# Service difficulty reports: N14939, cancelled Aug 13, 2015 A list on [N14939, cancelled Aug 13, 2015](https://openairdocs.org/deregistered/N14939-2015-08-13.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 · 135 reports - [SDR ASOA20140801100](https://openairdocs.org/sdr/ASOA20140801100.md): Light · inoperative · Aug 1, 2014 · N14939 · Emb EMB145EP · Emergency Lighting > DURING PREFLIGHT INSPECTION, THE CREW REPORTED EXIT ROW EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE R & R THE AFFECTED LIGHT ASSEMBLY, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20140318066](https://openairdocs.org/sdr/ASOA20140318066.md): Frame · cracked · Mar 18, 2014 · N14939 · Emb EMB145EP · Passenger/Crew Doors > 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.md): Channel · corroded · Mar 18, 2014 · N14939 · Emb EMB145EP · Fuselage Miscellaneous Structure > 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.md): Floorbeam · cracked · Mar 18, 2014 · N14939 · Emb EMB145EP · Fuselage Main, Floor Beam > FLOORBEAM FRAME 61 NUTPLATE HOLE CRACKED. R & R TEE ON FLOORBEAM IAW SRM 51-40-02. - [SDR ASOA20140318063](https://openairdocs.org/sdr/ASOA20140318063.md): Shear Tie · cracked · Mar 18, 2014 · N14939 · Emb EMB145EP · Fuselage Internal Mounting Structure > 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.md): Shear Tie · cracked · Mar 18, 2014 · N14939 · Emb EMB145EP · Fuselage Internal Mounting Structure > 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.md): Attach Angle · cracked · Mar 18, 2014 · N14939 · Emb EMB145EP · Fuselage Main, Attach Fittings > 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.md): Channel · cracked · Mar 18, 2014 · N14939 · Emb EMB145EP · Fuselage Miscellaneous Structure > 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.md): Channel · corroded · Mar 18, 2014 · N14939 · Emb EMB145EP · Fuselage Miscellaneous Structure > 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.md): Floor Support · chafed · Mar 18, 2014 · N14939 · Emb EMB145EP · Fuselage Miscellaneous Structure > 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.md): Shear Tie · cracked · Mar 18, 2014 · N14939 · Emb EMB145EP · Fuselage Internal Mounting Structure > FRAME 46 SHEAR TIE CRACKED. - [SDR ASOA20140318056](https://openairdocs.org/sdr/ASOA20140318056.md): Floor Support · corroded · Mar 18, 2014 · N14939 · Emb EMB145EP · Fuselage Miscellaneous Structure > 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.md): Floor Support · cracked · Mar 18, 2014 · N14939 · Emb EMB145EP · Fuselage Miscellaneous Structure > RT OMEGA BEAM SUPPORT FLANGE CRACKED NEAR FOOT RADIUS AT FRAME 47 ON OTBD SIDE OF BEAM. - [SDR ASOA20140318054](https://openairdocs.org/sdr/ASOA20140318054.md): Channel · corroded · Mar 18, 2014 · N14939 · Emb EMB145ER · Fuselage Miscellaneous Structure > 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, REV ORIGINAL. - [SDR ASOA20140318053T](https://openairdocs.org/sdr/ASOA20140318053T.md): Channel · corroded · Mar 18, 2014 · N14939 · Emb EMB145ER · Fuselage Miscellaneous Structure > 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.md): Shear Tie · cracked · Mar 18, 2014 · N14939 · Emb EMB145ER · Fuselage Internal Mounting Structure > 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.md): Floor Support · cracked · Mar 18, 2014 · N14939 · Emb EMB145ER · Fuselage Miscellaneous Structure > 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.md): Gcu · malfunctioned · Aug 30, 2013 · N14939 · Emb EMB145EP · AC Generator-Alternator > 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 IN THE COCKPIT) AFTER THE BANG. THE ACFT PERFORMED AN EMERGENCY LANDING IN BPT WITHOUT INCIDENT. - [SDR ASOA20130830157](https://openairdocs.org/sdr/ASOA20130830157.md): Starter Gen · malfunctioned · Aug 30, 2013 · N14939 · Emb EMB145EP · Starter-Generator > 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 IN THE COCKPIT, AFTER THE BANG. THE ACFT PERFORMED AN EMERGENCY LANDING WITHOUT INCIDENT. MX INSPE - [SDR ASOA20130209010H](https://openairdocs.org/sdr/ASOA20130209010H.md): Skin · cracked · Feb 9, 2013 · N14939 · Emb EMB145EP · Fuselage Main, Plate/Skin > 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 OF A DOUBLER IAW EC5330-02353. - [SDR ASOA20120323043](https://openairdocs.org/sdr/ASOA20120323043.md): Cdu · shorted · Mar 23, 2012 · N14939 · Emb EMB145EP · Flight Management Computing Hardware System > 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, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20120229029](https://openairdocs.org/sdr/ASOA20120229029.md): Sensor · inoperative · Feb 29, 2012 · N14939 · Emb EMB145EP · Landing Gear Brake System > 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 TO THE GATE WHERE MX INSPECTED THE ACFT R & R A FAULTY BRAKE TEMP SENSOR, OPERATIONALLY TESTED WITH - [SDR ASOA2011112600005](https://openairdocs.org/sdr/ASOA2011112600005.md): Skin · damaged · Nov 26, 2011 · N14939 · Emb EMB145ER · Fuselage Main, Plate/Skin > 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. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA2011112600004](https://openairdocs.org/sdr/ASOA2011112600004.md): Skin · cracked · Nov 26, 2011 · N14939 · Emb EMB145ER · Fuselage Main, Plate/Skin > 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 EC5330-02501 ORIG. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA2011112600003](https://openairdocs.org/sdr/ASOA2011112600003.md): Skin · cracked · Nov 26, 2011 · N14939 · Emb EMB145ER · Fuselage Main, Plate/Skin > 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. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA201111260002](https://openairdocs.org/sdr/ASOA201111260002.md): Skin · cracked · Nov 26, 2011 · N14939 · Emb EMB145LR · Fuselage Main, Plate/Skin > 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 SERVICE. - [SDR ASOA201111261009](https://openairdocs.org/sdr/ASOA201111261009.md): Threshold · corroded · Nov 26, 2011 · N14939 · Emb EMB145ER · Fuselage Miscellaneous Structure > 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.md): Skin · cracked · Nov 26, 2011 · N14939 · Emb EMB145ER · Fuselage Main, Plate/Skin > 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 EC5330-02501. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA201111261006](https://openairdocs.org/sdr/ASOA201111261006.md): Skin · cracked · Nov 26, 2011 · N14939 · Emb EMB145ER · Fuselage Main, Plate/Skin > 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 EC5330-02353. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA11IA244](https://openairdocs.org/sdr/C2XA11IA244.md): Indication Sys · malfunctioned · Oct 29, 2011 · N14939 · Emb EMB145EP · Fuel Indicating System > 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 TESTED THE FUEL QUANTITY SYSTEM WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN T - [SDR C2XA11IA129](https://openairdocs.org/sdr/C2XA11IA129.md): Bracket · broken · Jun 24, 2011 · N14939 · Emb EMB145EP · Elevator Tab Control System > 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. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE SPRING TAB FAIRING BRACKET, OPERATIONALL - [SDR C2XA11IA078](https://openairdocs.org/sdr/C2XA11IA078.md): Computer · faulty · May 1, 2011 · N14939 · Emb EMB145EP · Integrated Flight System > 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. MAINTENANCE REMOVED AND REPLACED THE NR 1 AHRS COMPUTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE A - [SDR C2XA11IA059](https://openairdocs.org/sdr/C2XA11IA059.md): Engine · vibration · Mar 21, 2011 · N14939 · Emb EMB145EP · Engine (Turbine/Turboprop) > 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 RANGE, RETURNED AIRCRAFT TO CLIMB POWER AND VIBRATION STABILIZED BETWEEN 2.0 AND 2.4 IPS. THE AIRCRAFT - [SDR C2XA11IA007](https://openairdocs.org/sdr/C2XA11IA007.md): Light · overheated · Jan 3, 2011 · N14939 · Emb EMB145EP · Passenger Compartment Lighting > 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 SOCKET AT ROW 5A LATERAL LIGHT. MAINTENANCE REMOVED THE BULB AND PLACED THE LIGHT ON MEL, AND THE AIR - [SDR C2XA10IA089](https://openairdocs.org/sdr/C2XA10IA089.md): Ecu · inoperative · Mar 7, 2010 · N14939 · Emb EMB145EP · Trailing Edge Flap Control System > 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 THE FLAP ELECTRONIC CONTROL UNIT (FECU), OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WA - [SDR C2XA09SH343](https://openairdocs.org/sdr/C2XA09SH343.md): Fitting · cracked · Oct 13, 2009 · N14939 · Emb EMB145EP · Engine Mount Section > 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 SERVICE. - [SDR C2XA09IA216](https://openairdocs.org/sdr/C2XA09IA216.md): Splice · broken · Aug 27, 2009 · N14939 · Emb EMB145EP · Light System Wiring > IAH - DURING MAINTENANCE INSPECTION THE AFT SECTION OF AISLE PATH LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BROKEN SPLICES, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09IA178](https://openairdocs.org/sdr/C2XA09IA178.md): Light · inoperative · Jul 13, 2009 · N14939 · Emb EMB145EP · Emergency Lighting > IAH - FLIGHT 2115 - DURING POST FLIGHT INSPECTION THE LEFT FORWARD WING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SE - [SDR C2XA09TY137A](https://openairdocs.org/sdr/C2XA09TY137A.md): Socket · broken · Jul 4, 2009 · N14939 · Emb EMB145EP · Emergency Lighting > 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.md): Fan · inoperative · Jun 10, 2009 · N14939 · Emb EMB145EP · Integrated Flight System > 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 REPLACED THE NR 1 AHRS FAN, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETU - [SDR C2XA09CL075](https://openairdocs.org/sdr/C2XA09CL075.md): Turbine Wheel · cracked · May 27, 2009 · N14939 · Emb EMB145EP · Turbine Section > 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 ULTRASOUND INSPECTION. THE NR 2 ENGINE WAS REPLACED. - [SDR C2XA09SH169](https://openairdocs.org/sdr/C2XA09SH169.md): Frame · damaged · May 24, 2009 · N14939 · Emb EMB145EP · Fuselage Main, Frame > 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. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09SH168](https://openairdocs.org/sdr/C2XA09SH168.md): Frame · damaged · May 24, 2009 · N14939 · Emb EMB145EP · Fuselage Main, Frame > 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. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. - [SDR C2XA09SH167](https://openairdocs.org/sdr/C2XA09SH167.md): Beam · corroded · May 24, 2009 · N14939 · Emb EMB145EP · Fuselage Miscellaneous Structure > 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 AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. - [SDR C2XA09SH166](https://openairdocs.org/sdr/C2XA09SH166.md): Floor Support · corroded · May 24, 2009 · N14939 · Emb EMB145EP · Fuselage Miscellaneous Structure > 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 WAS APPROVED TO RETURN TO SERVICE. - [SDR C2XA09SH165](https://openairdocs.org/sdr/C2XA09SH165.md): Floor Support · corroded · May 24, 2009 · N14939 · Emb EMB145EP · Fuselage Miscellaneous Structure > 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 51-21-04/05/06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09TY027](https://openairdocs.org/sdr/C2XA09TY027.md): Battery · discharged · Feb 14, 2009 · N14939 · Emb EMB145 · Emergency Lighting > 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.md): Light · inoperative · Feb 11, 2009 · N14939 · Emb EMB145EP · Emergency Lighting > 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, OPS TESTED WITH NO DEFECTS NOTED. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2X2008F00006](https://openairdocs.org/sdr/C2X2008F00006.md): Wire · broken · Jul 19, 2008 · N14939 · Emb EMB145EP · Landing Gear System Wiring > 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 POPPING. THE CREW ABORTED TAKEOFF, AND TAXIED BACK TO THE GATE WITHOUT INCIDENT. MAINTENANCE INSP - [SDR C2XA08IA103](https://openairdocs.org/sdr/C2XA08IA103.md): Uplock · malfunctioned · Apr 6, 2008 · N14939 · Emb EMB145EP · Landing Gear Retraction/Extension System > 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 AND AMBER. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND Next page: https://openairdocs.org/deregistered/N14939-2015-08-13/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 = 'N14939' AND deregistration_id = 'N14939-2015-08-13' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N14939-2015-08-13/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.