# Service difficulty reports: N13949, cancelled Mar 3, 2023

A list on [N13949, cancelled Mar 3, 2023](https://openairdocs.org/deregistered/N13949-2023-03-03.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 · 100 reports

- [SDR ASOA20121126156T](https://openairdocs.org/sdr/ASOA20121126156T.md): Skin · dented · Nov 19, 2012 · N13949 · Emb EMB145LR · Rudder, Plate/Skin
  > RUDDER HAS SMALL DENT WITH CREASE ON RT SIDE JUST FORWARD OF FRONT SPAR AND BETWEEN RIBS ZV-3469 & ZV-3179. CUTOUT DENT AND INSTALLED FILLER AND DOUBLER. ACFT STILL IN C-CHECK.
- [SDR ASOA20120715061](https://openairdocs.org/sdr/ASOA20120715061.md): Hose · blown · Jul 15, 2012 · N13949 · Emb EMB145LR · Hydraulic System, Main
  > THE CREW REPORTED AN HYD SYS 1 FAIL MESSAGE IN FLIGHT. THE ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MX INSPECTED AND REPLACED THE HYD HOSE ON THE LT GEAR ACTUATOR. THEY ALSO REPLACED THE NR 1 ENGINE DRIVEN HYD PUMP. OPS CHECKS WERE GOOD.
- [SDR C2XA11TY140](https://openairdocs.org/sdr/C2XA11TY140.md): Panel · blocked · Sep 7, 2011 · N13949 · Emb EMB145LR · Pneumatic Distribution System
  > TYS - A/C RETURNED TO BASE AFTER LEAVING EWR TO BNA WHEN CREW HAD A ECIAS MESSAGE OG THE BLEED 2 OVER TEMP IN ICING CONDITIONS. MAINTENANCE FOUND THE ACESS PANEL 414CB LT PANEL TO THE FAN AIR VALVE/PRE COOLER INSTALL ON THE RT SIDE AND THE 424CB RT PANEL TO T
- [SDR C2XA11IA051](https://openairdocs.org/sdr/C2XA11IA051.md): Unknown · odor · Mar 11, 2011 · N13949 · Emb EMB145LR · Air Distribution System
  > EN ROUTE TO GSO THE CREW REPORTED A BURNING SMELL IN FRONT OF THE CABIN. THE AIRCRAFT DIVERTED TO MOB WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED AN INSPECTION OF THE AIRCRAFT, HIGH-POWER ENGINE RUNS AND OPERATES THE AIR CONDITIONING PACKS HOWEVE
- [SDR C2XA11RI012](https://openairdocs.org/sdr/C2XA11RI012.md): Potentiometer · faulty · Jan 23, 2011 · N13949 · Emb EMB145LR · Flight Compartment Lighting
  > FLIGHT 2488 - EWR - FLIGHT CREW REPORTED PFD DIM/BRT CONTROL INTERMITTENT BRIGHT/DIM, PRODUCING ELECTRICAL ODOR. EWR MX REMOVED AND REPLACED BRIGHT/DIM POTENTIOMETER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA10TY184](https://openairdocs.org/sdr/C2XA10TY184.md): Skin · dented · Dec 5, 2010 · N13949 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > TYS - DENT AT EXTERNAL FUSELAGE FRM 20 STR 1-3L. FABRICATED AND INSTALLED DOUBLER AND FILLER AT STR 1L AND 1R, AND STR 4L AND 5L. PRIMED AND PAINTED REPAIR.
- [SDR C2XA10TY183](https://openairdocs.org/sdr/C2XA10TY183.md): Window Frame · corroded · Dec 3, 2010 · N13949 · Emb EMB145LR · Fuselage Main, Structure
  > TYS - WINDSHIELD FRAME CORRODED UNDER NUT PLATE RT SIDE LOWER FRAME. CUT OUT DAMAGED SECTION OF WINDSHIELD FRAME ON RT SIDE. FABRICATED FILLER AND INSTALLED FILLER AND NUT PLATE.
- [SDR C2XA10TY182](https://openairdocs.org/sdr/C2XA10TY182.md): Skin · damaged · Dec 3, 2010 · N13949 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > TYS - RT EXTERNAL SKIN FWD OF FRM 75 BETWEEN STR 1R AND 2R HAS DEEP BLEND FROM PREVIOUS REPAIR. INSTALLED INTERNAL DOUBLER AND EXTERNAL PATCH. PERFORMED EDDY CURRENT AND NO CRACKS NOTED.
- [SDR C2XA10IA260](https://openairdocs.org/sdr/C2XA10IA260.md): Hose · worn · Sep 19, 2010 · N13949 · Emb EMB145LR · APU Core Engine
  > MCI - FLIGHT 3026, THE CREW REPORTED A STRONG FUEL SMELL ON TAKE OFF ROLL. THE CREW ABORTED TAKE OFF AND RETURNED TO THE GATE WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE APU ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 9-22-10
- [SDR C2XA10TY142](https://openairdocs.org/sdr/C2XA10TY142.md): Drain Line · cracked · Sep 15, 2010 · N13949 · Emb EMB145LR · APU Engine Fuel and Control
  > CHS - IAH - FLIGHT DIVERTED TO TYS BECAUSE OF FUEL SMELL IN COCKPIT AFTER TAKEOFF. TYS MX VERIFIED THE FUEL SMELL COMING FROM APU. APU PLACED ON MEL LP--2625735. REMOVED AND REPLACED APU FUEL DRAIN HOSE, LEAK CHECK GOOD.
- [SDR C2XA10TY131](https://openairdocs.org/sdr/C2XA10TY131.md): Apu · odor · Sep 14, 2010 · N13949 · Emb EMB145LR · APU Engine Fuel and Control
  > CHS - IAH - FLIGHT DIVERTED TO TYS BECAUSE OF FUEL SMELL IN COCKPIT AFTER TAKEOFF. TYS MX VERIFIED THE FUEL SMELL COMING FROM APU. APU PLACED ON MEL LP--2625735. SDR FILED OPEN PENDING CORRECTIVE ACTION.
- [SDR C2XA10CL146](https://openairdocs.org/sdr/C2XA10CL146.md): Unknown · odor · Sep 7, 2010 · N13949 · Emb EMB145LR · Air Distribution System
  > CLE FLT 2297 CREW REPORTED FUEL SMELL AFTER TAKEOFF. CREW REPORTED SMELL DISSIPATED AFTER APU SHUT-DOWN. IN CLE MAINTENANCE INSPECTED AND FOUND NO FUEL SMELL. OPERATIONAL CHECKS GOOD.
- [SDR C2XA10IA246](https://openairdocs.org/sdr/C2XA10IA246.md): Inverter · inoperative · Sep 5, 2010 · N13949 · Emb EMB145LR · Emergency Lighting
  > IAH - FLIGHT 3079, DURING POST FLIGHT INSPECTION THE CREW REPORTED THE EMERGENCY EXIT SIGN ON THE RIGHT SIDE TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FIVE EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT W
- [SDR C2XA10CL098](https://openairdocs.org/sdr/C2XA10CL098.md): Hydraulic Line · leaking · Jun 23, 2010 · N13949 · Emb EMB145LR · Hydraulic System, Main
  > CLE FLT 2243 THE CREW REPORTED A HYDRAULIC SYSTEM 1 FAIL DURING CLIMB. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE HYDRAULIC HOSE ON THE LEFT MAIN GEAR ACTUATOR. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA09TY091](https://openairdocs.org/sdr/C2XA09TY091.md): Light · inoperative · May 10, 2009 · N13949 · Emb EMB145LR · Emergency Lighting
  > AIRCRAFT IN FOR A ROUTINE INSPECTION WHEN THE EMERGENCY LIGHT IN THE CEILING PANEL AT ROW 12 WAS FOUND INOP. MAINTENANCE REMOVED AND REPLACED THE LIGHT BULB IAW EMB 145 AMM 33-50-08. OPS CHECK GOOD AND WAS RELEASED.
- [SDR C2XA08IA178](https://openairdocs.org/sdr/C2XA08IA178.md): Contactor · malfunctioned · Jul 27, 2008 · N13949 · Emb EMB145LR · AC Power Distribution System
  > IAH - FLIGHT 2350, THE CREW REPORTED THAT AT FL360, THE AIRCRAFT LOST ALL ELECTRICAL POWER FOR 10 SECONDS, POWER RETURNED FOR 2 SECONDS, WAS INTERMITTENT FOR 2 MINUTES WITH T/O CONFIG, AUTOPILOT, FLAPS, STALL WARNINGS. THE POWER WAS FINALLY RESTORED AFTER THR
- [SDR C2XA08RI107](https://openairdocs.org/sdr/C2XA08RI107.md): Computer · intermittent · Jul 25, 2008 · N13949 · Emb EMB145LR · Central Computers
  > FLIGHT 2882 - EWR - FLIGHT CREW REPORTED ELECTRICAL POWER LOSS IN FLIGHT AT 35,000 FT WITH A LOUD THUMP, MFD, PFD, EICAS ALL RED "X", AP FAIL. STALL TEST LIGHT ILLUMINATED BUT EVERYTHING CAME BACK A FEW SECONDS LATER. CREW LANDED ACFT AS PLANNED WITHOUT INCI
- [SDR C2XA08SH092](https://openairdocs.org/sdr/C2XA08SH092.md): Actuator · leaking · Jul 3, 2008 · N13949 · Emb EMB145LR · Landing Gear Door Actuator
  > FLIGHT 3082 - DIVERTED FROM IAH - HYD IN SYSTEM 1 LEAKED, HYD SYSTEM I FAILURE. MX REMOVED AND REPLACED NOSE LANDING GEAR DOOR ACTUATOR AND HOSES IAW EMB 145 32-33-03. OPS CHECK GOOD AND LEAK CHECK GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A)
- [SDR C2XA08TY028](https://openairdocs.org/sdr/C2XA08TY028.md): Frame · cracked · Feb 5, 2008 · N13949 · Emb EMB145LR · Fuselage Main, Frame
  > TYS MOD - DURING ROUTINE MX FOUND FRAME 81 CRACKED AT THE 6 O'CLOCK POSITION. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND A/C WAS RELEASED FOR SERVICE.
- [SDR C2XA07RI097](https://openairdocs.org/sdr/C2XA07RI097.md): Inverter · inoperative · Nov 9, 2007 · N13949 · Emb EMB145LR · Emergency Lighting
  > EWR - DURING ROUTINE MAINTENANCE, MX FOUND GALLEY SERVICE LIGHT INOPERATIVE. MX REMOVED AND REPLACED NR 2 EMERGENCY LIGHT INVERTER AND PERFORMED OPERATIONAL SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA07CL050](https://openairdocs.org/sdr/C2XA07CL050.md): Light · inoperative · May 31, 2007 · N13949 · Emb EMB145LR · Emergency Lighting
  > CLE FLIGHT 2414 - THE CREW REPORTED THE RIGHT AISLE PATH EMERGENCY LIGHT STRIP WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA07IA095](https://openairdocs.org/sdr/C2XA07IA095.md): Unknown · odor · Apr 24, 2007 · N13949 · Emb EMB145LR · Air Distribution System
  > IAH - FLIGHT 2824, THE CREW REPORTED A 115VAC OFF BUSS INDICATION WITH A BURNING SMELL IN THE COCKPIT. MAINTENANCE INSPECTED THE AIRCRAFT AND COULD NOT DUPLICATE ANY DISCREPANCY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA07IA114](https://openairdocs.org/sdr/C2XA07IA114.md): Battery Pack · discharged · Apr 16, 2007 · N13949 · Emb EMB145LR · Emergency Lighting
  > BNA - DURING MAINTENANCE INSPECTION THE NUMBER TWO EMERGENCY LIGHT BATTERY WAS FOUND TO BE NOT HOLDING A CHARGE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SER
- [SDR C2XA07IA042](https://openairdocs.org/sdr/C2XA07IA042.md): Proximity Sensor · intermittent · Feb 19, 2007 · N13949 · Emb EMB145LR · Landing Gear Position and Warning
  > GRK - FLIGHT 2963, THE CREW REPORTED A LANDING GEAR AIR GROUND FAILURE. THE CREW RESET THE SYSTEM SUCCESSFULLY AND THE AIRCRAFT LANDED AT GRK WITHOUT INCIDENT. ON FLIGHT 2114 THE DISCREPANCY RETURNED, AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTEN
- [SDR C2XA07TY004](https://openairdocs.org/sdr/C2XA07TY004.md): Floor Support · corroded · Feb 7, 2007 · N13949 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING A CURRENT 1C/5C INSPECTION CORROSION WAS FOUND ON BOTH ENDS OF A COMPOSITE CROSSMEMBER FLOOR SUPPORT AT FR PANEL 231FF. MAINTENANCE REPAIRED THE OMEGA BEAM AT THE DESIGNATED AREA IAW SRM 53-00-10.REMOVED AND REPLACED THE RAMP ANGLE IAW SRM 51-40-02. AL
- [SDR C2XA07BT011](https://openairdocs.org/sdr/C2XA07BT011.md): Wire Harness · burned · Jan 26, 2007 · N13949 · Emb EMB145LR · Light System Wiring
  > FLT NR 1271 ABOVE SEAT 15A PASSENGER REPORTED SEEING SMOKE AND BURNING SMELL. REMOVED AND REPLACED SIDEWALL LIGHT HARNESS IAW EMB145 IPC 33-21-06. OPS CHECK GOOD IAW EMB145 AMM 33-21-00.
- [SDR C2XA07BT005](https://openairdocs.org/sdr/C2XA07BT005.md): Battery · discharged · Jan 16, 2007 · N13949 · Emb EMB145LR · Emergency Lighting
  > DURING SERVICE/ROUTINE CHECK, FOUND EMERGENCY LIGHT FWD AISLE STRIP INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY NR 2 IAW EMB-145 AMM 33-50-04. OPS CHECK GOOD.
- [SDR C2XA07BT004](https://openairdocs.org/sdr/C2XA07BT004.md): Inverter · inoperative · Jan 12, 2007 · N13949 · Emb EMB145LR · Emergency Lighting
  > BTV DURING ROUTINE/SERVICE CHECK FOUND EMERGENCY EXIT LIGHT ON CEILING AT 1A INOP. ALSO EMERGENCY EXIT LIGHT ON COCKPIT STEP INOP. REMOVED AND REPLACED NR 3 EMERGENCY LIGHT INVERTER IAW AMM 33-50-11. OPS CHECK GOOD.
- [SDR C2XA06RI008](https://openairdocs.org/sdr/C2XA06RI008.md): Connector · disconnected · Oct 8, 2006 · N13949 · Emb EMB145LR · Light System Wiring
  > DURING AC ROUTINE MAINTENANCE, MX FOUND REAR AND FRONT FLOOR EMERGENCY LIGHTS INOP. MX FOUND CONNECTOR PLUG AT INVERTER NR 6 DISCONNECTED. MX RECONNECTED CONNECTOR PLUG AND PERFORMED OPERATIONAL TESTS SUCCESSFULLY. AC WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA05IA105](https://openairdocs.org/sdr/C2XA05IA105.md): Elevator · out of rig · Sep 12, 2005 · N13949 · Emb EMB145LR · Elevator Control System
  > IAH - FLIGHT 2703, THE CREW REPORTED THAT THEY HAD INSUFFICENT TRAVEL ON THE ELEVATOR FOR ROTATION. THE CREW ABORTED THE TAKEOFF WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND ELEVATOR RIGGING WITH NO DEFECTS BEING NOTED, AND THE AIRCRAFT WAS APPROV
- [SDR C2XA05CL044](https://openairdocs.org/sdr/C2XA05CL044.md): Acm · seized · Jun 6, 2005 · N13949 · Emb EMB145LR · Cabin Cooling System
  > CREW REPORTED STRONG ODOR OF MELTING RUBBER PREVALENT WITHIN A/C CABIN DURING PACK USAGE. MX INSP AND RELEASED A/C IAW MEL 21-51-00/1. SUPPLEMENT TO FOLLOW. MX REPLACED NR 1 ACM. OPS CHECKS GOOD.
- [SDR C2XA05RI009](https://openairdocs.org/sdr/C2XA05RI009.md): Computer · inaccurate · May 28, 2005 · N13949 · Emb EMB145LR · Attitude and Direction Data System
  > FLT 2609 - RIC - AFTER TAKEOFF, THE CREW REPORTED THAT HEADING WAS NOT MATCHING COMPASS IN DG AND SLVD MODE. CREW RETURNED TO RIC AND LANDED WITHOUT INCIDENT. RIC MAINTENANCE UPDATED NAV DATA BASE. OPERATIONAL CHECK WAS PERFORMED SUCCESFULLY. ACFT WAS APPR
- [SDR C2XA05CL036](https://openairdocs.org/sdr/C2XA05CL036.md): Holder · cracked · May 16, 2005 · N13949 · Emb EMB145LR · Emergency Equipment
  > DURING ROUTINE MAINTENANCE, THE F/A`S FLASHLIGHT HOLDER/CHARGER WAS FOUND CRACKED AND THE FLASHLIGHT WOULD NOT STAY LOCKED ONTO THE HOLDER. MAINTENANCE REPLACED THE FLASHLIGHT HOLDER. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA05IA033](https://openairdocs.org/sdr/C2XA05IA033.md): Duct · ruptured · Mar 1, 2005 · N13949 · Emb EMB145LR · Pneumatic Distribution System
  > IAH - FLIGHT 2654, ON TAKEOFF THE CREW REPORTED A NUMBER ONE ENGINE OVERTEMP AND FIRE WARNING. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE 13TH STAGE ENGINE BLEED TUBE TO BE RUPTURED. MAINT
- [SDR C2XA04CL107](https://openairdocs.org/sdr/C2XA04CL107.md): Inverter · inoperative · Oct 13, 2004 · N13949 · Emb EMB145LR · Emergency Lighting
  > CREW REPORTED THE LAST THREE ROWS OF AISLE EMERGENCY LIGHTING INOPERATIVE. FOUND LOOSE CONNECTION ON THE LIGHTS AND RECONNECTED. ITEM REPEATED ON THE NEXT FLIGHT AND MAINTENANCE REPLACED THE NUMBER 6 EMERGENCY INVERTED. OPS CHECK GOOD.
- [SDR C2XA04CL096](https://openairdocs.org/sdr/C2XA04CL096.md): Sign · loose · Sep 22, 2004 · N13949 · Emb EMB145LR · Emergency Lighting
  > EWR FLIGHT 2167- CREW REPORTED THE EMERGENCY LIGHT IN FRONT OF SEAT 3BC WAS INOPERATIVE. MAINTENANCE INSPECTED THE LIGHT ASSEMBLY AND RESECURED THE ELECTRICAL CONNECTORS AND THE EMERGENCY LIGHT OPERATIONAL CHECK WAS GOOD.
- [SDR C2XA04BT100](https://openairdocs.org/sdr/C2XA04BT100.md): Connector · loose · Sep 22, 2004 · N13949 · Emb EMB145LR · Fasteners
  > DURING SERVICE AND ROUTINE INSPECTION ON RON BTV, MAINTENANCE FOUND SEVERAL FORWARD CABIN EMERGENCY LIGHTS AND LT HAND FORWARD EXTERNAL EMERGENCY LIGHTS INOPERATIVE IN ALL MODES. RESECURED CONNECTOR TO NR 1 EMERGENCY LIGHT BATTERY AS REQUIRED, OPS CHECKED GOO
- [SDR C2XA04SD008](https://openairdocs.org/sdr/C2XA04SD008.md): Inverter · inoperative · Sep 18, 2004 · N13949 · Emb EMB145LR · Emergency Lighting
  > EMERGENCY LIGHTS BELOW COCKPIT DOOR AND ABOVE MAIN CABIN DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT INVERTER AS PER THE EMB AMM 33-50-11. EMERGENCY LIGHTS OPERATIONALLY CHECKED NORMAL AND AIRCRAFT WAS RELEASED.
- [SDR C2XA04CL081](https://openairdocs.org/sdr/C2XA04CL081.md): Inverter · inoperative · Aug 17, 2004 · N13949 · Emb EMB145LR · Emergency Lighting
  > CREW REPORTED THAT THE EMERGENCY LIGHTS WILL NOT TURN ON. MAINTENANCE INSPECTED AND REMOVED AND REPLACED THE POSITION 6 EMERGENCY LIGHT INVERTER. ALL OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA04IA103](https://openairdocs.org/sdr/C2XA04IA103.md): Charger · inoperative · Aug 16, 2004 · N13949 · Emb EMB145LR · Emergency Lighting
  > DURING PRE-FLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY CHARGER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA04BT085](https://openairdocs.org/sdr/C2XA04BT085.md): Battery Pack · failed · Aug 7, 2004 · N13949 · Emb EMB145LR · Emergency Lighting
  > MCI LOG SQUAWK FWD OVER THE WING AISLE EXIT LOCATOR SIGN INOP. REMOVED AND REPLACED NR 4 BATTERY POWER SUPPLY IAW EMB 145 AMM 33-50-04. OPS CHECK GOOD.
- [SDR C2XA04CL078](https://openairdocs.org/sdr/C2XA04CL078.md): Light · inoperative · Aug 6, 2004 · N13949 · Emb EMB145LR · Emergency Lighting
  > FLIGHT NR 3233, THE CREW REPORTED THAT THE RT SIDE EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE. MAINTENANCE INSPECTED AND RESET THE EMERGENCY LIGHT SYSTEM. ALL OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA04CL069](https://openairdocs.org/sdr/C2XA04CL069.md): Light · inoperative · Jul 10, 2004 · N13949 · Emb EMB145LR · Emergency Lighting
  > DURING ROUTINE MAINTENANCE THE EMERGENCY FLOOR LIGHT STRIP WAS INTERMITTENT AT ROW 15-17. MAINTENANCE REPLACED THE FLOOR LIGHT STRIP AT ROW 15-17. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA04CL070](https://openairdocs.org/sdr/C2XA04CL070.md): Lamp · inoperative · Jul 10, 2004 · N13949 · Emb EMB145LR · Emergency Lighting
  > DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT IN AISLE AT ROW 12 WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT BULB AT ROW 12 EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA04IA082](https://openairdocs.org/sdr/C2XA04IA082.md): Light · malfunctioned · Jul 3, 2004 · N13949 · Emb EMB145LR · Emergency Lighting
  > IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHTS FROM ROW 12 AFT WERE INOPERATIVE. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA04BT040](https://openairdocs.org/sdr/C2XA04BT040.md): Bulb · burned out · Mar 27, 2004 · N13949 · Emb EMB145LR · Emergency Lighting
  > CREW REPORTED, SERVICE DOOR EMERGENCY LIGHT BULB BURNED OUT. MAINTENANCE REMOVED AND REPLACED LIGHT BULB IAW EMB145 AMM 33-50-06. OPS CHECKED GOOD.
- [SDR C2XA04CL004](https://openairdocs.org/sdr/C2XA04CL004.md): Engine · failed · Jan 14, 2004 · N13949 · Emb EMB145LR · Engine (Turbine/Turboprop)
  > EWR FLT 2247, THE CREW REPORTED A LOUD BANG FROM NR 2 ENGINE, ITT WENT TO 900 CELSIUS. POWER WAS REDUCED, TEMP STAYED AT 900 CELSIUS FOR 5 SECONDS, THEN ENGINE NR 2 FLAMED OUT. AIRCRAFT DIVERTED TO CLE AND LANDED WITHOUT FURTHER DIFFICULTY. NR 2 ENGINE WAS
- [SDR C2XA03BT091](https://openairdocs.org/sdr/C2XA03BT091.md): Battery Pack · faulty · Sep 13, 2003 · N13949 · Emb EMB145LR · Emergency Lighting
  > CREW REPORTED, "EMERGENCY EXIT SIGN BACKLIGHT INOPERATIVE ABOVE SEAT 1A. MAINTENANCE REMOVED AND REPLACED NR 1 EMERGENCY EXIT LIGHT BATTERY PACK. IAW EMB145 AMM #33-50-04. OPS.CHECKED GOOD.
- [SDR C2XA03SH051](https://openairdocs.org/sdr/C2XA03SH051.md): Stringer · gouged · Mar 10, 2003 · N13949 · Emb EMB145LR · Fuselage Structure (General)
  > SHV DURING C CHECK REPAIR DOUBLER ON T REINFORCEMENT ON STRINGER 19 RIGHT BETWEEN FRAMES 52 TO 53 WAS FOUND GOUGED. MAINTENANCE REMOVED DAMAGED AND PERFORMED A DOUBLER REPAIR IAW EMB SRM 53-24-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA03SH045](https://openairdocs.org/sdr/C2XA03SH045.md): Stringer · gouged · Mar 10, 2003 · N13949 · Emb EMB145LR · Fuselage Structure (General)
  > SHV DURING C CHECK REPAIR DOUBLER ON T REINFORCEMENT ON STRINGER 19 LEFT WAS FOUND TO HAVE A GOUGE BETWEEN FRAMES 52 TO 53. MAINTENANCE REMOVED DAMAGE AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVIC

Next page: https://openairdocs.org/deregistered/N13949-2023-03-03/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 = 'N13949' AND deregistration_id = 'N13949-2023-03-03'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N13949-2023-03-03/reports

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