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 GUUA93652082110ADoor · bindingDURING SCHEDULED ROUTINE INSP, DISCOVERED RT EMERGENCY FWD EXIT DOOR IS HARD TO OPEN. ADJUSTED RT FWD EMERGENCY EXIT DOOR UPHOLSTRY.SDR GUUA95432082010ASwitch · malfunctionedFLIGHT 9202, ON LANDING GEAR RETRACTION RED UNSAFE LIGHT REMAINS ILLUMINATED AND GEAR HORN IS HEARD.RETURNED TO GHB LANDED WITHOUT INCIDENT. REPLACED RT POWER LEVER GEAR HORN SWITCH OPS CHECK NORMAL. TEST FLIGHT SATISFACTORY.SDR GLBA201008232Holder · failedRT SIDE INST EMERGENCY LIGHTS DO NOT TURN ON WITH SWITCH. MX INSPECTED AND FOUND CORROSION ON THE FUSE HOLDER, REPLACED HOT BATTERY BUSS FUSE HOLDER PN 4532 IAW BMM 24-31-00, OPS CHECKS GOOD.SDR GLBA201008201Holder · corrodedPILOT REPORTED THAT THE RT SIDE INSTRUMENT EMERGENCY LIGHTS DO NOT TURN ON WITH THE SWITCH. MX INSPECTED AND FOUND CORROSION ON THE FUSE HOLDER, REPLACED HOT BATTERY BUSS FUSE HOLDER PN 4532 IAW BMM 24-31-00, OPS CHECKS GOOD.SDR GLBA20100819FFastener · looseSIG EVENT - PILOT REPORTED THAT AN OVERWHELMING ODOR OF FUEL ENTER THE CABIN AND COCKPIT. MAINTENANCE FOUND LOOSE FASTENERS JUST OUTBOARD OF RT NACELLE AT FORWARD SPAR, REPLACED FASTENERS AND SEALED AREA, REFUELED, NO LEAKS OR ODOR PRESENT IAW SRM 51-10-00, CSDR GLBA20100818GSkin · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION FOUND EMERGENCY EXIT DOOR 4C INNER LOWER AFT CORNER SKIN CRACKED , 1.7" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 10-1900-52-004. MATERIALS UTILISDR GUUA94528081810ACoupling · leakingDURING SCHEDULED ROUTINE MX DISCOVERED FUEL LEAKING FROM BOTTOM OF RT NACELLE. REPLACED WIRE HARNESS TUBING COUPLING ASSY AT FUEL ACCESS PANELS 642 BB AND 642CB APPLIED SEALANT AT COUPLING AND REPLACED PRC AROUND CONDUIT NEXT TO AUX PUMP LEAK CHECK GOOD.SDR ERAA201000004ALine · leakingFUEL ON RIGHT COWLING. FOUND PIN HOLE LEAK IN FUEL LINE FROM FCU TO FUEL FLOW TRANSMITTER. REMOVED AND REPLACED FUEL LINE WITH SERVICEABLE LINE IAW B1900D MM 73-10-00. LEAK CHECK GOOD.SDR GLBA20100818BFuel Sys · leakingOVERWHELMING ODORS OF JET FUEL PRESENT IN CABIN COCKPIT EXTREMELY BAD TO A POINT OF BEING NAUSEATING AND AFFECTING SAFETY SLOW DRIP UNDER RT NACELLE DIFFERENT AREA THAN REPAIR.SDR 19MA201008196584Door · crackedWHILE PERFORMING A DETAIL INSP, DISCOVERED ENGINE INTAKE DEICE DOOR GUIDE VANE PN 118-910038-29, WOULD NOT ALLOW THE DEICE DOOR TO WORK FREELY AND CATCHES ON THE L/E OF THE VANE AND ALSO HAD A POPPED RIVET ALONG THE AFT SIDE OF THE VANE. (THIS WAS NOT VISIBLE SDR GUUA94652081810ADoor · lack of lubeDURING SCHEDULED ROUTINE INSP DISCOVERED LT EMERGENCY EXIT HARD TO OPEN. LUBRICATED LT EMERGENCY EXIT DOOR OPS CHECKS NORMAL.SDR GLBA20100818FFrame · crackedDURING A SCHEDULED ROUNTINE INSP, A CRACK IN THE FRAME AT FS 456 WAS FOUND AT STRINGER CUTOUT 10R, .25" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 10-1900-53-050. MATERIALS UTILIZED ARE INCLUDED IN TSDR CA100817019Pressure Switch · leakingOIL LEAKING FROM VENT HOLE IN BODY OF SWITCH.SDR GUUA93921081510ATransfer Tube · leakingDURING CLIMBOUT, PASSENGERS REPORTED SMOKE AFTER OPENING BLEED VALVES. SMOKE DISSIPATED WITH VALVES SWITCH TO ENVIRO OFF. FOUND FUEL NOZZLE TRANSFER TUBE LEAKING AT (3) O`CLOCK POSITION, REPLACED TRANSFER TUBE, LEAK CHECK, OK, NO SMOKE NOTED.SDR GLBA20100816GClamp · looseSIG EVENT - PILOT REPORTED THAT THE ACFT WOULD NOT PRESSURIZE IN FLIGHT. MX INSPECTED THE ACFT AND RESEATED A LOOSE CLAMP ON THE ACM TO THE HEAT EXCHANGER, OPS CHECKS OK, REF 71-51-01.SDR GUUA93727081210ATorque Tube · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED LT ELEVATOR TORQUE TUBE HAS CORROSION. REPLACED LT ELEVATOR TORQUE TUBE.SDR GLBA20100812FSkin · debondedDURING A SCHEDULED ROUNTINE INSP, FOUND THE AIRSTAIR DOOR SKIN DEBONDING ON THE LOWER AFT, APPROX 19" IN LENGTH. MX REPLACED THE AIRSTAIR DOOR BONDED SKIN IAW BMM 52-10-03 AND COMPLIED WITH SB 52-3094, OPS CHECKS GOOD.SDR CA100817015Engine · malfunctionedABORTED TAKEOFF DURING TAKEOFF ROLL, A LOUD NOISE WAS HEARD FOLLOWED BY A HIGH PITCHED NOISE. THE ACFT HAD A SUDDEN YAW TO THE LT. TAKEOFF WAS ABORTED. ACFT WAS TOWED FOR EXAMINATION.SDR V0DR967YASpacer · mismanufacturedA SPACER (PN: 5012404-1) WAS INSTALLED NEW FROM STOCK INTO A BRAKE ASSY (PN: 5006749-5R). DURING THE TESTING PROCESS, THE MECHANIC WAS UNABLE TO ACHIEVE THE DESIRABLE SPACING BETWEEN BRAKE PARTS. THE SPACER (PN 5012404-1) WAS REMOVED AND INSPECTED IN REFERENCESDR V0DR967YBJam-Nut · defective(V0DR) DURING ASSY OF A PROPELLER ASSY, THE JAM-NUTS (PN B-3368) WERE INSTALLED AND THE BETA RING RUN-OUT TOLERANCE COULD NOT BE MAINTAINED. FURTHER TROUBLESHOOTING IDENTIFIED THE JAM-NUTS (PN B-3368) WERE MFG WITH THE THREADS NOT TRUE. CAUSING THE RUN-OUT TSDR GUUA93352081110BDoor · bindingDURING SCHEDULED ROUTINE MX, DISCOVERED LT EMERGENCY EXIT HARD TO CLOSE. MADE ADJUSTMENTS TO UPPER PIN GUIDES, OPS CHECK GOOD.SDR GUUA93352081110ADoor · bindingDURING SCHEDULED ROUTINE MX DISCOVERED RT AFT EMERGENCY EXIT HARD TO OPEN. LUBRICATED RT AFT EMERGENCY EXIT OPS CHECK GOOD.SDR V0DR967Y001Jam-Nut · defectiveDURING ASSY OF A PROPELLER, THE JAM-NUTS, PN B-3368 WERE INSTALLED AND THE BETA RING RUN-OUT TOLERANCE COULD NOT BE MAINTAINED. FURTHER TROUBLESHOOTING IDENTIFIED THAT THE NUT PN B-3368 WAS MFG WITH THE THREADS NOT TRUE. CAUSING THE RUN-OUT TO BECOME EXCESSISDR GLBA20100810FSkin · dentedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, A DENT ON RT SIDE OF FUSELAGE AT FS 531 BETWEEN STRINGER 11R AND 10R WAS FOUND. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-049. MATERIALS UTILIZED ARE INSDR GUUA95552080510ADoor · lack of lubeDURING SCHEDULED ROUTINE INSP, DISCOVERED LT EMERGENCY EXIT DOOR HARD TO OPEN. LUBRICATED LT EMERGENCY EXIT DOOR.SDR GUUA95152080410ACable · kinkedDURING SCHEDULED STRUCTURAL INSP DISCOVERED TOP FWD AND BOTTOM FWD AIRSTAIR DOOR CABLES KINKED. REPLACED TOP FWD AND BOTTOM FWD AIRSTAIR DOOR CABLES. NOTE: ACFT DOWN FOR STRUCTURAL INSP.SDR GLBA20100805FAEngine · overtorquedPILOT REPORTED THAT UPON APPROACH, RT POWER LEVER STUCK WITH AN OVERTORQUE INDICATION, PERFORMED PRECAUTIONARY RT ENGINE SHUTDOWN. RT PROPELLER CONTINUED TO WINDMILL AFTER ENGINE SHUTDOWN. MX PERFORMED AN INSPECTION ON RT ENGINE POWER CONTROL LINKAGE, CABLE, CSDR GLBA20100802JBulkhead · crackedDURING A SCHEDULED ROUTINE INSPECTION A CRACK WAS FOUND AT THE AFT CARGO BAY FLOORBOARD FORWARD SUPPORT BULKHEAD AT F.S. 531.0 LH SIDE WHERE IT ATTACHES TO THE FRAME, 13/16" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPESDR GLBA20100802KBulkhead · buckledMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION A BULKHEAD AT FS 531 AFT CARGO FLOORBOARD FORWARD SUPPORT BUCKLED ABOUT 11/32" AT TOP, TOTAL DAMAGE AREA ABOUT 26" IN LENGTH, AND A .5" CRACK IN THE RADIUS 12" FROM RT SIDE. MAINTENANCE REPAIRED THE AFFECTESDR GUUA93352080210ADoor Latch · inoperativeDURING SCHEDULED ROUTINE INSP DISCOVERED RT AFT EMERGENCY EXIT HARD TO OPEN. LUBRICATED RT AFT EMERGENCY EXIT DOOR LATCH MECHANISM. OPS CHECK GOOD.SDR GLBA201008101ALanding Gear · malfunctionedDURING CHECK FLIGHT GEAR WAS SELECTED DOWN. AFTER 3 SECONDS THE LANDING GEAR RELAY CIRCUIT BREAKER POPPED. RED INTRANSIT LIGHT ON 2ND RT MAIN INDICATED GREEN, VERIFIED GEAR WERE ALL DOWN AND LOCKED VIA THE THROTTLE SWITCH AND SELECTED FLAPS 35. THEN PERFORMSDR GLBA20100805FUnknown · unknownSIG EVENT - PILOT REPORTED THAT ON FINAL WITH TORQUE SET AT 300, INCREASED TORQUE TO 1000, LEFT ENGINE BEGAN TO CYCLE IN AND OUT OF FEATHER. MAINTENANCE PERFORMED TESTS OF THE AUTOFEATHER SYSTEM AT ALL TORQUE SETTINGS, IAW MM 61-21-00, AUTOFEATHER SYSTEM OPERASDR GUUA95232073110ASwitch · failedPILOT REPORTED LANDING GEAR WARNING HORN WILL NOT SILENCE. REPLACED LANDING GEAR HORN SILENCE SWITCH (PN C2006) AND RELAY PCB A113 OPS CHECK NORMAL.SDR GLBA20100730FSkin · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION A CRACK IN THE SKIN WAS FOUND ON THE EMERGENCY EXIT DOOR 6A, LOWER FORWARD CORNER, 2" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 10-1900-52-003. MSDR GUUA93377072810ATransducer · fluctuatesDURING TEST FLIGHT, LT TORQUE GAUGE WENT TO 5,000 THEN STARTED TO FLUCTUATE TO ZERO. REPLACED LT TORQUE TRANSDUCER, OPERATIONAL CHECK OK. TEST FLIGHT SATISFACTORY.SDR GUUA93327072810AAoa · malfunctionedUPON TAKEOFF AFTER LANDING GEAR UP STALL WARNING CAME ON AND SOUNDED UP TO 500 FEET ON AND OFF. SECURED AND CLEANED STALL WARNING VANE. TEST FLIGHT SATISFACTORY.SDR GLBA20100729FFan · failedSIG EVENT - PILOT REPORTED THAT DURING FLIGHT BLOWERS AIRFLOW BECAME VERY WEAK AND A SLIGHT BURNING SMELL WAS THEN NOTICED. MX REPORTED THAT THEY REPLACED THE VENT BLOWER IAW AMM 21-20-01, PN 114-380078-11 SN OFF 558A, SN ON 57A.SDR GLBA20100728FFrame · crackedDURING A SCHEDULED ROUNTINE INSP A CRACK WAS FOUND IN THE FRAME ANGLE AT FS 303, .5" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 10-1900-53-045. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDESDR GLBA20100729GFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, A2 CRACKS WAS FOUND IN THE FRAME AT FS 456 AND STRINGER 10R CUTOUT, .45" AND .5" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-046. MATERIALS UTISDR GUUA95153072610BAngle · crackedDURING SCHEDULED ROUTINE INSP, DISCOVERED LT WING TO FUSELAGE CLOSING ANGLE CRACKED 1.65 INCHES. STOP DRILLED END OF CRACK AND INSTALLED REPAIR ANGLE. NOTE: ATA CODE UPDATED TO 5300.SDR GUUA95157072610BAngle · crackedDURING SCHEDULED ROUTINE INSP, DISCOVERED LT WING TO FUSELAGE CLOSING ANGLE CRACKED 1.65 INCHES. STOP DRILLED END OF CRACK AND INSTALLED REPAIR ANGLE.SDR GUUA95153072610AAngle · crackedDURING SCHEDULED ROUTINE INSP DISCOVERED AIRSTAIR DOOR ANGLE CRACKED AT TOP AND BOTTOM, SNUBBER BRACKET ATTACH POINTS APPROX FS 150 STRINGERS 9AL AND 4L. REMOVED DAMAGED SECTION AND INSTALLED REPAIR ANGLE.SDR GLBA201007261Gas Generator · seizedPILOT REPORTED THAT RIGHT ENGINE SECURED IN FLIGHT, ITT WAS STEADILY RISING ABOVE LIMITS TO AROUND 940C AND TORQUE WAS STEADILY DECREASING UNTIL ENGINE WAS SECURED. AFTER LANDING OIL FOUND LEAKING FROM ENGINE AND PROP WAS SEIZED. MAINTENANCE PULLED THE COCKPITSDR GUUA95221072410AHydraulic System · leakingDURING FLIGHT, RTV SEALANT SMELL COMING FROM CAPTAINS OVERHEAD VENT, VARYING INTENSITY THROUGHTOUT THE FLIGHT. FOUND HYD OVERFILL LINE NOT THROUGH WING PANEL ALOWING HYD FLUID BUILD UP IN ACM AREA, CLEANED ACM AREA AND REINSTALLED HYD OVERFILL LINE PROPERLY. SDR GUUA93332072310AProximity Switch · out of adjustAFTER TAKEOFF LANDING GEAR UNSAFE LIGHTS IN THE GEAR HANDLE REMAIN ILLUMINATED AFTER GEAR RETRACTION. ADJUSTED LT MAIN GEAR UP POSITION SWITCH. OPS CHECK NORMAL TEST FLIGHT SATISFACTORY.SDR GLBA201007201Circuit Board · burnedPILOT REPORTED THAT ON APPROACH TO PHX FO NOTICED A SYNTHETIC BURNING SMELL BRIEFLY, THEN GOT A BATT TIE ANNUNCIATOR LIGHT. MAINTENANCE INSPECTED THE ELECTRICAL SYSTEM AND FOUND CIRCUIT BOARD A130 HAD A BURNT DIODE, REPLACED BOARD IAW AIM 10-24-01, RAN AIRCRAFSDR GUUA94155071910CHinge Bracket · corrodedDURING SCHEDULED ROUTINE INSPECTION DISCOVERED RIGHT ELEVATOR INBOARD HINGE BRACKET HAS CORROSION. REPLACED RIGHT ELEVATOR INBOARD HINGE BRACKET.SDR GUUA94155071910BHinge Bracket · corrodedDURING SCHEDULED ROUTINE INSPECTION DISCOVERED RIGHT ELEVATOR CENTER HINGE BRACKET EXFOLIATED. REPLACED RIGHT ELEVATOR CENTER HINGE BRACKET.SDR GUUA94155071910AHinge Bracket · corrodedDURING SCHEDULED ROUTINE INSPECTION DISCOVERED RIGHT ELEVATOR CENTER HINGE BRACKET EXFOLIATED. REPLACED RIGHT ELEVATOR CENTER HINGE BRACKET.SDR GUUA95221071910AUnknown · odorFLIGHT 9150 MHH/FLL WHEN AIRCRAFT DEPARTS INTO THE AIR AIRCRAFT WILL PRODUCE A BURNT SMELL COMING FROM EYEBALL AND FLOOR VENTS. OPENED FLOORBOARDS AND INSPECTED FOR CAUSE OF BURNT SMELL, NO CAUSE OF BURNT SMELL FOUND TURNED ON ALL SYSTEMS FOR 30 MINUTES AND N
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