# N14942: 1997 Embraer EMB-145EP, registration cancelled 2016-11-15 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 15, 2016 - Exported to: Israel - 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: 145037 - Year built: 1997 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 27, 2005 - Certificate issued: May 12, 2016 - Last registry action: May 12, 2016 - Mode S code: A0C71E - 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/N14942 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14942 - Page: https://openairdocs.org/deregistered/N14942-2016-11-15 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-145EP: https://openairdocs.org/model/embraer-emb-145ep.md ## Service difficulty reports (90, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASOA20130514070](https://openairdocs.org/sdr/ASOA20130514070), May 14, 2013: INVERTER. INOPERATIVE. DURING 1A INSPECTION THE AFT GALLEY EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MX R & R THE AFFECTED LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND - [SDR ASOA20130407050](https://openairdocs.org/sdr/ASOA20130407050), Apr 7, 2013: SKIN. CRACKED. DURING A-CK INSPECTION, THE RT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75 JUST BELOW STR2R. MX PERFORMED A DOUBLER REPAIR WITH DRAG ANGLE IAW ENGINEERING - [SDR ASOA20121205164](https://openairdocs.org/sdr/ASOA20121205164), Dec 4, 2012: SKIN. CORRODED. THE FORWARD LOWER FUSELAGE INTERNAL SKIN WAS NOTED WITH CORROSION BEYOND LIMITS BETWEEN FRAMES 13 & 14, STRINGER 19L THRU 18R. R & R SKIN PANEL, REMAPPED LT & R - [SDR ASOA20121128160](https://openairdocs.org/sdr/ASOA20121128160), Nov 27, 2012: SPLICE. CORRODED. LONGITUDINAL SKIN SPLICE STRAP CORRODED BETWEEN FRAME 13 AND 14, STRINGER 19L. REMOVED CORRODED SECTION OF STRAP, FABRICATED AND INSTALLED NEW STRAP. - [SDR ASOA20121128159](https://openairdocs.org/sdr/ASOA20121128159), Nov 27, 2012: SPLICE. CORRODED. CIRCUMFERENTIAL SKIN SPLICE STRAP CORRODED BETWEEN FRAME 13 & 14, STRINGER 21L THRU 18R. CUT-OUT CORRODED SECTION OF STRAP, FABRICATED AND INSTALLED NEW STRAP. - [SDR ASOA20120509070](https://openairdocs.org/sdr/ASOA20120509070), May 9, 2012: SOCKET. DIRTY. DURING MX INSPECTION, THE LT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MX CLEANED THE LIGHT BULB SOCKET, OPS TESTED WITH NO DEFECTS AND THE ACFT WAS - [SDR ASOA201205068](https://openairdocs.org/sdr/ASOA201205068), May 8, 2012: LIGHT. INOPERATIVE. DURING MX INSPECTION OF THE EMERGENCY LIGHTS, THE AISLE PATH LIGHT STRIP AT ROW 12 WAS FOUND TO BE INOPERATIVE. MX R & R THE EMERGENCY LIGHT STRIP, OPS TESTED W - [SDR ASOA20120214020](https://openairdocs.org/sdr/ASOA20120214020), Feb 14, 2012: TERMINAL. LOOSE. THE CREW REPORTED A STRONG ELECTRICAL ODOR COMING FROM BEHIND THE CAPTAINS SEAT. MX R & R BURNED LOOSE TERMINAL LUGS AT DC BUSS NR 1 BUSS BAR, OPS TESTED WITH N - [SDR C2XA11IA060](https://openairdocs.org/sdr/C2XA11IA060), Mar 27, 2011: SKIN. CRACKED. IAH - DURING MAINTENANCE INSPECTION THE CROWN SKIN PANEL ON THE CAPTAINS SIDE WAS FOUND TO BE CRACKED BETWEEN THE CAPTAINS DV WINDOW AND THE CAPTAINS WINDSHIELD - [SDR C2XA10IA225](https://openairdocs.org/sdr/C2XA10IA225), Aug 11, 2010: BATTERY. OVERTEMP. IAH - FLIGHT 2336, DURING TAXI THE CREW REPORTED A BATTERY TWO OVERTEMP. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO - [SDR C2XA10SH257](https://openairdocs.org/sdr/C2XA10SH257), Aug 3, 2010: BATTERY. OVERTEMP. JAN - BATTERY NR 2 OVERTEMP. REMOVED AND REPLACED NR 2 BATTERY IAW EMB 145 AMM 24-36-01. OPS CHECK GOOD. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10IA211](https://openairdocs.org/sdr/C2XA10IA211), Jul 27, 2010: BALLAST. DEFECTIVE. IAH - FLIGHT 2547, DURING PREFLIGHT INSPECTION THE CREW REPORTED A BURNING SMELL IN THE CABIN. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE G - [SDR C2XA10IA204](https://openairdocs.org/sdr/C2XA10IA204), Jul 17, 2010: BALLAST. OVERHEATED. IAH - FLIGHT 2034, DURING POST FLIGHT INSPECTION THE CREW REPORTED A STRONG BURNING SMELL IN THE GALLEY, AND THAT THE GALLEY LIGHT BALLAST WAS INOP. MAINTENANCE - [SDR C2XA10SH199](https://openairdocs.org/sdr/C2XA10SH199), Jun 7, 2010: SKIN. CRACKED. SHV - DURING C CHECK IT WAS FOUND THAT THE VERTICAL STABILIZER INTERNAL FITTING WAS FRETTING WITH THE AFT FUSELAGE SKIN AT FRAME 75 BY STRINGER 1L. THE FRETTING - [SDR C2XA10SH198](https://openairdocs.org/sdr/C2XA10SH198), Jun 7, 2010: ATTACH BRACKET. WORN. SHV - DURING C CHECK THE LT SPEED BRAKE CENTER ATTACH BRACKET WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHING. MAINTENANCE REMOVED AND REPLACED THE AF - [SDR C2XA10SH197](https://openairdocs.org/sdr/C2XA10SH197), Jun 7, 2010: ATTACH BRACKET. WORN. SHV - DURING C CHECK THE LT GROUND SPOILER ACTUATOR ATTACH BRACKET WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHING. MAINTENANCE PERFORMED A BUSHING RE - [SDR C2XA10SH196](https://openairdocs.org/sdr/C2XA10SH196), Jun 7, 2010: BEAM. CORRODED. SHV - DURING C CHECK THE PILOTS WINDSHIELD CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED AT SCREW HOLES 41, 43, 45, 49. MAINTENANCE REMOVED THE CORROSION AND PERFO - [SDR C2XA10SH195](https://openairdocs.org/sdr/C2XA10SH195), Jun 7, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS A - [SDR C2XA10SH194](https://openairdocs.org/sdr/C2XA10SH194), Jun 7, 2010: SKIN. CRACKED. SHV - DURING C CHECK THE RT AFT SKIN WAS FOUND TO BE CRACKED AROUND FASTENER AT FRAME 75 BETWEEN STRINGERS 1-2R. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC53 - [SDR C2XA10SH189](https://openairdocs.org/sdr/C2XA10SH189), Jun 2, 2010: BEAM. CORRODED. SHV-DURING C CHECK THE CARGO DOOR CUT-OUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC 5320-01479. THE AIRCRAFT WAS APPROV - [SDR C2XA10SH188](https://openairdocs.org/sdr/C2XA10SH188), Jun 2, 2010: STRINGER SPLICE. CORRODED. SHV - DURING C CHECK THE SPLICE ON STRINGER 18L WAS FOUND TO BE CORRODED BETWEEN FRAMES 60-61. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SPLICE IAW EMB 145 - [SDR C2XA10TY011](https://openairdocs.org/sdr/C2XA10TY011), Jan 12, 2010: SKIN. DENTED. TYS - A/C WAS A OVERNIGHT A/C WHEN INSPECTION FOUND MULTIPLE DENTS IN A SMALL AREA OUT OF LIMITS. MAINTENANCE CUT OUT THE DAMAGE AREA AND FAB A FILLER AND DOUBL - [SDR C2XA09IA199](https://openairdocs.org/sdr/C2XA09IA199), Aug 6, 2009: WIRE. BROKEN. IAH - DURING MAINTENANCE INSPECTION THE AISLE PATH LIGHT STRIP AT ROWS 16 & 17 WAS FOUND TO HAVE BROKEN WIRES. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIG - [SDR C2XA09IA198](https://openairdocs.org/sdr/C2XA09IA198), Aug 6, 2009: WIRE. BROKEN. IAH - DURING MAINTENANCE INSPECTION THE AISLE PATH LIGHT STRIP AT ROW 8 & 9 WAS FOUND TO HAVE BROKEN WIRES. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT - [SDR C2XA09IA077](https://openairdocs.org/sdr/C2XA09IA077), Mar 14, 2009: LIGHT. INOPERATIVE. IAH - DURING A-CK INSPECTION THE SERVICE DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE SERVICE DOOR EMERGENCY LIGHT, OP - [SDR C2XA08IA160](https://openairdocs.org/sdr/C2XA08IA160), Jul 13, 2008: OIL SYSTEM. LEAKING. IAH - FLIGHT 2684, THE CREW REPORTED THAT THE NUMBER ONE ENGINE OIL QUANTITY DROPPED TO 3 QTS IN FLIGHT WHILE PRESSURE AND TEMPERATURE REMAINED NORMAL. THE CREW - [SDR C2XA08CL011](https://openairdocs.org/sdr/C2XA08CL011), Jan 23, 2008: STRUCTURE. LOOSE. CLE FLIGHT 2532 - THE CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN. MAINTENANCE INSPECTED AND TIGHTENED BOLTS ON THE MAIN CABIN DOOR INNER HANDLE BOX. OPE - [SDR C2XA07SH063](https://openairdocs.org/sdr/C2XA07SH063), Sep 6, 2007: PANEL. CORRODED. SHV - DURING C-CHECK MAINTENANCE FOUND LOWER AILERON SHROUDS BONDING STRIPS WITH CORROSION. MAINTENANCE REPAIRED LOWER AILERON SHROUD IAW EC5750-01315 REV D. AI - [SDR C2XA07SH062](https://openairdocs.org/sdr/C2XA07SH062), Sep 6, 2007: PANEL. CORRODED. SHV - DURING C-CHECK MAINTENANCE FOUND PNL 193 BONDING STRIPS WITH CORROSION. MAINTENANCE REPAIRED PNL 193 BONDING STRIPS IAW EC 5750-01315 REV D. THE AIRCRAFT - [SDR C2XA07SH061](https://openairdocs.org/sdr/C2XA07SH061), Sep 6, 2007: FRAME. CRACKED. SHV - DURING C-CHECK MAINTENANCE FOUND FRAME 65 WITH CORROSION UNDER CARGO DOOR HOLD OPEN ROD SUPPORT BRACKET. MAINTENANCE REPAIRED CARGO DOOR HOLD OPEN ROD SUP - [SDR C2XA07SH060](https://openairdocs.org/sdr/C2XA07SH060), Sep 6, 2007: NUT PLATE. CORRODED. SHV - DURING C-CHECK MAINTENANCE FOUND 4 NUT PLATES LOCATED AT BOTTOM OF MAIN DOOR CORRODED. MAINTENANCE REPAIRED NUT PLATES AT THE BOTTOM OF THE MAIN DOOR IAW - [SDR C2XA07RI006](https://openairdocs.org/sdr/C2XA07RI006), Feb 20, 2007: ENGINE. CONTAMINATED. FLT 4930 - IAD CREW REJECTED TAKE OFF DUE TO SMOKE IN COCKPIT. SMOKE OCCURRED WHEN THRUST WAS ADVANCED TO DETENT. SMOKE CLEARED WHEN THRUST WAS REDUCED AND AFTE - [SDR C2XA07TY007](https://openairdocs.org/sdr/C2XA07TY007), Feb 20, 2007: ENGINE. DAMAGED. TYS A/C HAD SMOKE ON CLIMBOUT AND THEN CLEARED. THEN ANOTHER TIME ON LEVELING OFF, AGAIN LEFT. A/C WAS CHECKED OUT AND FERRIED TO TYS. MAINTENANCE REMOVED AND R - [SDR C2XA07CL015](https://openairdocs.org/sdr/C2XA07CL015), Jan 26, 2007: ENGINE. CONTAMINATED. CLE FLIGHT 2965 THE CREW REPORTED CLIMBING THRU 7500 FT. THE F/A REPORTED SMOKE FILLING THE CABIN. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT INCIDEN - [SDR C2XA07IA027](https://openairdocs.org/sdr/C2XA07IA027), Jan 24, 2007: RELAY. SHORTED. FLIGHT 1281, PILOT REPORTED THAT A LAV SMOKE INDICATION ILLUMINATED DURING CLIMB OUT. A VISUAL INSPECTION WAS PERFORMED AND SMOKE, FIRE AND/OR UNUSUAL ODORS WER - [SDR C2XA06CL050](https://openairdocs.org/sdr/C2XA06CL050), May 13, 2006: INVERTER. INOPERATIVE. CLE FLIGHT 2808 THE CREW REPORTED THE FORWARD EMERGENCY SIGN OVER THE F/A'S SEAT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 INVERTER. OPERATIO - [SDR C2XA05CL075](https://openairdocs.org/sdr/C2XA05CL075), Aug 31, 2005: LIGHT. INOPERATIVE. DURING ROUTINE MAINTENANCE, THE EMERGENCY LIGHT ON THE SERVICE DOOR WAS INTERMITTENT. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY ON THE SER - [SDR C2XA05SH051](https://openairdocs.org/sdr/C2XA05SH051), Jun 11, 2005: FIREWALL. CHAFED. SHV - DURING C-CHECK RIVET HEAD WEAR MARKS ON BOTTOM RT SIDE OF APU FIREWALL. MAINTENANCE REPAIRED THE APU FIREWALL AT FRAME 81 IAW EC 5310-01337. AIRCRAFT WAS - [SDR C2XA05SH050](https://openairdocs.org/sdr/C2XA05SH050), Jun 11, 2005: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT VARIOUS AREAS BETWEEN FRAMES 35-39. MAINTENANCE REPAIRED LT OMEGA BEAM BETWEEN FRAME 38 - FRAME 39 PER EC 53 - [SDR C2XA05SH049](https://openairdocs.org/sdr/C2XA05SH049), Jun 11, 2005: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM HAS AREAS OF CORROSION BETWEEN FRAMES 45 & 53. MAINTENANCE REPAIRED LT OMEGA BEAM AT FRAME 49 PER EC 5320-01247, NO FURTHER A - [SDR C2XA05SH048](https://openairdocs.org/sdr/C2XA05SH048), Jun 11, 2005: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM HAS VARIOUS AREAS OF CORROSION BETWEEN FRAMES 29-36. MAINTENANCE REPAIRED LT OMEGA BEAM AT FRAME 33 - FRAME 34 PER EC 5320-01 - [SDR C2XA05SH047](https://openairdocs.org/sdr/C2XA05SH047), Jun 11, 2005: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT VARIOUS AREAS BETWEEN FRAMES 22 & 29. MAINTENANCE REPAIRED LT OMEGA BEAM AT FRAME 29 PER EC 5320-01247, NO F - [SDR C2XA05SH046](https://openairdocs.org/sdr/C2XA05SH046), Jun 11, 2005: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT VARIOUS AREAS BETWEEN FRAMES 52 & 59. MAINTENANCE REPAIRED LT OMEGA BEAM AT FRAME 54 AND AT FRAME 59 PER EC - [SDR C2XA05SH045](https://openairdocs.org/sdr/C2XA05SH045), Jun 11, 2005: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION FR 39-45. MAINTENANCE REPAIRED LT OMEGA BEAM AT FR 44 PER EC 5320-01247, NO FURTHER ACTION REQUIRED. THE AIRCRA - [SDR C2XA05IA055](https://openairdocs.org/sdr/C2XA05IA055), Apr 18, 2005: CONNECTOR. DIRTY. IAH - FLIGHT 2638, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHT ABOVE THE FA SEAT WAS INOPERATIVE. MAINTENANCE CLEANED THE ELECTRICAL CONNECTORS, OPERATIONAL - [SDR C2XA04IA135](https://openairdocs.org/sdr/C2XA04IA135), Oct 19, 2004: WIRE. LOOSE. CREW REPORTED THE OVERHEAD EMERGENCY EXIT LIGHT AT THE EXIT ROW WAS INOPERATIVE. RESECURRED THE WIRE AT THE LIGHT. OPERATIONALLY CHECK OK. AIRCRAFT RETURNED TO - [SDR C2XA04CL058](https://openairdocs.org/sdr/C2XA04CL058), May 21, 2004: SIGN. INOPERATIVE. THE CREW REPORTED THE EMERGENCY EXIT SIGN ABOVE THE FLIGHT ATTENDANT JUMPSEAT WAS INOPERATIVE. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE EMERGENCY LIGHT S - [SDR C2XA04SH202](https://openairdocs.org/sdr/C2XA04SH202), Apr 4, 2004: WIRE HARNESS. PINCHED. IAH - FLIGHT 2064 THE CREW REPORTED A STRONG ELECTRIC BURNING ODOR WHEN THE WINDSHIELD HEAT WAS SELECTED ON. THE AIRCRAFT LANDED AT IAH WHERE IT LANDED WITHOUT - [SDR C2XA03CL168](https://openairdocs.org/sdr/C2XA03CL168), Sep 20, 2003: INVERTER. INOPERATIVE. DURING ROUTINE MAINTENANCE THE CENTER FUSELAGE CABIN EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE CENTER FUSELAGE CABIN EMERGENCY CEILING LIG - [SDR C2XA03BT094](https://openairdocs.org/sdr/C2XA03BT094), Sep 15, 2003: LIGHT. FAULTY. CREW REPORTED, OVERHEAD EMERGENCY EXIT LIGHT AFT SIDE, WILL NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ON THE AFT SIDE IAW EMB145 All 90: https://openairdocs.org/deregistered/N14942-2016-11-15/reports.md ## Other aircraft with N14942 - [Cancelled 1948-07-27](https://openairdocs.org/deregistered/N14942-1948-07-27): Lockheed ELECTRA 10-A, S/N 1031. Owner: [Executive Transport Corp](https://openairdocs.org/faa-owner/EXECUTIVE%20TRANSPORT%20CORP), [Dallas, TX](https://openairdocs.org/faa-place/TX/Dallas) --- 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.