# N14937: 1997 Embraer EMB-145EP, registration cancelled 2016-10-04 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 4, 2016 - Exported to: Poland - 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: 145026 - Year built: 1997 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 27, 2005 - Certificate issued: August 31, 2016 - Last registry action: August 31, 2016 - Mode S code: A0C700 - Owner when cancelled: [Strong Tower Services LLC Trustee](https://openairdocs.org/faa-owner/STRONG%20TOWER%20SERVICES%20LLC%20TRUSTEE) - Location: [New Castle, DE](https://openairdocs.org/faa-place/DE/New%20Castle) - Owner type: Corporation - Owner's area on the map: 39.6466° N, 75.6048° W: Placed by OpenAirDocs at the center of ZIP code 19720, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N14937 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14937 - Page: https://openairdocs.org/deregistered/N14937-2016-10-04 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 (107, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASOA20140517076](https://openairdocs.org/sdr/ASOA20140517076), May 17, 2014: BEAM. CORRODED. DURING C-CHECK THE LT WINDSHIELD LOWER FRONT CUTOUT BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED BUSHING REPAIRS IAW EC5310-01 - [SDR ASOA20140513063](https://openairdocs.org/sdr/ASOA20140513063), May 13, 2014: STRINGER. CRACKED. DURING C-CHECK STRINGER 6R WAS FOUND TO BE CRACKED BETWEEN FRAME 12-13. MAINTENANCE R & R THE STRINGER IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SER - [SDR ASOA20140513062](https://openairdocs.org/sdr/ASOA20140513062), May 13, 2014: BRACKET. GOUGED. DURING C-CHECK THE LT WINDSHIELD PILLAR BRACKET AT FRAME 10, STRINGER 5L, WAS FOUND TO BE GOUGED. MAINTENANCE R & R THE BRACKET IAW SRM 51-40-02. THE ACFT WAS A - [SDR ASOA20140513061](https://openairdocs.org/sdr/ASOA20140513061), May 13, 2014: SKIN. CORRODED. DURING C-CHECK THE CENTRAL FUSELAGE LOWER SKIN WAS FOUND TO BE CORRODED AT FRAME 21, STRINGERS 21L AND 21R. MAINTENANCE R & R THE SKIN IAW EC5330-02895. THE ACF - [SDR ASOA20140513060V](https://openairdocs.org/sdr/ASOA20140513060V), May 13, 2014: SHEAR TIE. CORRODED. DURING C-CHECK THE CARGO DOOR CUTOUT FWD SHEAR TIE WAS FOUND TO BE CORRODED AT FRAME 65, STRINGERS 15L-16L. MAINTENANCE R & R THE SHEAR CLIP IAW SRM 53-31-04. T - [SDR ASOA20140513059](https://openairdocs.org/sdr/ASOA20140513059), May 13, 2014: FITTING. CRACKED. DURING C-CHECK THE NR 2 ENGINE FORWARD LOWER YOKE FITTING WAS FOUND TO BE CRACKED AND VERIFIED WITH EDDY CURRENT. MAINTENANCE R & R THE FITTING IAW EC5450-01088 - [SDR ASOA20140401056](https://openairdocs.org/sdr/ASOA20140401056), Apr 1, 2014: FLAPPER VALVE. LEAKING. THE CREW REPORTED THAT PILOT REPORTED MASSIVE AMOUNTS OF FLUID LOSS JUST INBD OF THE LT AILERON DURING FLIGHT WITH A HEAVY SCENT OF FUEL IN THE AREA. THE ACFT L - [SDR ASOA20140115010](https://openairdocs.org/sdr/ASOA20140115010), Jan 15, 2014: RELAY. INOPERATIVE. CREW REPORTED A NR 2 PITOT HEAT INOPERATIVE ON EICAS ACCOMPANIED BY A FAINT ELECTRICAL ODOR ON FINAL APPROACH. THE ACFT LANDED WITHOUT INCIDENT, WHERE MAINTENAN - [SDR ASOA20140106003](https://openairdocs.org/sdr/ASOA20140106003), Jan 6, 2014: SKIN. CRACKED. DURING MAINTENANCE INSPECTION, THE COCKPIT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT THE UPPER AFT CORNER OF THE F/O DV WINDOW. MAINTENANCE REMOVED THE DAMAGE AN - [SDR ASOA20130820154](https://openairdocs.org/sdr/ASOA20130820154), Aug 20, 2013: INVERTER. INOPERATIVE. DURNG MX INSPECTION, SEVERAL FLOOR EMERGENCY LIGHT PROXIMITY STRIPS DID NOT ILLUMINATE. MX R & R THE NR 3 EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO - [SDR ASOA20130610173](https://openairdocs.org/sdr/ASOA20130610173), Jun 10, 2013: TIRE. FAILED. FLIGHT 4358. RT MLG NR 3 TIRE BLEW OUT AT V1 DAMAGING OTHER ITEMS. R & R NR 3 TIRE. - [SDR ASOA20130419058](https://openairdocs.org/sdr/ASOA20130419058), Apr 19, 2013: SKIN. CRACKED. DURING 5A INSP THE LAFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FR78 STR 09L AROUND 1 RIVET. MX REMOVED THE DAMAGED SECTION OF SKIN AND PERFORMED A DOUBLER REP - [SDR ASOA20130419057H](https://openairdocs.org/sdr/ASOA20130419057H), Apr 19, 2013: SKIN. CRACKED. DURING 5A INSPECTION, THE FUSELAGE SKIN AT FR 78 BELOW STR 1R WAS FOUND TO BE CRACKED. MX REMOVED THE DAMAGED SECTION, AND PERFORMED A DOUBLER REPAIR IAW ENGINE - [SDR ASOA20130419056H](https://openairdocs.org/sdr/ASOA20130419056H), Apr 19, 2013: SKIN. CRACKED. DURING 5A INSPECTION THE FUSELAGE CROWN SKIN WAS FOUND TO BE CRACKED ON THE LT SIDE BETWEEN THE WINDSHIELD AND DV WINDOW. MX REMOVED THA DAMAGED SECTION, AND PE - [SDR C2XA11IA056](https://openairdocs.org/sdr/C2XA11IA056), Mar 16, 2011: ELEMENT. INOPERATIVE. IAH - FLIGHT 2804 THE CREW REPORTED AN E2 FIRE DETECTOR FAIL MESSAGE IN FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLAC - [SDR C2XA11IA010](https://openairdocs.org/sdr/C2XA11IA010), Jan 9, 2011: WINDSHIELD. ARCED. LCH - FLIGHT 2555, THE CREW REPORTED THAT THE CAPTAINS WINDSHIELD WAS ARCING IN FLIGHT, THE AIRCRAFT DIVERTED TO LCH WHERE IT LANDED WITHOUT INCIDENT. MAINTENAN - [SDR C2XA10IA300](https://openairdocs.org/sdr/C2XA10IA300), Nov 19, 2010: BALLAST. OVERHEATED. IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED AN ELECTRICAL BURNING SMELL IN THE CABIN. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE LI - [SDR C2XA10IA293](https://openairdocs.org/sdr/C2XA10IA293), Nov 11, 2010: BALLAST. OVERHEATED. IAH - DURING CLIMB THE CREW REPORTED AN ELECTRICAL BURNING SMELL IN THE AIR BETWEEN THE CABIN AND FLIGHT DECK. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITH - [SDR C2XA10IA292](https://openairdocs.org/sdr/C2XA10IA292), Nov 11, 2010: SMOKE DETECTOR. MALFUNCTIONED. IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED A BAGGAGE SMOKE WARNING. THE CREW VERIFIED NO SMOKE, AND MAINTENANCE INSPECTED THE AIRCRAFT AND RESET THE BA - [SDR C2XA10IA153](https://openairdocs.org/sdr/C2XA10IA153), May 18, 2010: LIGHT. OVERHEATED. IAH - DURING MAINTENANCE INSPECTION A BURNING SMELL WAS NOTED AT SEAT 11A AREA. MAINTENANCE REMOVED AND REPLACED SIDEWALL LIGHTS FROM 10A-12A, AND GASPER HOSE A - [SDR C2XA10IA151](https://openairdocs.org/sdr/C2XA10IA151), May 18, 2010: HOSE. UNKNOWN. IAH - DURING MAINTENANCE INSPECTION A BURNING SMELL WAS NOTED AT SEAT 11A AREA. MAINTENANCE REMOVED AND REPLACED SIDEWALL LIGHTS FROM 10A-12A, AND GASPER HOSE A - [SDR C2XA10IA150](https://openairdocs.org/sdr/C2XA10IA150), May 18, 2010: BALLAST. OVERHEATED. IAH - DURING POST FLIGHT INSPECTION, AN ELECTRICAL SMELL MID CABIN WAS REPORTED WITH NO SMOKE OBSERVED. MAINTENANCE REMOVED AND REPLACED THE BALLAST AT 11A, OPE - [SDR C2XA10IA132](https://openairdocs.org/sdr/C2XA10IA132), Apr 26, 2010: CONNECTOR. DIRTY. LRD - FLIGHT 2616, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE LAST THREE AISLE PATH LIGHT STRIPS AFT OF ROW 12 WERE INOPERATIVE. CONTRACT MAINTENANC - [SDR C2XA10IA125](https://openairdocs.org/sdr/C2XA10IA125), Apr 19, 2010: BATTERY PACK. DISCHARGED. IAH - FLIGHT 2217, THE DURING POST FLIGHT THE CREW REPORTED THAT THE LAST THREE AISLE PATH LIGHT STRIPS WERE NOT ILLUMINATING. MAINTENANCE REMOVED AND REPLACED - [SDR C2XA09IA307](https://openairdocs.org/sdr/C2XA09IA307), Dec 2, 2009: INVERTER. INOPERATIVE. LCH - DURING MAINTENANCE INSPECTION THE AFT OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER SIX EMERGENCY - [SDR C2XA09IA200](https://openairdocs.org/sdr/C2XA09IA200), Aug 12, 2009: BATTERY PACK. DISCHARGED. IAH - DURING MAINTENANCE INSPECTION THE AFT THREE AISLE PATH LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGEN - [SDR C2XA09TY186](https://openairdocs.org/sdr/C2XA09TY186), Jul 27, 2009: FLOOR SUPPORT. CORRODED. TYS - A/C WAS IN A C-CHECK STATUS WHEN CORROSION WAS FOUND ON THE LEFT OMEGA BEAM AT FRAMES 20 AND 21. MAINTENANCE REPLACED THE PREVIOUS REPAIR BY REMOVING THE - [SDR C2XA09TY185](https://openairdocs.org/sdr/C2XA09TY185), Jul 27, 2009: SILL. CORRODED. TYS - A/C WAS IN A C-CHECK WHEN CORROSION WAS FOUND IN THE FLOOR SILL AT FRAME 24 THRU 30. MAINTENANCE REPLACED THE FLOOR SILL IAW EMB 135/145 SRM 51-40-02. ALL - [SDR C2XA09TY184](https://openairdocs.org/sdr/C2XA09TY184), Jul 27, 2009: SILL. CORRODED. TYS - A/C WAS IN A C-CHECK STATUS WHEN THE LEFT FLOOR SILL WAS FOUND CORRODED AT FRAME 30 THRU 35. ALL WORK WAS ACCOMPLISHED AND WAS RELEASED AT THE END OF THE - [SDR C2XA09TY179](https://openairdocs.org/sdr/C2XA09TY179), Jul 24, 2009: FLOOR SUPPORT. CORRODED. TYS - CORROSION WAS FOUND AROUND THE NUT PLATES ON THE FWD DIGITAL PLATE. MAINTENANCE REMOVED THE LITE CORROSION IAW EMB 135/145 SRM 51-21-10. ALL WORK WAS ACCO - [SDR C2XA09TY178](https://openairdocs.org/sdr/C2XA09TY178), Jul 24, 2009: FLOOR SUPPORT. CORRODED. TYS - CORROSION WAS FOUND AROUND THE NUT PLATES ON THE PAX DOOR ENTRYWAY AT THE AFT DIGITAL PLATE. MAINTENANCE BLENDED OUT THE LIGHT CORROSION IAW EMB 135/145 S - [SDR C2XA09TY177](https://openairdocs.org/sdr/C2XA09TY177), Jul 24, 2009: FLOOR SUPPORT. CORRODED. TYS - CORROSION WAS FOUND ON THE CENTER OMEGA BEAM AT FRAME 22. MAINTENANCE BLENDED OUT THE CORROSION IAW EMB 135/145 SRM 51-40-01 AND CPM 51-21-04-05-06. ALL W - [SDR C2XA09TY176](https://openairdocs.org/sdr/C2XA09TY176), Jul 24, 2009: FLOOR SUPPORT. CORRODED. TYS - CORROSION WAS FOUND ON THE TOPCAP AT FRAME 20. MAINTENANCE REPLACED THE TOPCAP IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASE - [SDR C2XA09TY175](https://openairdocs.org/sdr/C2XA09TY175), Jul 24, 2009: FLOOR SUPPORT. CORRODED. TYS - CORROSION WAS FOUND ON THE RIGHT OMEGA BEAM AT FRAME 22 TOPCAP. MAINTENANCE REPLACED THE TOPCAP IAW EMB 135/145 SRM 51-40-07. ALODINED, PRIMED AND PAINTED - [SDR C2XA09TY174](https://openairdocs.org/sdr/C2XA09TY174), Jul 24, 2009: SILL. CORRODED. TYS - CORROSION WAS FOUND AROUND A NUT PLATE ON THE SERVICE DOOR AFT SILL. MAINTENANCE BLENDED OUT THE CORROSION, FABRICATED AND INSTALL A DOUBLER IAE EMB 145 S - [SDR C2XA09TY169](https://openairdocs.org/sdr/C2XA09TY169), Jul 22, 2009: FITTING. CHAFED. TYS - A/C CURRENTLY IN A C-CHECK STATUS WHEN INSPECTION FOUND CORROSION ON FRAME 75 VERTICAL STAB FITTING, 4 BOLT HOLES HAD SOME CORROSION. MAINTENANCE REMOVED - [SDR C2XA09TY171](https://openairdocs.org/sdr/C2XA09TY171), Jul 17, 2009: FITTING. CRACKED. CRACKED SHEAR CLIP AT FRM 10 JUST BELOW DV WINDOW. REMOVED CRACKED SHEAR CLIP, PARTIAL CRACKED FRM AND GUSSET AT FRM 10 JUST BELOW DV WINDOW. INSTALLED NEW SECT - [SDR C2XA09TY170](https://openairdocs.org/sdr/C2XA09TY170), Jul 17, 2009: SIGN. INOPERATIVE. SERVICE DOOR EXIT SIGN INOP. REMOVED AND REPLACED EXIT SIGN IAW EMB 145 AMM 33-50-09. OPS CHECK GOOD. - [SDR C2XA09TY161](https://openairdocs.org/sdr/C2XA09TY161), Jul 15, 2009: SILL. CORRODED. ACFT CURRENTLY IN A C-CHECK STATUS AND CORROSION WAS FOUND UNDER THE SVC DOOR THRESHOLD PLATE AROUND THE NUT PLATES. MX REMOVED AND REPLACED SVC DOOR THRESHOLD - [SDR C2XA09TY156](https://openairdocs.org/sdr/C2XA09TY156), Jul 15, 2009: SILL. CORRODED. ACFT IN C-CHECK AND THE RT FLOOR SILL WAS FOUND CORRODED BETWEEN FR 24 THRU FR 30. MX REMOVED AND REPLACED THE FLOOR SILL IAW SRM 51-40-02. ALL WORK WAS ACCOMPL - [SDR C2XA09TY152](https://openairdocs.org/sdr/C2XA09TY152), Jul 13, 2009: FLANGE. CORRODED. NR 2 ENG INLET MOUNTING FLANGE HAS CORROSION AT MOUNTING HOLES. CLEANED AREA AND FOUND 3 HOLES TO HAVE CORROSION. REPAIRED THE MOUNTING FLANGE HOLES IAW EC5420- - [SDR C2XA09TY150](https://openairdocs.org/sdr/C2XA09TY150), Jul 12, 2009: BUSHING. MISSING. RUDDER II UPPER CONTROL ROD UPPER MOUNT HAT BUSHING ON RUDDER MISSING. REMOVED AND REPLACED MOUNT IAW EC 5540-01028. - [SDR C2XA09TY149](https://openairdocs.org/sdr/C2XA09TY149), Jul 10, 2009: DOOR FRAME. CORRODED. CORROSION ON AFT LOWER END OF SERVICE DOOR CUT OUT FRAME. DOUBLER WAS MADE FROM A SPARE FRAME AND INSTALLED IAW EC 5310-01373. - [SDR C2XA09TY147](https://openairdocs.org/sdr/C2XA09TY147), Jul 8, 2009: CAP. CORRODED. RT LAV TOP CAP HAS CORROSION. BLENDED MINOR CORROSION, ALODINED, PRIMED, AND PAINTED. - [SDR C2XA09TY146](https://openairdocs.org/sdr/C2XA09TY146), Jul 8, 2009: WEB. CRACKED. NR 1 ENGINE FWD/LWR YOKE WEBBING CRACKED. REMOVED AND REPLACED NR 1 ENGINE FWD/LWR YOKE WEBBING. CLOSED - [SDR C2XA09TY145](https://openairdocs.org/sdr/C2XA09TY145), Jul 8, 2009: CAP. CORRODED. LT LAV TOP CAP CORRDED, WITHIN LIMITS, BLENDED, ALODINED, PRIMED, AND PAINTED. - [SDR C2XA09TY144](https://openairdocs.org/sdr/C2XA09TY144), Jul 8, 2009: SILL. CORRODED. CORROSION ON LT FLOOR SILL AT FRM 43. REMOVED AND REPLACED LT FLOOR SILL. - [SDR C2XA09TY143](https://openairdocs.org/sdr/C2XA09TY143), Jul 8, 2009: SILL. CORRODED. RT FLOOR SILL CORRODED BETWEEN FRM 29-35. FLOOR SILL WAS REMOVED AND REPLACED. - [SDR C2XA09TY142](https://openairdocs.org/sdr/C2XA09TY142), Jul 8, 2009: SILL. CORRODED. CORROSION ON LT FLOOR SILL FROM FRM 18-23. FLOOR SILL WAS REMOVED AND REPLACED. - [SDR C2XA09TY141](https://openairdocs.org/sdr/C2XA09TY141), Jul 8, 2009: FLOOR SUPPORT. CORRODED. CORROSION ON CENTER OMEGA BEAM AND STEP UP AT FRM 18. CORROSION WITHIN LIMITS. BLENDED OUT, ALODINED, PRIMED, AND PAINTED. All 107: https://openairdocs.org/deregistered/N14937-2016-10-04/reports.md ## FAA accident and incident reports (1) 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 19990525041749I](https://openairdocs.org/incident/19990525041749I), May 25, 1999: Emb EMB145ER (N14937), Wichita, KS. (-23)Hung start occurred during start of right engine off of an air bottle at Wichita mid Continent airport. A flame was reported in the exhaust by ground… --- 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.