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 aircraft_model_key = '1900D' 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 aircraft_model_key = '1900D' 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 GUUA95457060309ASkin · corrodedDURING SCHEDULED ROUTINE INSP, RT WING OTBD L/E SKIN IS BULGING DUE TO CORROSION AT RWS 276.01. REMOVED CORRODED SKIN AND INSTALLED DOUBLER REPAIR.SDR GLBA200906031Shutoff Valve · deterioratedAT 400 FT, TURNED BLEEDS ON AN LT ENVIRO FAIL ANNUN ILLUMINATED, TRIED TO RESET SEVERAL TIMES IAW THE CHECKLIST, DID NOT RESET, RETURNED TO DEPARTURE AND TRANSFERED THE ISSUE TO DML NR 35433 PER MEL 21-14 CAT C ALL O PROCEDURES COMPLIED WITH. MX REMOVED AND RSDR GUUA95152060209ADoor · stiffFLIGHT: 9245, PILOT REPORTED AIRSTAIR DOOR DIFFICULT TO CLOSE. PERFORMED AIRSTAIR DOOR RIGGING OPS CHECK, OK.SDR GUUA95457060209ASkin · corrodedDURING SCHEDULED ROUTINE INSP, DISCOVERED RT T/E SKIN FWD OF OTBD FLAP SHOWS SIGNS OF EXFOLIATION WS 138.36 TO WS 196.06. REMOVED DAMAGED, SKIN FABRICATED AND INSTALLED EXTERNAL REPAIR DOUBLER.SDR GUUA94057060209ASkin · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED RT WING UPPER SKIN AREA EXFOLIATED AT RWS 136.86. REMOVED DAMAGED SKIN AND INSTALLED AN EXTERNAL REPAIR DOUBLER.SDR GLBA200906011Indicator · malfunctionedNR 2 TORQUE GAUGE DROPPED TO 0 ON TAKEOFF ROLL. THE NR 2 TORQUE GAUGE DROPPED TO ZERO. MX REMOVED AND REPLACED THE NR 2 TORQUE GAUGE IAW MM 31-10-00. OPS CHECK WAS GOOD.SDR GLBA20090530AAltimeter · intermittentUPON CLIMBING OUT, THE PILOTS REPORTED THAT THE CAPTAINS ALTIMETER FAILED, HOWEVER, IT WAS NORMAL AFTER FIVE MINUTES. MX REMOVED AND REPLACED THE CAPTAINS ENCODING ALTIMTER IAW GMM 9.7.0, FAR 43 APPENDIX (E)AND(C)(A). MX PERFORMED PITOT STATIC CHECKS IAW BMM 2SDR GLBA20090531FCircuit Board · inoperativeTHE PILOTS REPORTED THAT THE AFX SYS FEATHERED THE NR 1 PROPELLER WHILE ON FINAL WITH PROPS FULL FWD AND TORQUE AT 1000 LBS. MX REMOVED AND REPLACED THE A123 PRINTED CIRCUIT BOARD IAW MM 20-00-01. OPS CHECKS WERE NORMAL.SDR GLBA20090524092Sensor · dirtyPILOTS REPORTED A STALL HEAT CAUTION ANNUNCIATOR WOULD NOT TURN OFF WITH THE SWITCH IN THE ON POSITION. MAINTENANCE CLEANED CONNECTIONS ON A1 & A2 STALL WARNING CURRENT SENSORS. FUNCTIONAL CHECKS WERE GOOD.SDR GLBA200905241Annunciator · inoperativeSTALL HEAT CAUTION ANNUNCIATOR WILL NOT TURN OFF WITH THE SWITCH IN THE ON POSITION.SDR GUUA92755052109AHinge Bracket · corrodedDURING SCHEDULED ROUTINE MAINT DISCOVERED RUDDER CENTER HINGE BRACKET HAS EXFOLIATION. REPLACED RUDDER CENTER HINGE BRACKET.SDR GUUA93732051809ALine · crackedPILOT REPORTED LT BRAKE PEDAL GOES TO THE FLOOR. REMOVED AND REPLACED CRACKED HYD BRAKE LINE.SDR GLBA20090522GPressure Switch · wornAFX ANNUNCIATORS AND REPEATER LIGHTS WOULD NOT ILLUMINATE WHEN POWER ADVANCED ABOVE 1000 FT LBS ON TAKEOFF ROLL. MAINT REMOVED AND REPLACED THE HIGH PRESSURE SWITCH CONNECTOR PLUG IAW GMM 9.3.0. MAINT ALSO REMOVED AND REPLACED THE NR1 AUTOFEATHER HIGH PRESSUSDR GLBA20090520FCircuit Board · failedPILOTS REPORTED THAT THE AFX ANNUNCIATORS AND REPEATER LIGHTS EXTINGUISHED AFTER V. THE AFX FAULT ANNUNCIATOR DID NOT ILLUMINATE. MAINT REMOVED AND REPLACED THE PRINTED CIRCUIT BOARD A123 IAW 1900D MM 61-20-00. MAINT ADDTIONALLY COMPLIED WITH FLEET CAMPAIGN DISDR GUUA94232051709ASwitch · out of adjustPILOT REPORTED LANDING GEAR WARNING HORN SOUNDS AT 3000 FT LBS TORQUE AT 91 PERCENT N1. ADJUSTED RT GEAR WARNING HORN SWITCH TEST FLIGHT SATISFACTORY.SDR GUUA93752051709ACable · brokenDURING SCHEDULED ROUTINE MX DISCOVERED FWD AIRSTAIR DOOR CAMS NOT MOVING. REPLACED FWD LOWER DOOR CABLE.SDR GUUA93953051709ASkin · corrodedDURING SCHEDULED ROUTINE INSP LT AND RT SIDE FUSELAGE BELLY REQUIRES SURFACE CORROSION CLEANING FROM FS 243.250 TO FS 327.630. REMOVED SURFACE CORROSION AND DISCOVERED SKIN EXFOLIATION LWR CTR AFT SPAR. REMOVED SECTION OF EXFOLIATED SKIN AND FABRICATED AND INSDR 19MA8866171Hinge Fitting · crackedWHILE PERFORMING AN I-CHECK THE ELEVATOR OTBD HINGE AREA WAS INSPECTED AND SUBSTANTIAL PLAY WAS NOTED IN AN UP AND DOWN DIRECTION. FURTHER INVESTIGATION REVEALED THE ELEVATOR HINGE CASTING WAS LOOSE IN ITS MOUNT AND A BORESCOPE INSP WAS PERFORMED TO THE OTBD HSDR GLBA20090512FHandle · misalignedFLT 5091 - ENROUTE, PILOTS REPORTED THAT THE GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE J-HOOK DID RELEASE. THEY TRIED A COUPLE TIME TO GET THE GEAR TO COME UP. MAINTENANCE RE-STOWED THE EMERGENCY HANDLE AND INSPECTED THE LT AND RIGHT SAFETY SWITCHES. GEAR SWINSDR GLBA200905121Line · overheatedPILOTS REPORTED THAT WHEN FULL POWERE WAS SET THE RT TORQUE WAS AT APPROX 3100 LBS BEFORE ITT LIMIT WAS EXCEEDED. TAKEOFF TORQUE SHOULD HAVE BEEN 3572 AT FLAPS 17 DEGREE AND BLEEDS CLOSED. ITT WAS EXCEEDED FOR APPROXIMATELY 1 SECOND. MAINTENANCE FOUND THE P3 LSDR GUUA95253051109ASkin · corrodedDURING SCHEDULED ROUTINE INSPECTION DISCOVERED CORROSION ON BELLY SKIN AT FUSELAGE STATION 340.75 STRINGER 15 RIGHT. REMOVED CORROSION FABRICATED AND INSTALLED EXTERNAL DOUBLER REPAIR.SDR GUUA52051109ACable · brokenFLIGHT: 9244 FLL/GGT - PILOT REPORTED DOOR CABLE BROKEN. REPLACED TOP AFT AIRSTAIR DOOR CABLE AND LOWER FORWARD DOOR CABLE OPERATIONAL CHECK OK.SDR GUUA95752051009ACable · brokenFLIGHT:9244 FLL/GGT - PILOT REPORTED DOOR CABLE BROKEN. REPLACED TOP AFT AIRSTAIR DOOR CABLE AND FORWARD AIRSTAIR DOOR CABLE. OPERATIONAL CHECK NORMAL.SDR GLBA200905111Switch · malfunctionedPILOTS REPORTED THAT THE AUTOFEATHER SYSTEM ENGAGED AND CYCLED IN FLIGHT ON FINAL WITH PROPS FULL FORWARD AS POWER WAS REDUCED TO JUST JUNDER 1000 LBS TORQUE ON NR 1 ENGINE. MAINTENANCE REMOVED AND REPLACED THE LOW PRESSURE SWITCH IAW BMM 61-21-01. OPERATIONALSDR GUUA92732050909AUplock Switch · malfunctionedFLIGHT: 5400 AFTER TAKEOFF, LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION, LIGHT EXTINGUISHED AFTER RUNNING QRH. REPLACED LT MAIN GEAR UPLOCK SWITCH. OPS CHECK OK.SDR GUUA93553050809ASkin · corrodedDURING SCHEDULED ROUTINE INSP FOUND SURFACE CORROSION UNDER ACFT BELLY FROM FS 408.25 TO FS 438.25. DURING FUTHER MX DISCOVERED BELLY SKIN CORROSION DAMAGE, REMOVED DAMAGED SKIN AND INSTALLED EXTERNAL DOUBLER REPAIR.SDR GUUA93753050809ASkin · crackedDURING SCHEDULED ROUTINE INSP, DISCOVERED LT FUSELAGE BELLY SKIN HAS .75 INCH CRACK AT FS 260.750. STOP DRILLED CRACK AND INSTALLED EXTERNAL REINFORCEMENT DOUBLER.SDR GLBA20090508CValve · wornFLIGHT 5145 - THE PILOTS REPORTED THAT DURING CRUISE THE VACUUM PRESSURE WAS READING AS LOW AS 3.5 AT FLIGHT LEVEL 220. MAINTENANCE REMOVED AND REPLACED THE VACUUM REGULATOR VALVE IAW B1900D MM 37-00-01. THE OPERATIONAL CHECK WAS GOOD.SDR GLBA20090508BWindow · cracked(SUP) - DIVERSION - AIRCRAFT N240GL - FLIGHT 10 - THE PILOTS REPORTED THAT ENROUTE FROM "LWT" - "DEN" THE CAPTAINS WINDSHIELD SHATTERED/BROKEN. THE AIRCRAFT DIVERTED TO "CYS" FOR REPAIRS. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDSHIELD IAW BMM 52-10SDR GLBA20090507AUplock Switch · malfunctionedTHE PILOTS REPORTED THAT UPON GEAR RETRACTION OUT OF "LWT" THE GEAR INTRANSIT LIGHT DID NOT EXTINGUISH. VERIFIED THAT ALL GREEN LIGHTS WERE OUT AS WELL. MAINTENANCE REMOVED AND REPLACED THE NOSE GEAR UPLOCK SWITCH PERFORMED LANDING GEAR. RETRACTION TEST OPS CSDR GLBA20090506AUplock Switch · dirtyPILOTS REPORTED THAT AFTER TAKEOFF THEY RETRACTED THE GEAR AND THE GEAR HANDLE REMAINED ILLUMINATED. MAINTENANCE TROUBLESHOT THE SYSTEM AND INSPECTED AND CLEANED THE NOSE GEAR UP LOCK SWITCH AND OPS CK WAS GOOD IAW MM 32-60-00. PERFORMED EXTENSION/RETRACTIONSDR GUUA93632050309ASwitch · out of adjustFLIGHT:5202 FLL/FLL - DURING TEST FLIGHT LANDING GEAR WARNING HORN ACTIVATE AT 81 PERCENT N1. ADJUSTED LANDING GEAR WARNING HORN SWITCHES TEST FLIGHT SATISFACTORY.SDR GUUA93628050309APump · leakingFLIGHT: 5202 FLL/FLL - DURING TEST FLIGHT, CABIN SMELLS LIKE FUEL. REPLACED LEFT ENGINE DRIVEN FUEL PUMP.SDR GUUA95652050309ALatch · lack of lubeDURING SCHEDULED ROUTINE INSP, DISCOVERED EMERGENCY EXIT DOOR 6A LATCHING MECHANISM IS NOT OPENING PROPERLY FROM INSIDE. LUBRICATED LATCHING MECHANISM. OPS CHECK GOOD.SDR GLBA200905031Bulb · burned outDURING ROUTINE MAINTENANCE AN INSTRUMENT EMERGENCY LIGHT WAS FOUND BURNED OUT. MAINTANENANCE REMOVED AND REPLACED THE BULB. OPERATIONAL CHECK WAS GOOD.SDR GLBA20090502ACircuit Board · looseRIGHT ENVIRO FAIL ANNUNCIATOR ILLUMINATED DURING TAKEOFF WITH TAKEOFF POWER AND BLEED AIR VALVES CLOSED. MAINTENANCE RE-SEATED THE PRINTED CIRCUIT BOARD AND OPERATIONAL CHECKS WERE GOOD.SDR GLBA200930041Indicator · erraticIN CRUISE AT 2300 NR 1 TORQUE GAUGE WAS FLUCTUATING 200-300FT/LBS. COULD HEAR THE CHANGE IN TORQUE. OCCURRED WITH PROP SYNC ON AND OFF. WHEN TORQUE BELOW 2500FT/LBS IN DESCENT ALL PWR CHANGE DECREASES AN ADDITIONAL 300FT/LBS WITHOUT BEING COMMANDED WITH POWER SDR GLBA20090430CSwitch · out of adjustCABIN DOOR ANNC CAME ON IN FLIGHT. DIVERTED TO NEAREST SUITABLE AIRPORT. MAINTENANCE TROUBLESHOT THE SYSTEM AND ADJUSTED THE FORWARD AND AFT LATCH SWITCHES.SDR GLBA20090430BRadar · malfunctionedWX RADAR WILL NOT PICK UP PRECIPITATION. RETURN TO DEPARTURE. PILOTS REPORTED THAT THE WEATHER RADAR TESTED FINE, PAINTED THE GROUND FINE, HOWEVER, IT DOES NOT REGISTER EVEN EXTREME WEATHER PRECIPTATION AS REORTED BY ATC AT 12 O'CLOCK. MAINTENANCE REMOVED ANDSDR GLBA20090504GFcu · malfunctionedPILOTS REPORTED THAT THE RT ENGINE ATTEMPTED TO AUTOFEATHER ON ABOUT A 3 NAUTICAL MILE FINAL. THE AFX DISABLE ANNUNCIATOR ILLUMINATED WHEN THIS OCCURRED AND THE AUTOFEATHER SWITCH WAS IN THE ARMED POSITION. RT SIDE FLUCTUATED BETWEEN 400 AND 1700 LBS. LT TORQUSDR GUUA95032042909ASwitch · failedDURING APPROACH, WHEN ATTEMPTING TO SILENCE THE LANDING GEAR WARNING HORN THE PIN CONNECTED TO THE SYS FELL OUT RENDERING IT INOPERATIVE. REPLACED LANDING GEAR WARNING HORN SWITCH. OPS CHECK OK.SDR GLBA20090429AEngine · malfunctionedRT ENGINE ATTEMPTED TO AUTOFEATHER ON ABOUT A CLOSE FINAL THE AFX DISABLE ANNUNCIATOR ILLUMINATED WHEN THIS OCCURED AND THE AUTOFEATHERS SWITCH WAS IN THE ARMED POSITION. TORQUE GAUGE ON RT SIDE FLUCTUATED BETWEEM 400 AND 1700 LBS. LT TORQUE WAS STABLE AT APPRSDR GLBA200904282Annunciator · false activationCABIN DOOR ANNUNCIATOR ILLUMINATED DURING TAXI OUT AND ONTO RUNWAY. TAKEOFF ABORTED. MAINTENANCE PERFORMED GROUND OPERATIONAL CHECK OF CABIN DOOR ANNUNCITOR. NO DEFECTS NOTED THIS CLEARS DML 34909 ALL PLACARD REMOVED. REF MM 52-70-00.SDR GLBA20090504FStructure · corrodedMAJOR REPAIR - AIRSTAIR DOOR WAS FOUND CORRODED ON LOWER END CLOSURE AREA. MAINTENANCE REMOVED A SECTION OF THE LOWER INNER DOOR PAN, CLEANED CORROSIONFROM INNER MATERIAL, INTALLED NEW LOWERE DOOR PAN AND INSTALLED THE HINGE ASSEMBLY IAW EO 09-1900-52-001.SDR GLBA200904281Relay · odorBURNING PLASTIC ODOR WHEN MODE CONTROLLER & BLOWERS ON. MAINTENANCE REMOVED FLOORBOARDS OVER THE FORWARD AND AFT VENT BLOWERES. FOUND BLOWERS TO OPERATE. RE-INSTALLED FLOORBOARDS. REMOVED FLOORBOARD COVERING FLAP MOTOR, GEARBOX, AND FLAP RELAY. NOTICED AN SDR GUUA95452042709ADoor · stuckDURING SCHEDULED ROUTINE MX DISCOVERED RT AFT EMERGENCY EXIT HARD TO OPEN. LUBRICATED RT AFT EMERGENCY EXIT OUTER AND INNER HANDLE, OPERATIONAL CHECK OK.SDR GUUA95052042609ADoor · stuckDURING SCHEDULED ROUTINE MX DISCOVERED LT EMERGENCY EXIT DIFFICULT TO OPEN. LUDRICATED LT EMERGENCY EXIT HANDLE. OPS CHECK GOOD.SDR GLBA20090425ACabin Pressure · malfunctionedPILOTS REPORTED THAT UPON CLIMBING THE AIRCRAFT FAILED TO PRESSURIZE AND THEY THEN RETURNED TO FMN. MAINTENANCE OPERATIONALLY CHECKED THE SYSTEM ON THE GROUND WHICH WAS GOOD PER MM 21-30-00. OPERATIONAL CHECK FLIGHT WAS PERFORMED AND WAS SATISFACTORY.SDR CA090427003Starter Gen · inoperative(CAN) RT ENGINE WOULD NOT CRANK, STARTER WAS ENGAGING BUT DID NOT HAVE ENOUGH POWER TO TURN THE ENGINE WITH SMOKE COMING FROM THE STARTER.SDR GLBA200924042Circuit Board · malfunctionedPILOTS REPORTED THAT UPON TAKEOFF POWER UP ABOVE 2500 LBS. FOR TAKEOFF THE AFX DISABLE LIGHT ILLUMINATED AND THE NR 2 ENGINE STARTED TO TRANSITION IN AND OUT OF FEATHER. MAINTENANCE REMOVED AND REPLACED THE A123 PRINTED CIRCUIT BOARD PER GMM 9.2.0 & OPERATIONA
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