# Service difficulty reports: N14937, cancelled Oct 4, 2016 A list on [N14937, cancelled Oct 4, 2016](https://openairdocs.org/deregistered/N14937-2016-10-04.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 3 · 107 reports - [SDR ASOA20140517076](https://openairdocs.org/sdr/ASOA20140517076.md): Beam · corroded · May 17, 2014 · N14937 · Emb EMB145LR · Fuselage Main, Structure > DURING C-CHECK THE LT WINDSHIELD LOWER FRONT CUTOUT BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED BUSHING REPAIRS IAW EC5310-01782. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20140513063](https://openairdocs.org/sdr/ASOA20140513063.md): Stringer · cracked · May 13, 2014 · N14937 · Emb EMB145LR · Fuselage Main, Longeron/Stringer > 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 SERVICE. - [SDR ASOA20140513062](https://openairdocs.org/sdr/ASOA20140513062.md): Bracket · gouged · May 13, 2014 · N14937 · Emb EMB145LR · Fuselage Miscellaneous Structure > 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 APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20140513061](https://openairdocs.org/sdr/ASOA20140513061.md): Skin · corroded · May 13, 2014 · N14937 · Emb EMB145LR · Fuselage Main, Plate/Skin > 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 ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20140513060V](https://openairdocs.org/sdr/ASOA20140513060V.md): Shear Tie · corroded · May 13, 2014 · N14937 · Emb EMB145LR · Fuselage Internal Mounting Structure > 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. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20140513059](https://openairdocs.org/sdr/ASOA20140513059.md): Fitting · cracked · May 13, 2014 · N14937 · Emb EMB145LR · Engine Mount Section > 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. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20140401056](https://openairdocs.org/sdr/ASOA20140401056.md): Flapper Valve · leaking · Apr 1, 2014 · N14937 · Emb EMB145EP · Aircraft Fuel Distribution System > 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 LANDED WITHOUT INCIDENT WHERE MAINTENANCE R & R THE OTBD FLAPPER VALVE IN THE LT WING, LEAK CHECKED - [SDR ASOA20140115010](https://openairdocs.org/sdr/ASOA20140115010.md): Relay · inoperative · Jan 15, 2014 · N14937 · Emb EMB145EP · Pitot/Static Anti-Ice System > 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 MAINTENANCE INSPECTED THE ACFT, R & R RELAY K0055, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR - [SDR ASOA20140106003](https://openairdocs.org/sdr/ASOA20140106003.md): Skin · cracked · Jan 6, 2014 · N14937 · Emb EMB145EP · Fuselage Main, Plate/Skin > 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 AND INSTALLED A FILLER/ TRIPLER REPAIR, LEAK CHECKED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RE - [SDR ASOA20130820154](https://openairdocs.org/sdr/ASOA20130820154.md): Inverter · inoperative · Aug 20, 2013 · N14937 · Emb EMB145EP · Emergency Lighting > 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 DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20130610173](https://openairdocs.org/sdr/ASOA20130610173.md): Tire · failed · Jun 10, 2013 · N14937 · Emb EMB145ER · Tire > 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.md): Skin · cracked · Apr 19, 2013 · N14937 · Emb EMB145EP · Fuselage Main, Plate/Skin > 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 REPAIR ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5330-02501, AND THE ACFT WAS APPROVED FOR RETURN TO S - [SDR ASOA20130419057H](https://openairdocs.org/sdr/ASOA20130419057H.md): Skin · cracked · Apr 19, 2013 · N14937 · Emb EMB145EP · Fuselage Main, Plate/Skin > 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 ENGINEERING CHANGE/REPAIR EC5330-02353, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20130419056H](https://openairdocs.org/sdr/ASOA20130419056H.md): Skin · cracked · Apr 19, 2013 · N14937 · Emb EMB145EP · Fuselage Main, Plate/Skin > 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 PERFORMED A DOUBLER REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE ON 04/22/13. - [SDR C2XA11IA056](https://openairdocs.org/sdr/C2XA11IA056.md): Element · inoperative · Mar 16, 2011 · N14937 · Emb EMB145EP · Fire Detection > 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 REPLACED THE NUMBER TWO ENGINE FIRE DETECTOR ELEMENT, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCR - [SDR C2XA11IA010](https://openairdocs.org/sdr/C2XA11IA010.md): Windshield · arced · Jan 9, 2011 · N14937 · Emb EMB145EP · Flight Compartment Windows > LCH - FLIGHT 2555, THE CREW REPORTED THAT THE CAPTAINS WINDSHIELD WAS ARCING IN FLIGHT, THE AIRCRAFT DIVERTED TO LCH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDSHIELD, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRC - [SDR C2XA10IA300](https://openairdocs.org/sdr/C2XA10IA300.md): Ballast · overheated · Nov 19, 2010 · N14937 · Emb EMB145EP · Passenger Compartment Lighting > IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED AN ELECTRICAL BURNING SMELL IN THE CABIN. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE LIGHT BALLAST ABOVE SEAT 14B/C, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED F - [SDR C2XA10IA293](https://openairdocs.org/sdr/C2XA10IA293.md): Ballast · overheated · Nov 11, 2010 · N14937 · Emb EMB145EP · Passenger Compartment Lighting > 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 WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LIGHT BALLAST AT ROW 12, OPERATIONALLY TESTED WI - [SDR C2XA10IA292](https://openairdocs.org/sdr/C2XA10IA292.md): Smoke Detector · malfunctioned · Nov 11, 2010 · N14937 · Emb EMB145EP · Smoke Detection > IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED A BAGGAGE SMOKE WARNING. THE CREW VERIFIED NO SMOKE, AND MAINTENANCE INSPECTED THE AIRCRAFT AND RESET THE BAGGAGE SMOKE DETECTOR SYSTEM, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FO - [SDR C2XA10IA153](https://openairdocs.org/sdr/C2XA10IA153.md): Light · overheated · May 18, 2010 · N14937 · Emb EMB145EP · Passenger Compartment Lighting > 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 AT 11A, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10IA151](https://openairdocs.org/sdr/C2XA10IA151.md): Hose · unknown · May 18, 2010 · N14937 · Emb EMB145EP · Air Distribution System > 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 AT 11A, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10IA150](https://openairdocs.org/sdr/C2XA10IA150.md): Ballast · overheated · May 18, 2010 · N14937 · Emb EMB145EP · Passenger Compartment Lighting > IAH - DURING POST FLIGHT INSPECTION, AN ELECTRICAL SMELL MID CABIN WAS REPORTED WITH NO SMOKE OBSERVED. MAINTENANCE REMOVED AND REPLACED THE BALLAST AT 11A, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10IA132](https://openairdocs.org/sdr/C2XA10IA132.md): Connector · dirty · Apr 26, 2010 · N14937 · Emb EMB145EP · Light System Wiring > LRD - FLIGHT 2616, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE LAST THREE AISLE PATH LIGHT STRIPS AFT OF ROW 12 WERE INOPERATIVE. CONTRACT MAINTENANCE CLEANED THE CONNECTOR ON THE EMERGENCY LIGHT POWER SUPPLY, OPERATIONALLY TESTED WITH NO DEFECTS. - [SDR C2XA10IA125](https://openairdocs.org/sdr/C2XA10IA125.md): Battery Pack · discharged · Apr 19, 2010 · N14937 · Emb EMB145EP · Emergency Lighting > 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 THE NUMBER FOUR EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAF - [SDR C2XA09IA307](https://openairdocs.org/sdr/C2XA09IA307.md): Inverter · inoperative · Dec 2, 2009 · N14937 · Emb EMB145EP · Emergency Lighting > LCH - DURING MAINTENANCE INSPECTION THE AFT OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER SIX EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO - [SDR C2XA09IA200](https://openairdocs.org/sdr/C2XA09IA200.md): Battery Pack · discharged · Aug 12, 2009 · N14937 · Emb EMB145EP · Emergency Lighting > IAH - DURING MAINTENANCE INSPECTION THE AFT THREE AISLE PATH LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETU - [SDR C2XA09TY186](https://openairdocs.org/sdr/C2XA09TY186.md): Floor Support · corroded · Jul 27, 2009 · N14937 · Emb EMB145EP · Fuselage Miscellaneous Structure > 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 PREVIOUS REPAIR AND INSTALLED A NEW RAMP ANGLE AND A NEW REPAIR FOR THE OMEGA BEAM IAW 135/145 SRM - [SDR C2XA09TY185](https://openairdocs.org/sdr/C2XA09TY185.md): Sill · corroded · Jul 27, 2009 · N14937 · Emb EMB145EP · Fuselage Miscellaneous Structure > 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 WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK. - [SDR C2XA09TY184](https://openairdocs.org/sdr/C2XA09TY184.md): Sill · corroded · Jul 27, 2009 · N14937 · Emb EMB145EP · Fuselage Miscellaneous Structure > 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 CHECK. - [SDR C2XA09TY179](https://openairdocs.org/sdr/C2XA09TY179.md): Floor Support · corroded · Jul 24, 2009 · N14937 · Emb EMB145EP · Fuselage Miscellaneous Structure > 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 ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK. - [SDR C2XA09TY178](https://openairdocs.org/sdr/C2XA09TY178.md): Floor Support · corroded · Jul 24, 2009 · N14937 · Emb EMB145EP · Fuselage Miscellaneous Structure > 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 SRM 53-21-10. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK. - [SDR C2XA09TY177](https://openairdocs.org/sdr/C2XA09TY177.md): Floor Support · corroded · Jul 24, 2009 · N14937 · Emb EMB145EP · Fuselage Miscellaneous Structure > 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 WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK. - [SDR C2XA09TY176](https://openairdocs.org/sdr/C2XA09TY176.md): Floor Support · corroded · Jul 24, 2009 · N14937 · Emb EMB145EP · Fuselage Miscellaneous Structure > 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 RELEASED AT THE END OF THE CHECK. - [SDR C2XA09TY175](https://openairdocs.org/sdr/C2XA09TY175.md): Floor Support · corroded · Jul 24, 2009 · N14937 · Emb EMB145ER · Fuselage Miscellaneous Structure > 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 IAW CPM 51-21-04-05-06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE C-CHECK - [SDR C2XA09TY174](https://openairdocs.org/sdr/C2XA09TY174.md): Sill · corroded · Jul 24, 2009 · N14937 · Emb EMB145EP · Fuselage Miscellaneous Structure > 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 SRM 53-21-10. ALL WORK WAS DONE AND WILL BE RELEASED AT THE END OF THE CHECK. - [SDR C2XA09TY169](https://openairdocs.org/sdr/C2XA09TY169.md): Fitting · chafed · Jul 22, 2009 · N14937 · Emb EMB145EP · Vertical Stabilizer Miscellaneous Structure > 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 THE FITTING AND REAMED THE FOUR HOLES AND BUSHINGS INSTALLED. THEN REINSTALL THE FITTING IAW EC 55 - [SDR C2XA09TY171](https://openairdocs.org/sdr/C2XA09TY171.md): Fitting · cracked · Jul 17, 2009 · N14937 · Emb EMB145EP · Fuselage Miscellaneous Structure > 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 SECTION OF FRM 10, REINSTALLED CONNECTING GUSSET. REPLACED SHEAR CLIP. - [SDR C2XA09TY170](https://openairdocs.org/sdr/C2XA09TY170.md): Sign · inoperative · Jul 17, 2009 · N14937 · Emb EMB145EP · Emergency Lighting > 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.md): Sill · corroded · Jul 15, 2009 · N14937 · Emb EMB145EP · Fuselage Miscellaneous Structure > 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 SILL IAE SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK. - [SDR C2XA09TY156](https://openairdocs.org/sdr/C2XA09TY156.md): Sill · corroded · Jul 15, 2009 · N14937 · Emb EMB145EP · Fuselage Miscellaneous Structure > 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 ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK. - [SDR C2XA09TY152](https://openairdocs.org/sdr/C2XA09TY152.md): Flange · corroded · Jul 13, 2009 · N14937 · Emb EMB145ER · Engine Air Intake System > 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 EC5420-01158. - [SDR C2XA09TY150](https://openairdocs.org/sdr/C2XA09TY150.md): Bushing · missing · Jul 12, 2009 · N14937 · Emb EMB145ER · Rudder Structure > 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.md): Door Frame · corroded · Jul 10, 2009 · N14937 · Emb EMB145EP · Fuselage Main, Structure > 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.md): Cap · corroded · Jul 8, 2009 · N14937 · Emb EMB145EP · Fuselage Miscellaneous Structure > RT LAV TOP CAP HAS CORROSION. BLENDED MINOR CORROSION, ALODINED, PRIMED, AND PAINTED. - [SDR C2XA09TY146](https://openairdocs.org/sdr/C2XA09TY146.md): Web · cracked · Jul 8, 2009 · N14937 · Emb EMB145EP · Nacelle/Pylon Miscellaneous Structure > 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.md): Cap · corroded · Jul 8, 2009 · N14937 · Emb EMB145EP · Fuselage Miscellaneous Structure > LT LAV TOP CAP CORRDED, WITHIN LIMITS, BLENDED, ALODINED, PRIMED, AND PAINTED. - [SDR C2XA09TY144](https://openairdocs.org/sdr/C2XA09TY144.md): Sill · corroded · Jul 8, 2009 · N14937 · Emb EMB145EP · Fuselage Miscellaneous Structure > CORROSION ON LT FLOOR SILL AT FRM 43. REMOVED AND REPLACED LT FLOOR SILL. - [SDR C2XA09TY143](https://openairdocs.org/sdr/C2XA09TY143.md): Sill · corroded · Jul 8, 2009 · N14937 · Emb EMB145EP · Fuselage Miscellaneous Structure > RT FLOOR SILL CORRODED BETWEEN FRM 29-35. FLOOR SILL WAS REMOVED AND REPLACED. - [SDR C2XA09TY142](https://openairdocs.org/sdr/C2XA09TY142.md): Sill · corroded · Jul 8, 2009 · N14937 · Emb EMB145EP · Fuselage Miscellaneous Structure > CORROSION ON LT FLOOR SILL FROM FRM 18-23. FLOOR SILL WAS REMOVED AND REPLACED. - [SDR C2XA09TY141](https://openairdocs.org/sdr/C2XA09TY141.md): Floor Support · corroded · Jul 8, 2009 · N14937 · Emb EMB145EP · Fuselage Miscellaneous Structure > CORROSION ON CENTER OMEGA BEAM AND STEP UP AT FRM 18. CORROSION WITHIN LIMITS. BLENDED OUT, ALODINED, PRIMED, AND PAINTED. Next page: https://openairdocs.org/deregistered/N14937-2016-10-04/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N14937' AND deregistration_id = 'N14937-2016-10-04' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N14937-2016-10-04/reports --- 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.