SDR ASOA20140318057](https://openairdocs.org/sdr/ASOA20140318057), Mar 18, 2014: SHEAR TIE. CRACKED. FRAME 46 SHEAR TIE CRACKED. - [SDR ASOA20140318056](https://openairdocs.org/sdr/ASOA20140318056), Mar 18, 2014: FLOOR SUPPORT. CORRODED. RT FORWARD FLOOR SUPPORT HAS CORROSION OTBD OF NUTPLATE BETWEEN FRAMES 23 & 24. FOUND OUT OF LIMITS IAW SRM 53-21-10. - [SDR ASOA20140318055](https://openairdocs.org/sdr/ASOA20140318055), Mar 18, 2014: FLOOR SUPPORT. CRACKED. RT OMEGA BEAM SUPPORT FLANGE CRACKED NEAR FOOT RADIUS AT FRAME 47 ON OTBD SIDE OF BEAM. - [SDR ASOA20140318054](https://openairdocs.org/sdr/ASOA20140318054), Mar 18, 2014: CHANNEL. CORRODED. C-CHECK, THE CENTER OMEGA BEAM GUSSET WAS CORRODED AT NUTPLATES AT FRAME 16. MAINTENANCE REMOVED THE CORROSION AND FABRICATED A NEW REPAIR IAW EC 5320-01215, RE - [SDR ASOA20140318053T](https://openairdocs.org/sdr/ASOA20140318053T), Mar 18, 2014: CHANNEL. CORRODED. DURING C-CHECK, THE RT SIDE OMEGA BEAM TOPCAP WAS FOUND CORRODED AT FRAME 59. MAINTENANCE R & R THE RT SIDE OMEGA BEAM GUSSET AT FRAME 59 IAW SRM 51-40-02 - [SDR ASOA20140318052T](https://openairdocs.org/sdr/ASOA20140318052T), Mar 18, 2014: SHEAR TIE. CRACKED. DURING C-CHECK, LT CENTER FUSELAGE FRAME 46 HAS A SHEAR TIE CRACKED. MAINTENANCE R & R THE SHEAR TIE IAW SRM 51-40-02. - [SDR ASOA20140318051](https://openairdocs.org/sdr/ASOA20140318051), Mar 18, 2014: FLOOR SUPPORT. CRACKED. C-CHECK, THE LT FLOOR SUPPORT SPLICE WAS FOUND CRACKED AT FRAMES 23 AND 24. MAINTENANCE R & R IAW SRM 51-40-02. - [SDR ASOA20130830158](https://openairdocs.org/sdr/ASOA20130830158), Aug 30, 2013: GCU. MALFUNCTIONED. THE CREW REPORTED AN ELECTRICAL PROBLEM WITH THE MAIN BUSS SHORTING OUT AT 23K FT ALT WITH A LOUD BANG WHICH SHOOK THE ENTIRE ACFT. SMOKE, ELECTRICAL ODOR CAME - [SDR ASOA20130830157](https://openairdocs.org/sdr/ASOA20130830157), Aug 30, 2013: STARTER GEN. MALFUNCTIONED. THE CREW REPORTED AN ELECTRICAL PROBLEM WITHTHE MAIN BUS SHORTING OUT AT 23K FT ALT WITH A LOUD BANG WHICH SHOOK THE ENTIRE ACFT. SMOKE, ELECTRICAL SMELL CAME I - [SDR ASOA20130209010H](https://openairdocs.org/sdr/ASOA20130209010H), Feb 9, 2013: SKIN. CRACKED. DURING SCHEDULED MX, THE AFT FUSELAGE AFT UPPER SKIN WAS FOUND TO BE CRACKED AT FRAME NR 75 NEAR STRINGER NR 2. THE FUSELAGE SKIN WAS REPAIRED BY INSTALLATION O - [SDR ASOA20120323043](https://openairdocs.org/sdr/ASOA20120323043), Mar 23, 2012: CDU. SHORTED. THE CREW REPORTED A STRONG ELECTRICAL ODOR FROM BEHIND THE CAPTAIN`S SEAT AREA. MX INSPECTED AND FOUND THE FMS, CMU TO BE CAUSING THE ODOR. MX R & R THE FMS CDU - [SDR ASOA20120229029](https://openairdocs.org/sdr/ASOA20120229029), Feb 29, 2012: SENSOR. INOPERATIVE. DURING TAKEOFF ROLL AT APPROX 90KTS, THE CREW REPORTED THAT THEY SMELLED SMOKE AND RECEIVED A BRAKE OVERHEAT MESSAGE. TAKEOFF WAS ABORTED AND THE ACFT RETURNED - [SDR ASOA2011112600005](https://openairdocs.org/sdr/ASOA2011112600005), Nov 26, 2011: SKIN. DAMAGED. DURING C-CHECK, WORKING RIVETS AT FRAME 77, STRINGER 4R-10R. MX PERFORMED REPAIR OF FUSELAGE EXTERNAL SKIN AT FRAME 77, STRINGER 4R-10R IAW EC5330-02501 ORIG. T - [SDR ASOA2011112600004](https://openairdocs.org/sdr/ASOA2011112600004), Nov 26, 2011: SKIN. CRACKED. DURING C-CHECK, FUSELAGE CRACKED AROUND RIVET AT FRAME 78, STRINGER 6R-7R. MX PERFORMED REPAIR OF FUSELAGE EXTERNAL SKIN AT FRAME 78, STRINGER 6R-7R IAW EC5330- - [SDR ASOA2011112600003](https://openairdocs.org/sdr/ASOA2011112600003), Nov 26, 2011: SKIN. CRACKED. DURING C-CHECK, FUSELAGE CRACKED AROUND RIVET AT FRAME 78, STRINGER 7R-8R. MX PERFORMED REPAIR OF FUSELAGE AT FRAME 78, STRINGER 7R-8R IAW EC5330-02501 ORIG. TH - [SDR ASOA201111260002](https://openairdocs.org/sdr/ASOA201111260002), Nov 26, 2011: SKIN. CRACKED. DURING C-CHECK FUSELAGE CRACKED AROUND RIVET AT FRAME 79 STRINGER 4R-5R. MX PERFORMED REPAIR OF FUSELAGE SKIN IAW EC5330-02501 ORIG. AIRCRAFT RETURNED TO SERVIC - [SDR ASOA201111261009](https://openairdocs.org/sdr/ASOA201111261009), Nov 26, 2011: THRESHOLD. CORRODED. DURING C-CHECK SERVICE DOOR THRESHOLD CORRODED AROUND NUTPLATES. MX R & R SERVICE DOOR CENTER SILL IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE - [SDR ASOA201111261008](https://openairdocs.org/sdr/ASOA201111261008), Nov 26, 2011: SKIN. CRACKED. DURING C-CHECK FUSELAGE CRACKED AROUND RIVET AT FRAME 79 STRINGER 5R-6R. MX PERFORMED REPAIR OF FUSELAGE EXTERNAL SKIN AT FRAME 79 STRINGER 5R-6R IAW EC5330-025 - [SDR ASOA201111261006](https://openairdocs.org/sdr/ASOA201111261006), Nov 26, 2011: SKIN. CRACKED. DURING C-CHECK FUSELAGE CRACKED AROUND RIVET AT FRAME 75 STRINGER 3R-4R. MX PERFORMED REPAIR OF FUSELAGE EXTERNAL SKIN AT FRAME 75 STRINGER 3R-4R IAW EC5330-023 - [SDR C2XA11IA244](https://openairdocs.org/sdr/C2XA11IA244), Oct 29, 2011: INDICATION SYS. MALFUNCTIONED. IAH - FLIGHT 4664 THE CREW REPORTED THAT FUEL QUANTITY NR 1 DASHED OUT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE OPERATIONALLY - [SDR C2XA11IA129](https://openairdocs.org/sdr/C2XA11IA129), Jun 24, 2011: BRACKET. BROKEN. IAH - FLIGHT 2481, THE CREW REPORTED AN INFLIGHT ABNORMAL VIBRATION IN THE YOKE WHILE AIRBORNE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. M - [SDR C2XA11IA078](https://openairdocs.org/sdr/C2XA11IA078), May 1, 2011: COMPUTER. FAULTY. IAH - FLIGHT 3127, THE CREW REPORTED THAT AHRS NR 1 FAILED IN FLIGHT TWICE FOR 30 SECONDS. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTE - [SDR C2XA11IA059](https://openairdocs.org/sdr/C2XA11IA059), Mar 21, 2011: ENGINE. VIBRATION. IAH - FLIGHT 2482 IAH-GPT, THE CREW REPORTED ENGINE TWO VIBRATION IN AMBER FOR 2-3 SECONDS DURING CLIMB, AND AFTER POWERING BACK THE VIBE RETURNED TO GREEN RANG - [SDR C2XA11IA007](https://openairdocs.org/sdr/C2XA11IA007), Jan 3, 2011: LIGHT. OVERHEATED. FLIGHT 2967, DURING PREFLIGHT INSPECTION THE CREW REPORTED AN ELECTRIC BURNING ODOR AROUND ROW 5 OR 6. MAINTENANCE INSPECTED THE AIRCRAFT, FOUND A BAD LIGHT SOC - [SDR C2XA10IA089](https://openairdocs.org/sdr/C2XA10IA089), Mar 7, 2010: ECU. INOPERATIVE. LCH - FLIGHT 2214, THE CREW REPORTED A FLAP FAIL DURING CRUISE. THE AIRCRAFT DIVERTED TO LCH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED - [SDR C2XA09SH343](https://openairdocs.org/sdr/C2XA09SH343), Oct 13, 2009: FITTING. CRACKED. DURING C-CHECK, NR 1 ENG FWD LOWER YOKE FITTING CRACKED. REMOVED AND REPLACED FWD LOWER YOKE FITTING IAW EC5450-01021. AIRCRAFT WAS APPROVED FOR RETURN TO SERVI - [SDR C2XA09IA216](https://openairdocs.org/sdr/C2XA09IA216), Aug 27, 2009: SPLICE. BROKEN. IAH - DURING MAINTENANCE INSPECTION THE AFT SECTION OF AISLE PATH LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BROKEN SPLICES, OPE - [SDR C2XA09IA178](https://openairdocs.org/sdr/C2XA09IA178), Jul 13, 2009: LIGHT. INOPERATIVE. IAH - FLIGHT 2115 - DURING POST FLIGHT INSPECTION THE LEFT FORWARD WING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECT - [SDR C2XA09TY137A](https://openairdocs.org/sdr/C2XA09TY137A), Jul 4, 2009: SOCKET. BROKEN. EMERGENCY LIGHT IN THE MAIN DOOR AND THE SERVICE DOOR INOP. REMOVED AND REPLACED THE LIGHT SOCKETS IAW EMB AMM 33-50-06. OPS CHECK GOOD. - [SDR C2XA09IA153](https://openairdocs.org/sdr/C2XA09IA153), Jun 10, 2009: FAN. INOPERATIVE. IAH - FLIGHT 3042, ON CLIMB, THE CREW REPORTED AN AHRS 1 OVERHEAT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLAC - [SDR C2XA09CL075](https://openairdocs.org/sdr/C2XA09CL075), May 27, 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 C2XA09SH169](https://openairdocs.org/sdr/C2XA09SH169), May 24, 2009: FRAME. DAMAGED. SHV - DURING C-CHECK FRAME 10 JUST ABOVE STRINGER 10L WAS CRACKED AND PIECE MISSING. MAINTENANCE REMOVED AND REPLACED FRAME 10 STRINGER 10L IAW SRM 51-40-02. TH - [SDR C2XA09SH168](https://openairdocs.org/sdr/C2XA09SH168), May 24, 2009: FRAME. DAMAGED. SHV - DURING C-CHECK RT CARGO FRAME 64 HAD A DAMAGED RIVET BETWEEN STRINGER 8R-9R. MAINTENANCE REPAIRED FRAME 64 STRINGER 8R-9R WITH REPAIR IAW IC2009-145/03545 - [SDR C2XA09SH167](https://openairdocs.org/sdr/C2XA09SH167), May 24, 2009: BEAM. CORRODED. SHV - DURING C-CHECK CARGO CUTOUT LOWER BEAM HAD CORROSION. MAINTENANCE REMOVED AND REPLACED CARGO LOWER BEAM AT FRAME 65-68 IAW EMB-145 SRM 51-40-02. THE AIRCR - [SDR C2XA09SH166](https://openairdocs.org/sdr/C2XA09SH166), May 24, 2009: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK RT OMEGA BEAM HAD CORROSION AT NUT PLATE HOLES AT FRAME 20. MAINTENANCE REPAIRED RT OMEGA BEAM AT FRAME 20 IAW EC5320-01461. THE AIRCRAFT W - [SDR C2XA09SH165](https://openairdocs.org/sdr/C2XA09SH165), May 24, 2009: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM HAD CORROSION AT FRAME 20. MAINTENANCE REPAIRED LT OMEGA BEAM WITH REPAIR AT FRAME 20 IAW EMB-145 SRM 51-40-02 AND CPM 51-21- - [SDR C2XA09TY027](https://openairdocs.org/sdr/C2XA09TY027), Feb 14, 2009: BATTERY. DISCHARGED. NR 2 EMERGENCY LIGHT BATTERY LOW VOLTAGE. REMOVED AND REPLACED BATTERY IAW EMB 145 AMM 33-50-04. OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE. - [SDR C2XA09IA043](https://openairdocs.org/sdr/C2XA09IA043), Feb 11, 2009: LIGHT. INOPERATIVE. IAH - FLIGHT 2931, DURING PREFLIGHT INSPECTION THE AISLE PATH EMERGENCY LIGHT STRIP BY THE EXIT ROW WAS FOUND TO BE INOPERATIVE. MX R&R THE AFFECTED LIGHT STRIP - [SDR C2X2008F00006](https://openairdocs.org/sdr/C2X2008F00006), Jul 19, 2008: WIRE. BROKEN. IAH - FLIGHT 3056 ON TAKEOFF ROLL THE CREW REPORTED SEEING HOT EMBERS AND DETECTING SMOKE FROM UNDER THE CAPTAINS DASH, WITH THE CIRCUIT BREAKER ON THE OVERHEAD - [SDR C2XA08IA103](https://openairdocs.org/sdr/C2XA08IA103), Apr 6, 2008: UPLOCK. MALFUNCTIONED. IAH - FLIGHT 2106, THE CREW REPORTED A LOUD BANGING NOISE UNDER THE FLIGHT COMPARTMENT FLOOR, AND THAT THE RIGHT MAIN LANDING GEAR INDICATION CYCLING BETWEEN UP All 135: https://openairdocs.org/deregistered/N14939-2015-08-13/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 20130830024749I](https://openairdocs.org/incident/20130830024749I), Aug 30, 2013: Embraer EMB-145EP (N14939), Beaumont, TX, No damage. On the ramp at george bush intercontinental airport (iah) in houston, Texas the EMB-145 had an electrical issue that resulted in the PFD and MFD screens losing… - [Incident 20000530033329I](https://openairdocs.org/incident/20000530033329I), May 30, 2000: Emb EMB145ER (N14939), Midland, TX. (-23)Pressurization difficulties caused the RJ-145 aircraft to declare an emergency as they reached 17,000 feet MSL and return to Midland airport. There were… ## Other aircraft with N14939 - [Cancelled 1943-05-06](https://openairdocs.org/deregistered/N14939-1943-05-06): Lockheed ELECTRA 10-A, S/N 1028. Exported to Brazil. Owner: [Defense Supplies Corp](https://openairdocs.org/faa-owner/DEFENSE%20SUPPLIES%20CORP), [Washington, DC](https://openairdocs.org/faa-place/DC/Washington) - [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N14939-undated): Boeing 747-123, S/N 20108. 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.