# Service difficulty reports: N14925, cancelled Sep 6, 2019

A list on [N14925, cancelled Sep 6, 2019](https://openairdocs.org/deregistered/N14925-2019-09-06.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 2 · 71 reports

- [SDR ASOA20140119011](https://openairdocs.org/sdr/ASOA20140119011.md): Ground Stud · melted · Jan 19, 2014 · N14925 · Emb EMB145EP · Ice/Rain Protection System Wiring
  > THE CREW REPORTED THAT THEY HAD SMOKE COMING FROM THE BASE OF WINDSHIELD NR 1, AND THAT IT STOPPED 1-2 MINUTES AFTER WINDSHIELD HEAT WAS TURNED OFF. THE ACFT LANDED WITH NO INCIDENT. THE CREW PLACED THE WINDSHIELD HEAT ON MEL 30-42-02, AND THE ACFT WAS APPRO
- [SDR ASOA20130930179](https://openairdocs.org/sdr/ASOA20130930179.md): Wire · loose · Sep 30, 2013 · N14925 · Emb EMB145EP · Light System Wiring
  > DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EXIT SIGN ABOVE F/A`S HEAD WOULD NOT ILLUMINATE. MX INSPECTED THE ACFT AND RESECURRED THE WIRING ON THE AFFECTED SIGN, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVIC
- [SDR ASOA20130212013](https://openairdocs.org/sdr/ASOA20130212013.md): Charger · inoperative · Feb 12, 2013 · N14925 · Emb EMB145EP · Emergency Lighting
  > DURING SCHEDULED MX, THE EMERGENCY FLOOR STIP LIGHTING AT POSITIONS 1,2,3 AND SERVICE DOOR EMERGENCY LIGHTING WERE FOUND INOPERATIVE. MX REPLACED THE EMERGENCY LIGHT BATTERY CHARGER, OPERATIONALLY TESTED THE SYSTEM AND CLEARED THE DISCREPANCY.
- [SDR ASOA20130130007H](https://openairdocs.org/sdr/ASOA20130130007H.md): Light · inoperative · Jan 30, 2013 · N14925 · Emb EMB145EP · Emergency Lighting
  > DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE AISLE PATH LIGHTING FROM ROW 3 TO ROW 6 WAS INOPERATIVE. MX R & R THE AFFECTED LIGHT STRIP, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20121217159](https://openairdocs.org/sdr/ASOA20121217159.md): Skin · cracked · Dec 17, 2012 · N14925 · Emb EMB145EP · Fuselage Main, Plate/Skin
  > DURING SCHEDULED MX THE RT UPPER FUSELAGE SKIN AT FRAME 75 WAS FOUND TO BE CRACKED. THE SKIN WAS REPAIRED IAW EC 5330-02353 AND THE DISCREPANCY CLEARED.
- [SDR ASOA20121217158](https://openairdocs.org/sdr/ASOA20121217158.md): Skin · cracked · Dec 17, 2012 · N14925 · Emb EMB145EP · Fuselage Main, Plate/Skin
  > DURING SCHEDULED MX THE LT UPPER FUSELAGE SKIN AT FRAME 75 WAS FOUND TO BE CRACKED. THE SKIN WAS REPAIRED IAW EC 5330-02353 AND THE DISCREPANCY CLEARED.
- [SDR ASOA111227019](https://openairdocs.org/sdr/ASOA111227019.md): Acm · smoke · Dec 27, 2011 · N14925 · Emb EMB145EP · Cabin Cooling System
  > THE CREW REPORTED THAT AFTER STARTING THE NR 2 ENGINE WITH THE NR1 PACK ON THERE WAS DARK SMOKE IN THE COCKPIT AND FORWARD CABIN WITH A NOTED SULPHUR SMELL. THE SOURCE OF THE SMOKE WAS DETERMINED TO BE THE NR1 PACK WHICH WAS SUBSEQUENTLY DEFERRED UNDER AN MEL
- [SDR C2XA11TY141](https://openairdocs.org/sdr/C2XA11TY141.md): Skin · corroded · Sep 13, 2011 · N14925 · Emb EMB145ER · Fuselage Main, Plate/Skin
  > TYS - A/C CURRENTLY IN C-CHECK WHEN INSPECTION FOUND VARIOUS AREAS OF CORROSION IN THE LOWER FUSELAGE BETWEEN FRAMES 13 AND 14, STRINGERS 20L TO 20R. MAINTENANCE REMOVED AND REPLACED THE SKIN, ALLODINED, PRIMED AND PAINTED. ALSO REMAPPED THE RVSM AREA. RVSM
- [SDR C2XA11TY138](https://openairdocs.org/sdr/C2XA11TY138.md): Sill · corroded · Sep 10, 2011 · N14925 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > TYS - A/C CURRENTLY IN A C-CHECK STATUS WHEN INSPECTION FOUND THE LT FLOOR SILL PITTED AT FR18 THRU FR 20. MAINTENANCE REMOVED AND 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 C2XA10IA274](https://openairdocs.org/sdr/C2XA10IA274.md): Controller · inoperative · Oct 25, 2010 · N14925 · Emb EMB145EP · Emergency Lighting
  > IAH - FLIGHT 2873, DURING PREFLIGHT INSPECTION THE CREW REPORTED A PLASTIC BURNING SMELL. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE OVERHEAD LIGHT CONTROLLER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN
- [SDR C2XA09SH493](https://openairdocs.org/sdr/C2XA09SH493.md): Wire Harness · broken · Dec 7, 2009 · N14925 · Emb EMB145EP · Landing Gear System Wiring
  > SHV - DURING TAKEOFF THE AIRCREW DISCOVERED THE LANDING GEAR WOULD NOT RETRACT. PERFORMED AN AIR RETURN TO MEM AND LANDED WITHOUT INCIDENT. AN EMERGENCY WAS NOT DECLARED. THE AIRCRAFT WAS FERRIED TO SHV FOR REPAIR ON 12/08/09, FLT 4923. MAINTENANCE TROUBLE
- [SDR C2XA09IA304](https://openairdocs.org/sdr/C2XA09IA304.md): Check Valve · inoperative · Dec 2, 2009 · N14925 · Emb EMB145EP · Landing Gear Retraction/Extension System
  > IAH - DURING PREFLIGHT INSPECTION THE CREW DISCOVERED A PIECE OF THE LEFT NOSE LANDING GEAR TO HAVE A PIECE MISSING. THE AIRCRAFT WAS INSPECTED AND FERRIED TO IAH WHERE IT LANDED WITHOUT INCIDENT. IAH MAINTENANCE INSPECTED THE AIRCRAFT, DETERMINED THAT THE N
- [SDR C2XA09IA303](https://openairdocs.org/sdr/C2XA09IA303.md): Solenoid Valve · defective · Dec 2, 2009 · N14925 · Emb EMB145EP · Landing Gear Door Retract Section
  > IAH - DURING PREFLIGHT INSPECTION THE CREW DISCOVERED A PIECE OF THE LEFT NOSE LANDING GEAR TO HAVE A PIECE MISSING. THE AIRCRAFT WAS INSPECTED AND FERRIED TO IAH WHERE IT LANDED WITHOUT INCIDENT. IAH MAINTENANCE INSPECTED THE AIRCRAFT, DETERMINED THAT THE N
- [SDR C2XA09IA279](https://openairdocs.org/sdr/C2XA09IA279.md): Electronic Unit · inoperative · Nov 2, 2009 · N14925 · Emb EMB145EP · Landing Gear Retraction/Extension System
  > IAH - FLIGHT 3102, ON DEPARTURE FROM MAF, THE CREW REPORTED THAT THE NOSE GEAR RETRACTION MADE LOUD NOISES DURING STOWAGE FOLLOWED BY PERSISTENT DEEP THUMPING FOR THE ENTIRE FLIGHT WITH THE NOSE GEAR POSITION INDICATOR CYCLING BETWEEN UP AND INTRANSIT FOR THE
- [SDR C2XA09IA278](https://openairdocs.org/sdr/C2XA09IA278.md): Uplock · inoperative · Nov 2, 2009 · N14925 · Emb EMB145EP · Landing Gear Retraction/Extension System
  > IAH - FLIGHT 3102, ON DEPARTURE FROM MAF, THE CREW REPORTED THAT THE NOSE GEAR RETRACTION MADE LOUD NOISES DURING STOWAGE FOLLOWED BY PERSISTENT DEEP THUMPING FOR THE ENTIRE FLIGHT WITH THE NOSE GEAR POSITION INDICATOR CYCLING BETWEEN UP AND INTRANSIT FOR THE
- [SDR C2XA09IA233](https://openairdocs.org/sdr/C2XA09IA233.md): Unknown · odor · Sep 11, 2009 · N14925 · Emb EMB145EP · Air Distribution System
  > IAH - FLIGHT 2959 - THE CREW REPORTED THAT AT FL260, SMELLED ELECTRICAL SMOKE WITH NONE VISIBLE. THE SMELL PERSISTED FOR 30-45 SECONDS AND CLEARED WITH THE F/A REPORTING SOME SMELL FROM ROW 7. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE PERFORM
- [SDR C2XA09IA096](https://openairdocs.org/sdr/C2XA09IA096.md): Smoke Detector · malfunctioned · Apr 13, 2009 · N14925 · Emb EMB145EP · Smoke Detection
  > IAH - FLIGHT 2493, THE CREW REPORTED A LAV SMOKE INDICATION AFTER STARTING THE NUMBER ONE ENGINE. THE CREW REPORTED THAT THERE WAS NO SMOKE IN THE LAV, BUT WAS HOT. CYCLING THE CIRCUIT BREAKER CLEARED THE WARNING. MAINTENANCE INSPECTED THE AIRCRAFT, AND LAV
- [SDR C2XA09TY054](https://openairdocs.org/sdr/C2XA09TY054.md): Skin · damaged · Mar 21, 2009 · N14925 · Emb EMB145EP · Fuselage Main, Plate/Skin
  > THE LT & RT FUSELAGE SKINS HAVE 15 HOLES (7 HOLES LT AND 8 HOLES RT) THAT HAVE CRACKS RADIATING FROM THE FASTENERS. THE HOLES WERE REAMED BETWEEN.531 INCH AND.533 INCH DIAMETER, ALODINED AND BUSHINGS INSTALLED. ALL WORK ACCOMPLISHED IAW EC5330-01896. AIRC
- [SDR C2XA09TY051](https://openairdocs.org/sdr/C2XA09TY051.md): Yoke · cracked · Mar 19, 2009 · N14925 · Emb EMB145EP · Nacelle/Pylon, Attach Fittings
  > TYS - DURING C-CHECK THE NR 1 ENGINE LOWER FORWARD YOKE WAS FOUND CRACKED AT ENGINE MOUNT WEBBING. THE NR 1 ENGINE LOWER FORWARD YOKE MOUNT WEBBING AFT SECTION WAS REMOVED AND REPLACED IAW EC 5450-01019. A/C IS STILL IN C-CHECK.
- [SDR C2XA09TY050](https://openairdocs.org/sdr/C2XA09TY050.md): Stiffener · cracked · Mar 18, 2009 · N14925 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > AIRCRAFT CURRENTLY IN A C-CHECK STATUS. INSPECTION FOUND A STIFFENER CRACKED IN THE LEFT PYLON INSIDE PANEL 414DB CRACKED ON BOTH ENDS. MAINTENANCE REMOVED AND REPLACED THE STIFFENER IAW EMB SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT TH
- [SDR C2XA09TY049](https://openairdocs.org/sdr/C2XA09TY049.md): Stiffener · cracked · Mar 18, 2009 · N14925 · Emb EMB145ER · Nacelle/Pylon Miscellaneous Structure
  > AIRCRAFT CURRENTLY IN A C-CHECK STATUS. INSPECTION FOUND A CRACK IN THE AFT PYLON STIFFENER/STRINGER INSIDE PANEL 414DB. MAINTENANCE REMOVED AND REPLACED THE PYLON STRINGER STIFFENER. ALL WORK WAS ACCOMPLISHED IAW EMB 145 SRM 51-40-02. AIRCRAFT WILL BE REL
- [SDR C2XA09TY055](https://openairdocs.org/sdr/C2XA09TY055.md): Fitting · damaged · Mar 17, 2009 · N14925 · Emb EMB145EP · Fuselage Main, Frame
  > THE FRAME 75 VERTICAL FITTING AND ADJACENT SKIN ARE SHOWING SIGNS OF FRETTING AT EDGES. REMOVED FITTING, BLENDED OUT DAMAGE, PERFORMED DYE PEN INSPECTION AND RE-INSTALLED FITTING IAW EC5310-01317 AND SRM 51-40-02. AIRCRAFT RELEASED FROM C-CHECK AND RETURNED
- [SDR C2XA09TY019A](https://openairdocs.org/sdr/C2XA09TY019A.md): Light · inoperative · Jan 22, 2009 · N14925 · Emb EMB145 · Emergency Lighting
  > EMERGENCY LIGHT OVER MAIN DOOR INOP. R&R LAMP IAW EMB 145AMM 33-50-06. OPS CHECK GOOD. ACFT RELEASED AND RETURNED TO SERVICE.
- [SDR C2XA08IA056](https://openairdocs.org/sdr/C2XA08IA056.md): Fuse · blown · Feb 9, 2008 · N14925 · Emb EMB145EP · Emergency Lighting
  > IAH - DURING MAINTENANCE INSPECTION THE BOTH LT OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FUSE FOR THE EMERGENCY LIGHTS, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO
- [SDR C2XA08IA022](https://openairdocs.org/sdr/C2XA08IA022.md): Power Supply · discharged · Jan 9, 2008 · N14925 · Emb EMB145EP · Emergency Lighting
  > IAH - DURING MAINTENANCE INSPECTION NUMEROUS EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER 1 EMERGENCY LIGHT BATTERY POWER SUPPLY, OPERATIONALLY CHECKED WITH NO DEFETCS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETU
- [SDR C2XA08IA012](https://openairdocs.org/sdr/C2XA08IA012.md): Skin · cracked · Jan 4, 2008 · N14925 · Emb EMB145EP · Wing, Plate/Skin
  > IAH, FLIGHT 2472, DURING PREFLIGHT INSPECTION THE CREW REPORTED A CRACK IN THE LEFT WING UPPER SKIN ADJACENT TO THE LEFT SPOILER INBOARD HINGE POINT. THE SKIN WAS INSPECTED AND PLACED ON DMI FO 500FC, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON
- [SDR C2XA07RI083](https://openairdocs.org/sdr/C2XA07RI083.md): Wire · broken · Sep 24, 2007 · N14925 · Emb EMB145EP · Light System Wiring
  > EWR - DURING ROUTINE MAINTENANCE, MX FOUND EMERGENCY LIGHT PATH STRIP NOT WORKING. MX FOUND STRIP WIRE BROKEN. MX REPAIRED THE WIRING AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA07RI079](https://openairdocs.org/sdr/C2XA07RI079.md): Light · inoperative · Sep 12, 2007 · N14925 · Emb EMB145EP · Emergency Lighting
  > FLT 2297 - EWR - CREW REPORTED EMERGENCY FLOOR LIGHTING WIRE IS VISIBLE OUTSIDE PLASTIC MOLDING AND STRIP IS INOPERATIVE BY SEAT 12A. EWR MX REMOVED AND REPLACED EMERGENCY FLOOR STRIP IAW EMB 145 AMM 33-50-12. MX PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AC
- [SDR C2XA06IA184](https://openairdocs.org/sdr/C2XA06IA184.md): Ballast · burned · Nov 22, 2006 · N14925 · Emb EMB145EP · Passenger Compartment Lighting
  > IAH - FLIGHT 2648, THE CREW REPORTED A SMOKE ODOR COMING FROM THE CABIN. MAINTENANCE REMOVED AND REPLACED THE SIDEWALL/CEILING LIGHT BALLAST, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA06IA176](https://openairdocs.org/sdr/C2XA06IA176.md): Ballast · inoperative · Nov 9, 2006 · N14925 · Emb EMB145EP · Passenger Compartment Lighting
  > IAH - FLIGHT 2555, DURING POST FLIGHT INSPECTION THE CREW REPORTED A BURNING SMELL IN THE CABIN. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE LIGHTING BALLAST AT SEAT 8A, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED
- [SDR C2XA06IA175](https://openairdocs.org/sdr/C2XA06IA175.md): Unknown · odor · Nov 9, 2006 · N14925 · Emb EMB145EP · Air Distribution System
  > IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED A BURNING ODOR IN THE CABIN. MAINTENANCE INSPECTED THE AIRCRAFT AND WAS UNABLE TO DUPLICATE THE DISCREPANCY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA06RI004](https://openairdocs.org/sdr/C2XA06RI004.md): Bevel Gear · fractured · Aug 29, 2006 · N14925 · Emb EMB145EP · Turbine Engine Reduction Gear
  > DURING CLIMB, ENG NR 1 IN FLT SHUTDOWN. ACFT DIVERTED TO IAD. MX FOUND METAL DEBRIS ON CHIP DETECTOR. MX R & R ENGINE. OPS CHECKS PERFORMED SUCCESSFULLY. ACFT APPROVED TO RETURN TO FLT. REMOVED ENG FOR INVEST & REPAIR. DFDR DATA REVIEWED & INDICATED N2 STEAD
- [SDR C2XA06SD012](https://openairdocs.org/sdr/C2XA06SD012.md): Warning System · false activation · Jul 22, 2006 · N14925 · Emb EMB145EP · Landing Gear Position and Warning
  > HEARD (LANDING GEAR) AURAL WARNING TWICE AT 13000 FT, IN MOD TURB AND PRECIP LANDING GEAR WAS UP AND NO INDICATIONS WERE SEEN ON EICAS. RESET RA CB'S TESTED RA'S IAW EMB 145 AMM 34-31-00. NO WARNINGS DURING OPS CHECK.
- [SDR C2XA06CL067](https://openairdocs.org/sdr/C2XA06CL067.md): Light · inoperative · Jul 21, 2006 · N14925 · Emb EMB145EP · Emergency Lighting
  > CLE FLIGHT NR 2221 THE CREW REPORTED THE EMERGENCY LIGHTS BY THE EXIT ROW WERE INOPERATIVE. MAINTENANCE INSPECTED AND RESET THE EMERGENCY LIGHT SYSTEM. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA06CL011](https://openairdocs.org/sdr/C2XA06CL011.md): Connector · loose · Jan 25, 2006 · N14925 · Emb EMB145EP · Light System Wiring
  > DURING ROUTINE MAINTENANCE THE RT EMERGENCY EXIT IDENTIFIER SIGN WAS INOPERATIVE. MAINTENANCE INSPECTED AND RESECURED THE CONNECTOR BEHIND THE EXIT SIGN. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA06CL010](https://openairdocs.org/sdr/C2XA06CL010.md): Battery · discharged · Jan 25, 2006 · N14925 · Emb EMB145EP · Emergency Lighting
  > DURING ROUTINE MAINTENANCE SEVERAL EMERGENCY LIGHTS WERE FOUND NOT WORKING. MAINTENANCE INSPECTED AND REPLACED THE NR 2 AND NR 3 EMERGENCY LIGHT BATTERIES. OPERATIONAL CHECKS WERE GOOD. NR 3 BATTERY P/N 2013-1A, S/N 84586.
- [SDR C2XA06BT003](https://openairdocs.org/sdr/C2XA06BT003.md): Charger · faulty · Jan 24, 2006 · N14925 · Emb EMB145EP · Emergency Lighting
  > CREW REPORTED, THE RIGHT WING EMERGENCY LIGHT IS NOT WORKING. REMOVED AND REPLACED NR 2 BATTERY CHARGER IAW EMB145 AMM 33-50-04. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR C2XA06IA009](https://openairdocs.org/sdr/C2XA06IA009.md): Hydraulic System · leaking · Jan 13, 2006 · N14925 · Emb EMB145EP · Hydraulic System, Main
  > IAH - FLIGHT 2966, THE CREW REPORTED THAT THE HYDRAULIC SYSTEM ONE QUANTITY INDICATION WENT TO ZERO DURING FLIGHT. THE CREW DEACTIVATED THE SYSTEM 1 HYDRAULICS, AND LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT WITH NO LEAKS NOTED, CLEAN
- [SDR C2XA04CL099](https://openairdocs.org/sdr/C2XA04CL099.md): Spline · stripped · Sep 25, 2004 · N14925 · Emb EMB145ER · Passenger/Crew Doors
  > THE CREW REPORTED THE MAIN PASSENGER DOOR WOULD NOT OPEN. MAINTENANCE INSPECTED AND REPLACED THE INSIDE DOOR HANDLE. OPS CHECKED GOOD.
- [SDR C2XA04CL091](https://openairdocs.org/sdr/C2XA04CL091.md): Control Lever · malfunctioned · Sep 10, 2004 · N14925 · Emb EMB145ER · Landing Gear Selector
  > AFTER TAKEOFF FROM CLE FLIGHT CREW HAD TO CYCLE THE LANDING GEAR HANDLE TWICE TO GET THE LANDING GEAR TO RETRACT. AIRCRAFT RETURNED TO CLE LANDED WITH OUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL LEVER. OPERATIONAL CHECKED GOOD.
- [SDR C2XA04SH488](https://openairdocs.org/sdr/C2XA04SH488.md): Floor Support · corroded · Aug 28, 2004 · N14925 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA04SH489](https://openairdocs.org/sdr/C2XA04SH489.md): Floor Support · corroded · Aug 28, 2004 · N14925 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA04SH485](https://openairdocs.org/sdr/C2XA04SH485.md): Floor Support · corroded · Aug 10, 2004 · N14925 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE RIGHT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 23. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA04CL059](https://openairdocs.org/sdr/C2XA04CL059.md): Inverter · inoperative · Jun 1, 2004 · N14925 · Emb EMB145ER · Emergency Lighting
  > THE CREW REPORTED THE EMERGENCY EXIT SIGN WAS INOPERATIVE WHEN TESTED. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA04BT044](https://openairdocs.org/sdr/C2XA04BT044.md): Battery · faulty · Apr 1, 2004 · N14925 · Emb EMB145ER · Emergency Lighting
  > CREW REPORTED, THE LT AND RT OVERWING EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 4 BATTERY POWER PACK IAW EMB145 MM 33-50-11, OPS CHECKED SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR C2XA03CL161](https://openairdocs.org/sdr/C2XA03CL161.md): Shroud · loose · Sep 6, 2003 · N14925 · Emb EMB145ER · Emergency Exits
  > WHILE PERFORMING A 1A INSPECTION MAINTENANCE REPORTED THAT THE RIGHT HAND EMERGENCY EXIT WOULD NOT OPEN IT WAS BLOCKED AT THE TOP BY A SIDEWALL PANEL. MAINTENANCE RESECURED SIDEWALL PANEL AND ALL OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA03BT085](https://openairdocs.org/sdr/C2XA03BT085.md): Power Supply · discharged · Aug 27, 2003 · N14925 · Emb EMB145ER · Emergency Lighting
  > EWR LOG BOOK SQUAWK AISLE PATH LIGHTING STRIPS SEGMENTS 2 AND 3 INOP. REMOVED AND REPLACED NR 2 EMERGENCY BATTERY POWER SUPPLY IAW EMB145 MM 33-50-04. OPS CHECK GOOD.
- [SDR C2XA03BT063](https://openairdocs.org/sdr/C2XA03BT063.md): Smoke Detector · malfunctioned · May 29, 2003 · N14925 · Emb EMB145ER · Smoke Detection
  > CREW REPORTED, DECLARED EMERGENCY FOR BAGGAGE AREA SMOKE WARNING IN FLIGHT, DIVERTED TO RDU, FIRE EXTINGUISHER BLOWN. MAINTENANCE DISPATCHED TO AIRCRAFT, INSPECTED AND FOUND NO EVIDENCE OF SMOKE. PLACED BAGGAGE SMOKE DETECTOR AND BAGGAGE FIRE EXTINGUISHER ON
- [SDR C2XA03CL029](https://openairdocs.org/sdr/C2XA03CL029.md): Ballast · faulty · Feb 3, 2003 · N14925 · Emb EMB145ER · Passenger Compartment Lighting
  > CLE FLIGHT#2267 THE CREW REPORTED A ELECTRICAL BURNING SMELL COMING FROM ABOVE THE FLIGHT ATTENDANT CALL PANEL.MAINTENANCE INSPECTED AND REPLACED THE DIMMING BALLAST FOR THE CEILING LIGHTS ABOVE SEAT 1A.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FO
- [SDR C2XA03BT010](https://openairdocs.org/sdr/C2XA03BT010.md): Uplock Switch · faulty · Jan 17, 2003 · N14925 · Emb EMB145LR · Landing Gear Retraction/Extension System
  > SYR---CO2576, CREW REPORTED, LANDING GEAR LEVER DISAGREEMENT AFTER TAKEOFF. LEFT MAIN GEAR WOULD NOT RETRACT. AIRCRAFT AIR RETURNED TO SYR AND LANDED UNEVENTFULLY. MAINTENANCE REMOVED AND REPLACED LEFT MAIN LANDING GEAR UPLOCK BOX IAW 32-33-10. OPS CHECKED

Next page: https://openairdocs.org/deregistered/N14925-2019-09-06/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 = 'N14925' AND deregistration_id = 'N14925-2019-09-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N14925-2019-09-06/reports

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