N234SW

Service difficulty reports not matched to an aircraft · 127

They name N234SW, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. Newest first.

Query with SQL
duckdb -csv -c "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 = 'N234SW' AND registry_match IS NULL
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR SWIA201025085Sign · brokenLOWER EMERGENCY EXIT SIGN BROKEN AT 6C. (FLT 6754) REPLACED THE LOWER EMERGENCY EXIT SIGN AT 6 C.Oct 22, 2010 · N234SW · Emb EMB120ER · Emergency LightingSDR SWIA201024962Skin · corrodedFUSELAGE BELLY SKIN AFT OF APU BLEED DUCT FORWARD MOST MOUNT, MARKED, APPEARS EXFOLIATED. (C-CHECK) REPAIRED SKIN PER APPROVED REPAIR IC2003-120/3960 AND SRM.Aug 17, 2010 · N234SW · Emb EMB120ER · Fuselage Main, Plate/SkinSDR SWIA201024477A/C Pack · smokeWHEN POWER REDUCED FOR DESCENT, LEFT PACK PRODUCED SMOKE. (FLT 6840) OPERATIONAL CHECKS NORMAL WITH ALL BLEED SOURCES.Jun 26, 2010 · N234SW · Emb EMB120ER · Cabin Cooling SystemSDR SWIA201024114Frame · crackedLEFT FORWARD FUSELAGE FRAME AT STA 1030.0 IS BENT AND CRACKED. (FLT 6843) INSTALLED DOUBLER PER SRM.Apr 20, 2010 · N234SW · Emb EMB120ER · Fuselage Main, FrameSDR SWIA200923130Light · inoperativeEMERGENCY LIGHT AT ROW 7 INOP. (FLT 6172) RELAMPED EMERGENCY LIGHT.Nov 14, 2009 · N234SW · Emb EMB120ER · Emergency LightingSDR SWIA200922745Connector · not seatedLAST THREE ROWS OF FLOOR EMERGENCY LIGHTS INOP. (FLT 6687) RESEATED CONNECTOR.Sep 21, 2009 · N234SW · Emb EMB120ER · Light System WiringSDR SWIA200922434Linkage · failedNOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. (FLT 6191) REPLACED NOSE LANDING GEAR RIGHT SIDE DOOR LINK ATTACH FITTING.Aug 21, 2009 · N234SW · Emb EMB120ER · Landing Gear Door Retract SectionSDR SWIA200922240Wire · looseLAST FIVE FLOOR EMERGENCY LIGHTS INOP. (FLT 6292) RESECURED WIRES ON LIGHT STRIP CONNECTOR.Jul 24, 2009 · N234SW · Emb EMB120ER · Light System WiringSDR SWIA200921494Rccb · overheatedFLT 6300 - RIGHT PROP RCCB OVERHEATED. REPLACED RCCB.Apr 21, 2009 · N234SW · Emb EMB120ER · Propeller/Rotor Anti-Ice/De-Ice SystemSDR SWIA200921503A/C Pack · smokeFLT 6202 - LEFT PACK CAUSING SMOKE. RAN LEFT PACK WITH ALL BLEED SOURCES AND COULD NOT DUPLICATE.Apr 18, 2009 · N234SW · Emb EMB120ER · Cabin Cooling SystemSDR SWIA200921457Rccb · smokeFLT 6355 - SMOKE IN CABIN ON SHUTDOWN. REPLACED RIGHT GROUND COOLING FAN RCCB.Apr 18, 2009 · N234SW · Emb EMB120ER · Air Distribution FanSDR SWIA200921364Fan · smokeFLT 6454 - LEFT PACK AND GROUND COOLING FAN INTRODUCED SMOKE INTO CABIN. OPERATIONAL CHECK NORMAL.Mar 29, 2009 · N234SW · Emb EMB120ER · Air Distribution FanSDR SWIA200821095Seat Track · corrodedC-CHECK, CABIN LEFT AND RIGHT SIDE SEAT TRACKS CORRODED. SPLICED IN LEFT SIDE SEAT TRACK SECTION, CLEANED AND TREATED RIGHT SIDE TRACK.Dec 3, 2008 · N234SW · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR SWIA200819806Light · brokenEMERGENCY EXIT LIGHT AT ENTRY DOOR IS BROKEN. REPLACED EMERGENCY LIGHT AS REQUIRED. OPS CHECK GOOD. Jun 16, 2008 · N234SW · Emb EMB120ER · Emergency LightingSDR SWIA200819631Sign · brokenEXIT SIGN AT ROW 6 IS BROKEN. REPLACED EXIT SIGN ASSEMBLY WITH A SERVICEABLE UNIT. OPS CHECK GOOD.May 15, 2008 · N234SW · Emb EMB120ER · Emergency LightingSDR SWIA200718628Lamp · burned outRIGHT OVERWING EMERGENCY EXIT SIGN IS NOT ILLUMINATING, FLIGHT NR 5737. RELAMPED EMERGENCY EXIT SIGN. OPS CHECKED GOOD.Aug 23, 2007 · N234SW · Emb EMB120ER · Emergency LightingSDR SWIA200718248Battery Pack · inoperativeFORWARD SECTION OF EMERGENCY FLOOR LIGHTING IS INOP. REPLACED FORWARD ELBP IAW 33-50-02 EMB MM.May 19, 2007 · N234SW · Emb EMB120ER · Emergency LightingSDR SWIA200718419Seat Track · corrodedRIGHT SIDE SEAT TRACK IS CORRODED IN SEVERAL AREAS, DISCOVERED AT C-CHECK. REPLACED RIGHT SIDE FORWARD SEAT TRACK WITH SERVICEABLE UNIT.May 1, 2007 · N234SW · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR SWIA200718418Rib · crackedLEFT INBOARD LEADING EDGE RIB IS CRACKED, DISCOVERED AT C-CHECK. REPLACED RIB IAW EMB 120 SRM 51-10-02 PG 2 SECT 2B AND 51-40-02.May 1, 2007 · N234SW · Emb EMB120ER · Wing, Rib/BulkheadSDR SWIA200718417Rib · crackedRIGHT INBOARD LEADING EDGE RIB IS CRACKED, DISCOVERED AT C-CHECK. REPLACED RIB IAW EMB 120 SRM 51-10-02 PG 2 SECT 2B AND 51-40-02.May 1, 2007 · N234SW · Emb EMB120ER · Wing, Rib/BulkheadSDR SWIA200718416Rod End · corrodedLEFT ELEVATOR TRIM INPUT ROD-ENDS HAVE CORROSION, DISCOVERED AT C-CHECK. REPLACED LEFT ELEVATOR TRIM INPUT ROD-ENDS IAW AMM 27-32-01, P/N NAS659-4-7.May 1, 2007 · N234SW · Emb EMB120ER · Elevator Tab Control SystemSDR SWIA200718415Torque Tube · corrodedLEFT ELEVATOR TORQUE TUBE INBOARD BEARING HAS PITTING CORROSION, DISCOVERED AT C-CHECK. REPLACED LEFT ELEVATOR TORQUE TUBE INBOARD BEARING IAW EMB 120 MM 20-40-03, P/N MS27648-33.May 1, 2007 · N234SW · Emb EMB120ER · Elevator Control SystemSDR SWIA200718414Seat Track · corrodedRIGHT SIDEWALL SEAT TRACK IS CORRODED IN SEVERAL AREAS, DISCOVERED AT C-CHECK. REPLACED RIGHT SIDEWALL SEAT TRACK ASSEMBLY, P/N 120-15997-603.May 1, 2007 · N234SW · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR SWIA200718067Frame · crackedLEFT MLG OUTBOARD AFT DOOR AFT ATTACH ARM UPPER ATTACH POINT NACELLE FRAME CRACKED, DISCOVERED DURING A-CHECK INSPECTION. INSTALLED SERVICEABLE HALF-FRAME ON LEFT OUTBOARD AFT NACELLE IAW SRM 51-40-02. OPERATIONAL CHECKS GOOD.Mar 25, 2007 · N234SW · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/RibSDR SWIA200617455Windshield · crackedF/O WINDSHIELD CRACKED. REPLACED F/O WINDSHIELD IAW MM 56-10-01 AND RII 56-220-1000.Dec 22, 2006 · N234SW · Emb EMB120ER · Flight Compartment WindowsSDR SWIA200617270Wire · failedEXIT LIGHT AT 9BC OVERHEAD BIN IS INOP. REPAIRED BROKEN WIRE ON EMERGENCY EXIT SIGN. OPERATIONAL CHECKS GOOD.Oct 14, 2006 · N234SW · Emb EMB120ER · Light System WiringSDR SWIA200617140Connector · faultyONE EMERGENCY FLOOR LEVEL WHITE LIGHT IS INOP BY SEAT 3A. REPLACED CONNECTOR FOR FLOOR EMERGENCY LIGHT AT 3A. OPERATIONAL CHECKS GOOD.Aug 31, 2006 · N234SW · Emb EMB120ER · Light System WiringSDR SWIA200616584Bushing · wornON DESCENT FROM FL250 WITH TORQUE AT 61 PERCENT A VIBRATION WAS FELT. REPLACED LEFT AILERON HINGE AND BUSHING IAW MM 57-00-00, REMOVED AND REPLACED RIGHT AILERON TRIM TAB IAW EMB 120 MM 27-72-02.Apr 17, 2006 · N234SW · Emb EMB120ER · AileronsSDR SWIA200616577Servo · malfunctionedTRIM LIGHT ON AUTOPILOT ENGAGE PANEL ILLUM INFLIGHT. REPLACED RUDDER SERVO IAW 22-00-00. OPERATIONAL CHECK GOOD.Apr 8, 2006 · N234SW · Emb EMB120ER · Autopilot Trim ServoSDR SWIA200515133Actuator · malfunctionedWHEN RETRACTING FLAPS AFTER LANDING, FLAP DISAGREEMENT. R & R LT NACELLE FLAP ACTUATOR IAW 27-50-00 CMM. OPS CHECK GOOD.Jun 13, 2005 · N234SW · Emb EMB120ER · Trailing Edge Flap ActuatorSDR SWIA200414304Actuator · malfunctionedDURING TAKEOFF ROLL, EXPERIENCED CONTINUOUS RAPID STIFFENING/RESISTANCE IN RUDDER PEDALS. REPLACED BLUE SYSTEM RUDDER ACTUATOR WITH A SERVICEABLE UNIT IAW EMB M/M 27-22-02. OPERATIONAL CHECK GOOD.Dec 17, 2004 · N234SW · Emb EMB120ER · Rudder Control SystemSDR SWIA200413756Wire · damagedAFT MOST WHITE LIGHT ON FLOOR EMERGENCY LIGHTS INOPERATIVE. REPAIRED WIRING AND RELAMPED EMERGENCY LIGHT IAW MM 33-51-02. OPERATIONAL CHECK GOOD.Aug 27, 2004 · N234SW · Emb EMB120ER · Light System WiringSDR SWIA200413642Control Unit · malfunctionedON TAXI OUT RECEIVED FLAP & ADVANCE SWS LIGHT ON MAP. REMOVED AND REPLACED FLAP CONTROL UNIT. OPERATIONAL CHECK GOOD IAW 27-50-00.Jul 24, 2004 · N234SW · Emb EMB120ER · Trailing Edge Flap Control SystemSDR SWIA200413602Wire · brokenLEFT SIDE FLOOR REAR ROW EMERGENCY LIGHT DOES NOT ILLUMINATE. REPAIRED WIRING TO AFT FLOOR EMERGENCY LIGHT. EMERGENCY LIGHTS OPERATE NORMALLY.Jul 21, 2004 · N234SW · Emb EMB120ER · Light System WiringSDR SWIA200413601Servo · malfunctionedAUTOPILOT DOESN'T CAPTURE ALTITUDES. REPLACED AUTOPILOT ELEVATOR SERVO PER MM 22-10-05. OPERATIONAL CHECK GOOD PER MM 22-11-00.Jul 20, 2004 · N234SW · Emb EMB120ER · Autopilot Main ServoSDR SWIA200413120Frame · corrodedFRAME 36 RIGHT SIDE FLOOR STRAP CORRODED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED FRAME AT RIGHT SIDE FLOOR STRAP IAW SRM 120 51-10-02 PG 3 SEC 3A.Mar 17, 2004 · N234SW · Emb EMB120ER · Fuselage Main, FrameSDR SWIA200413119Frame · crackedCARGO DOOR UPPER FORWARD INBOARD FRAME CRACKED AT BACKSTOP BRACKET SUPPORT. DISCOVERED DURING C-CHECK INSPECTION. NEW FRAME INSTALLED IAW SRM120 51-10-02 PG 3 SEC 3A.Mar 17, 2004 · N234SW · Emb EMB120ER · Cargo/Baggage DoorsSDR SWIA200413118Seat Track · corrodedCORROSION ON LEFT FLOOR SEAT TRACK IN VARIOUS SPOTS. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED FORWARD AND AFT SECTIONS OF LEFT FLOOR SEAT TRACK WITH NEW IAW EMB120 MM 53-01-05.Mar 17, 2004 · N234SW · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR SWIA200413117Floorbeam · corrodedCABIN FLOORBOARD FRAMES HAVE CORROSION AT FRAME 38. DISCOVERED DURING C-CHECK INSPECTION. REPLACED FRAME AT CABIN FLOOR IAW SRM 120 51-10-02 PG 3 SEC 3.A.Mar 17, 2004 · N234SW · Emb EMB120ER · Fuselage Main, Floor BeamSDR SWIA200412986Servo · malfunctionedWHEN AUTOPILOT ENGAGED ON FIRST OFFICER'S SIDE, THE AIRCRAFT ABRUPTLY LEVELS OFF 300 FEET PRIOR TO SELECTED ALTITUDE. REPLACED ELEVATOR SERVO AS REQUIRED. SYSTEM OPS CHECKS GOOD IAW 22-10-00.Mar 2, 2004 · N234SW · Emb EMB120ER · Autopilot Main ServoSDR SWIA200412891Computer · faultyFIRST OFFICERS' AUTOPILOT FAILED AND THE ELEVATOR SERVO LIGHT ILLUMINATED. CHECKED ASSOCIATED WIRING ON CONNECTORS BEHIND APC NR 2, NO DEFECTS. REMOVED AND REPLACED APC NR 2. OPS CHECK GOOD ON GROUND OPERATIONS IAW MM 22-10-00.Feb 11, 2004 · N234SW · Emb EMB120ER · Autopilot ComputerSDR SWIA200412741Actuator · malfunctionedIN CRUISE AT 22K FT, A/C STARTED TO PITCH UP SLOWLY AND AIR SPEED WAS BLEEDING OFF AT 160 KTS. REPLACED BOTH ELEVATOR TRIM ACTUATORS IAW EMB 120 MM 27-32-02. ALSO REPLACED VERTICAL STAB LEADING EDGE DEICE BOOT. OPS CHECK GOOD. ACTUATOR S/N OFF LEFT SIDE: Jan 2, 2004 · N234SW · Emb EMB120ER · Elevator Tab Control SystemSDR SWIA200312611Computer · malfunctionedF/O ADI SHOWS COMPUTER FLAG. AUTO PILOT DOES NOT ENGAGE ON F/O SIDE. REPLACED APC-65B. OPS CHECKS GOOD.Nov 18, 2003 · N234SW · Emb EMB120ER · Autopilot SystemSDR SWIA200312383Switch · inoperativeFO AUTOPILOT WILL NOT ENGAGE.REPLACED FO AP DISCONNECT SWITCH. SYSTEM OPS CHECK GOOD IAW 22-10-00.Sep 8, 2003 · N234SW · Emb EMB120ER · Autopilot SystemSDR SWIA200312304Servo · malfunctionedCAPT REPORTS A/P WILL NOT CAPTURE ALTITUDE AS GIVEN ON THE ALT ALERTER. REPLACED ELEVATOR SVO65 SERVO WITH SERVICEABLE UNIT. OPS CHECK GOOD.Aug 22, 2003 · N234SW · Emb EMB120ER · Autopilot Main ServoSDR SWIA200311989Wire · looseEXIT SIGN ON SEAT 1 C&B OUT.SECURED LOOSE WIRE CONNECTION ON EXIT SIGN AT SEAT 1 CB. OPS CHECK GOOD.May 20, 2003 · N234SW · Emb EMB120ER · Light System WiringSDR SWIA200311851Relay · malfunctionedAFTER TAKEOFF WITH AUTOPILOT SELECTED TO CAPTAIN'S SIDE, TRIM FAIL ILLUMINATED ON MAP MOMENTARILY, BUT THEN EXTINGUISHED. AUTOPILOT WAS ENGAGED; ON DESCENT PLANE PITCHED DOWN AND LIGHT CAME ON AGAIN. REPLACED TRIM PROXIMITY RELAY K0393. BOTH AUTOPILOT FLIGHMar 23, 2003 · N234SW · Emb EMB120ER · Autopilot SystemSDR SWIA200311850Computer · malfunctionedAUTOPILOT AND CAPTAIN'S FLIGHT DIRECTOR PITCHES UP AND DOWN 300 FT PRIOR TO LEVEL OFF. REPLACED AUTOPILOT COMPUTER APC-65B WITH SERVICEABLE UNIT. TESTED AND OPS CHECK GOOD.Mar 22, 2003 · N234SW · Emb EMB120ER · Autopilot SystemSDR SWIA200211628Wire · frayedDURING FIRST FLIGHT OF THE DAY AUTOPILOT TEST, RECEIVED -YAW DIS- ON FIRST OFFICER'S FLIGHT CONTROL PANEL AND ASSOCIATED -YAW DIS- ON AP CONTROL PANEL. ALSO -R- ON AUTOPILOT CONTROL PANEL. UPON INSPECTION FOUND RUDDER TRIM ACTUATOR CABLE WIRE FRAYED AND BINDDec 23, 2002 · N234SW · Emb EMB120ER · Flight Control System WiringSDR SWIA200211598Wire · burnedBURNING ODOR STARTED 20 MIN INTO FLIGHT. PACKS WERE TURNED OFF ONE AT A TIME TO ISOLATE THE PROBLEM. ODOR STILL REMAINED AND AT FL240 PRESSURE COULD NOT BE MAINTAINED ON ONE PACK. FOUND NUT LOOSE AT RCCB, CB0256 FOR BLUE HYDRAULIC AUX PUMP, AND BURNED WIRE.Dec 16, 2002 · N234SW · Emb EMB120ER · Hydraulic Power System Wiring
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