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 = 'N220SW' 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.
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 = 'N220SW' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR SWIA200921014Sign · brokenFLT 5568 - EMERGENCY EXIT SIGN AT ROW 9 BROKEN. REPLACED EMERGENCY EXIT SIGN.SDR SWIA200819457Frame · corrodedFOUND CORROSION AT FRAME 21 AT LOWER RIGHT SIDE. REPAIRED IAW IC2008-12/02091.
SDR SWIA200819406Smoke Detector · malfunctionedFLT 5560 - INTERMITTENT SMOKE LIGHT WHEN TESTING CARGO SMOKE SYSTEM. REPLACED NR 2 CARGO SMOKE DETECTOR, PN 473597-13, SN/OFF 1144.
SDR SWIA200718260Battery · unknownEMERGENCY LIGHTS CIRCUIT BREAKER POPS WITH THE SWITCH IN THE OFF POSITION. REPLACED THE FORWARD EMERGENCY LIGHT BATTERY. SYSTEM TESTS GOOD.SDR SWIA200718029Cooling Fan · smokeAPU BLEED AIR CAUSES PACKS TO SMOKE. REPLACED LEFT GROUND COOLING FAN. OPERATIONAL CHECKS GOOD.SDR SWIA200617351Support · crackedRT UPPER INSTRUMENT PANEL SUPPORT ON AIRFRAME SIDE IS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED RT UPPER INSTRUMENT PANEL SUPPORT BRACKET ON AIRFRAME IAW SRM 51-40-02.SDR SWIA200617350Mount · corrodedSEAT TRACK FOR FWD GALLEY MOUNT CORRODED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED SEAT TRACK SECTION WITH NEW.SDR SWIA200617349Pitot Tube · corrodedBOTH RT PITOT TUBE HAVE EXCESSIVE CORROSION, DISCOVERED DURING C-CHECK INSPECTION. REPLACED BOTH RT PITOT TUBES. OPERATIONAL CHECKS GOOD.SDR SWIA200617196Wire · brokenEMERGENCY EXIT SIGN OVER SEAT 9B INOP. REPAIRED BROKEN WIRE IN OVERHEAD LIGHT. OPERATIONAL CHECKS GOOD.SDR SWIA200515920Battery Pack · dischargedEMERGENCY LIGHTS WILL NOT TEST. REPLACED 3 ELBP'S. OPERATIONAL CHECK GOOD, FWD SN 059 OFF; MID SN 1161 OFF; AFT SN 1035 OFF.SDR SWIA200515644Selector · malfunctionedDURING CRUISE FLIGHT AT FL220 FLAP CONTROL FAULT O/B FLAP SECOND LIGHT SEGMENT FLASHING. REPLACED FCU AND FLAP CONTROL HANDLE ASSY, OPERATIONAL CHECK GOOD. P/N: 347200-1001, S/N: OFF 0217.SDR SWIA200515442Lamp · burned outEMERGENCY LIGHTS BY MCD OUT. INSTALLED SERVICEABLE LAMP. OPERATIONAL CHECK GOOD.SDR SWIA200515362Wire · brokenEMERGENCY EXIT SIGN OVER ROW 9 INOP. REPAIRED BROKEN WIRE AT ROW 9 EMERGENCY LIGHT. OPERATIONAL CHECK GOOD.SDR SWIA200514544Handle · malfunctionedON DEPARTURE, FLAPS DID NOT FULLY RETRACT. REPLACED FLAP HANDLE. OPERATIONAL CHECK GOOD.SDR SWIA200514543Connector · looseFOUR FLOOR LEVEL EMERGENCY LIGHTS OUT. RECONNECTED LIGHT CONNECTOR UNDER FLOOR AT SEAT 3A, OPERATIONAL CHECKS NORMAL.SDR SWIA200414290Control Module · malfunctionedLEFT FIRE PIPE ZONE LIGHT FLICKERED AFTER GEAR EXTENSION. REPLACED LEFT WHEEL WELL ENGINE DETECTION CONTROL MODULE. OPERATIONAL CHECKS GOOD.SDR SWIA200413086Ahrs · malfunctionedCAPTAIN'S AUTOPILOT FAILED FFOD CHECK AND COMPUTER FLAG STAYS IN VIEW. INSPECTED APC NR 1, NR 1 AHRS AND ADI NR 1 WIRING AND CONNECTORS. NO DEFECTS NOTED. CONTINUOUSLY TESTED AND NO FAULTS FOUND. REMOVED AND REPLACED NR 1 AHRS FOR TROUBLESHOOTING. OPS CHESDR SWIA200312608Power Supply · failedF/A REPORTS THAT 3 TIMES DURING THE FLIGHT SOME OF THE EMERGENCY LIGHTS ILLUMINATED FOR 30-60 SEC BEFORE GOING OUT. NO ABNORMAL INDICATIONS IN THE COCKPIT. REPLACED FORWARD ELBP BATTERY PACK. OPS CHECKS GOOD. S/N OFF: 1041-02/92.SDR SWIA200312370Tire · blownALL 4 MAIN TIRES BLEW ON LANDING. REMOVED AND REPLACED ALL 4 MLG WHEEL ASSY'S PER MM 32-44-02 AND C/W ST12-311. P/N: 3-1446-1, NR 1 S/N ON: 0966, S/N OFF: 1789, NR 2 S/N ON: 0618, NR 3 S/N ON: 0627 S/N OFF: 1101, NR 4 S/N ON: 0005, S/N OFF: 1729.SDR SWIA200312067Skin · crackedANGLE BEHIND CAPTAIN'S DV WINDOW CUTOUT CRACKED. DISCOVERED DURING C-CHECK. REPLACED BRACKET IAW SRM 120 51-10-02.SDR SWIA200312066Frame · crackedAT FRAME 13, BELOW FLOOR COCKPIT ENTRY DOOR, BOTH FRAME DOUBLERS CRACKED. DISCOVERED DURING C-CHECK. DOUBLERS APPLIED TO AREAS MENTIONED IAW SRM 120 51-10-02.SDR SWIA200312065Bracket · crackedRIGHT INBOARD LOWER FLAPWELL, INBOARD ROLLER BRACKET CRACKED. DISCOVERED DURING C-CHECK. REPLACED AFFECTED BRACKET IAW EMB120 SRM 51-10-02.SDR SWIA200311893Servo · bindingRUDDER PEDALS MAKE A LOUD GRINDING NOISE WHEN THEY ARE MOVED. REMOVED RUDDER TO INSPECT. FOUND SERVO TO MAKE GRINDING NOISE AND ALSO FOUND IT TO BE BINDING. REPLACED SERVO WITH SERVICEABLE UNIT. AUTOPILOT OP CHECKS GOOD.SDR SWIA200211482Battery Pack · dischargedAFT SECTION OF CABIN EMERGENCY LIGHTS ARE INOP. INSTALLED SERVICEABLE BATTERY PACK. OPS CHECK GOOD.SDR SWIA200210802Wire · brokenFLAP CONTROL FAULT ON FLAP INDICATOR PANEL AND FLAP/ADVANCED STALL WARNING ON MAP. ABORTED TAKEOFF. REPAIRED BROKEN WIRE AT NR 8 PIN ON LEFT OUTBOARD ACTUATOR. OPERATED FLAPS. OPS CHECK GOOD.SDR SWIA200210760Battery Pack · dischargedEMERGENCY LIGHTS AT ROW 6 AND FLOOR LIGHTING AT ROWS 3, 4 & 5 ARE INOPERATIVE. REPLACED CENTER BATTERY PACK PER 33-50-00. OPS CHECK GOOD.SDR SWIA200110381Wire · brokenON TAXI OUT FLAP CONTROL FAULT INDICATION OCCURRED UPON FLAP DEPLOYMENT TO 15 DEGREES. LEFT LVDT FLR ON ANNUNCIATOR OUTBOARD PAIR. FOUND BROKEN WIRE AND REPAIRED ON LEFT OUTBOARD FLAP ACTUATOR CANNON PLUG. OPS CHECK GOOD ON FLAP EXTENSION AND RETRACTION.SDR SWIA200110078Fuse · failedFOUR FLOOR EMERGENCY LIGHTS OUT BY ROW 8.INSTALLED SERVICEABLE FUSE. OPS CHECK GOOD.SDR SWIA972494Actuator · failedAT 21,000 AILERON TRIM WAS FOUND TO BE JAMMED. OAT WAS -10C DEGREES. AFTER LANDING THE TRIM SEEMED TO BE OPERATIONAL AGAIN. REPLACED AILERON TRIM TAB ACTUATOR IAW 120 MM 27-12-01. OPS CHECK GOOD. P/N: 5301, S/N ON: 411, S/N OFF: 373.SDR SWIA971754Valve · failedBLUE SYSTEM LOW PRESS LIGHT ILLUMINATED AFTER TAKEOFF. RETURNED TO PDX. REPLACED MOISTURE PURGE VALVE IAW MM 29-14-00, OPS CHECK GOOD.SDR SWIA971707Pedel · stuckAFTER TAKEOFF, ATTEMPTED TO USE RIGHT RUDDER AND RUDDER PEDAL, COULD NOT BE MOVED FOR RIGHT RUDDER DEFLECTION MORE THAN ABOUT 12. RETURNED TO YUM. DURING RETURN TO AIRPORT, RUDDER PEDALS BROKE LOOSE AND OPERATION RETURNED TO NORMAL. ALL HYDRAULIC AND RUDDERSDR SWIA971680Sensor · out of positionDURING CLIMB AT 2000 MSL, A TRIPLE CHIME SOUNDED FOLLOWED BY A DUCT LEAK AURAL WARNING. APU DUCT LEAK LIGHT WAS ILLUMINATED AS WAS THE DUCT LEAK LIGHT ON THE MAP. APU WAS NOT IN OPERATION. QRH PROCEDURES WERE FOLLOWED AND FLIGHT RETURNED TO SEA. ALL LIGHTSSDR SWIA971636Sequence Valve · failedRIGH MAIN LANDING GEAR DID NOT RETRACT AFTER TAKEOFF. RETURNED TO FAT. REPLACED AND ADJUSTED RIGHT MAIN LANDING GEAR SEQUENCE VALVES. OPS CHECKS GOOD ON GROUND.SDR SWIA971635Actuator · failedRIGHT MLG WILL NOT RETRACT AFTER TAKEOFF. RETURNED TO FAT. REMOVED AND REPLACED RIGHT MAIN GEAR ACTUATOR, PERFORMED GEAR SWING.SDR SWIA971391Selector · failedFLAPS WOULD NOT RETRACT AFTER TAKEOFF (DISAGREEMENT). RETURNED TO LAX. REPLACED FLAP SELECTOR WITH SERVICEABLE UNIT. OPERATED NUMEROUS TIMES, OPS CHECK GOOD.SDR SWIA971425Valve · failedRIGHT AND LEFT MIDDLE WING DEICE BOOTS FAILED DURING CLIMBOUT (FIRST FLIGHT CHECKS ON GROUND PRIOR TO FLIGHT OPERATION NORMALLY). RETURNED TO SFO. REPLACED RIGHT AND LEFT MIDDLE WING DEICE BOOT EJECTOR VALVE. OPS CHECKED GOOD. NO LEAKS NOTED UPON INSPECTIOSDR SWIA971305Boot · failedRIGHT ENGINE AIR INLET DEICE FAILED IN FLIGHT. RETURNED TO FIELD BECAUSE OF ICING IN AREA. REPLACED RIGHT ENGINE AIR INLET DEICE BOOT PRESSURE SWITCH. OPS CHECK GOOD.SDR SWIA971201Seat Track · corrodedCORROSION ON SEAT TRACK NEAR GALLEY AREA. REMOVED CORRODED PORTION OF SEAT TRACK AND FABRICATED NEW LEFT SEAT TRACK NEAR GALLEY AREA.SDR SWIA971200Seat Track · corrodedCORROSION ON SEAT TRACK NEAR LAV AREA. REPLACED SEAT TRACK AS REQUIRED.SDR SWIA971199Sill · corrodedRIGHT SIDE FORWARD HAS CORROSION. INSTALLED RIGHT SIDE FORWARD WITH NEW SILL IAW SRM 51-40-00.SDR SWIA971103Rollers · lack of lubeDEPARTED LAX, UPON FLAP RETRACTION FLAP DISAGREEMENT OCCURRED, SLIGHT ROLL WAS FELT DURING RETRACTION. FOLLOWED QRH INSTRUCTIONS, DID NOT SOLVE. RETURNED TO LAX. CHECKED FAULT CODES, LUBED FLAP ROLLERS AND CYCLED FLAPS 10 TIMES AND OPS CHECKS GOOD.SDR SWIA971089Actuator · dirtyTRIM WHEEL FROZEN IN FLIGHT, WHICH KICKED AUTO PILOT OFF DUE TO TRIM FAILURE. DESCENDED TO LOWER ALTITUDE WHERE TRIM RETURNED TO NORMAL OPERATION. CLEANED AUTO HUB BOTH LEFT AND RIGHT ELEVATOR TRIM ACTUATOR. OPS CHECKS GOOD ON GROUND.SDR SWIA97998Indication · malfunctionedAFTER TAKEOFF UPON FLAP RETRACTION, THERE WAS A FLAP DISAGREEMENT INBOARD PAIR. THE CHECK LIST WAS ACCOMPLISHED AND THE FLAPS AGAIN DISAGREED SO WE RETURNED TO LAX. CLEANED INBOARD FLAP TRACKS, ACTUATOR CANNON PLUGS, AND ALSO RERACKED FLAP CONTROL BOX, CYCLESDR SWIA97925Regulator · failedAFTER TAKEOFF, LEFT DUCT LEAK LIGHT CAME ON AND CABIN PRESSURE WAS LOST. RETURNED TO PSP. LIGHT STAYED ON WITH ENGINE SHUT DOWN. REPLACED LEFT 18 PSI REGULATOR, OPS CHECKS GOOD WITH NO DUCT LEAK INDICATION NOTED.SDR SWIA97891Inverter · failedAFTER TAKEOFF BOTH AHRS SHOWED GYRO AND COMPUTER FLAGS. NR 1 ADI CIRCUIT BREAKER OPENED. RETURNED FOR LANDING. AFTER LANDING, GYRO FLAGS DISAPPEARED BUT COMPUTER FLAG REMAINED ON CAPTAINS ADI. REPLACED NR 1 INVERTER. BOTH AHRS AND ADI'S CHECKED NORMAL WITSDR SWIA97821Actuator · failedIN CRUISE, ADVANCE STALL WARNING AND FLAP CONTROL FAULT LIGHTS ILLUMINATE. COULD NOT RESET. NACELLE FLAPS SHOW A PAIR OF LIGHT BARS FLASHING. RETURNED TO SLC. REMOVED AND REPLACED RIGHT NACELLE FLAP ACTUATOR IAW MM 27-50-08. CHECKS GOOD.SDR SWIA97819Flap Contl Comp · failedFLAP CONTROL FAULT LIGHT AND ADVANCED STALL WARNING LIGHT ILLUMINATED IN CRUISE FLIGHT, WOULD NOT RESET. REMOVED AND REPLACED FLAP CONTROL COMPUTER IAW MM 27-50-06. RAN FLAPS THROUGH SEVERAL CYCLES IAW MM 27-50-00. ADVANCED STALL WARNING SYSTEM ,OPS CHECKS SDR SWIA95674Regulator Vlv · malfunctionedDUCT LEAKAGE LIGHT ILLUMINATED IN FLIGHT, PROCEEDED WITH ENGINE SHUTDOWN. FOUND GASKET NR 2 ENGINE BLOWN ON RT SIDE OF 18 PSI REGULATOR FOR DE-ICE SYSTEM. REPLACED 18 PSI REGULATOR VALVE. RAN RT ENGINE TO TAKEOFF POWER AND OPS CK GOOD.
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