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 = '1900C' 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 = '1900C' 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 FFSA200900003Terminal · meltedSHORTLY AFTER TAKE OFF, SMOKE WAS OBSERVED COMING OUT OF FIRST OFFICER’S GLARE SHIELD. AIRCRAFT RETURNED FOR LANDING. FOUND TERMINAL BLOCK AND RING TERMINAL INSULATION FOR CO-PILOT WINDSHIELD LOW HEAT POWER LEAD MELTED AND CRACKED. THE TERMINAL APPEARED TO BESDR CA090519011Structure · corroded(CAN) DURING A YEARLY INTERNAL WING CORROSION INSP AS REQUIRED BY CHAPTER 5 REQUIREMENTS, EXTENSIVE SPAR/STRINGER/SKIN CORROSION WAS DISCOVERED IN THE INBD SECTION OF THE MAIN TANKS AND THE COLLECTOR TANKS. X-RAY INSP REVEALED UNDISCOVERED SPOTS OF CORROSION BSDR CA090312003Selector · unserviceable(CAN) THE LANDING GEAR RELAY CIRCUIT BREAKER "POPPED" IN FLIGHT, GEAR MANUALLY EXTENDED. GEAR HANDLE ASSY REPLACED WITH SERVICEABLE UNIT. NUMEROUS GEAR SWINGS CARRIED OUT. NO FAULTS FOUND. THE GEAR HANDLE SWITCH WAS TESTED BY MX. THE SWITCH WHEN SELECTED DOWSDR FFSA200900002Transistor · meltedENVIRONMENTAL TEMPERATURE CONTROL CIRCUIT BREAKER POPPED IN FLIGHT, RESET CIRCUIT BREAKER AND EVERYTHING SEEMED OK UNTIL IN DESCENT WHEN ELECTRICAL FUMES WERE SMELLED. PULLED CIRCUIT BREAKER AND LANDED NORMALLY. UPON INVESTIGATION FOUND THE COOL COMMAND TRANSDR CA090302007Stringer · corroded(CAN) SEVERE CORROSION FOUND IN LT WING STRINGER J STN 124.588. MFG RDO CONTACTED REGARDING REPAIR PROCEDURE.SDR FFSA200900001Door Frame · crackedDURING THE THIRD 200 HOUR DETAILED INSP, A CRACK WAS DISCOVERED IN THE AIRSTAIR DOOR FRAME RUNNING HORIZONTALLY ALONG THE RIVET HOLES OF THE UPPER LINE OF RIVETS THAT HOLD THE AIRSTAIR DOOR HINGE HALF TO THE FUSELAGE. THE DOOR FRAME, P/N 114-420034-1, WAS CRASDR CA090219005Spar Cap · corroded(CAN) SEVERE CORROSION FOUND ON RT HORIZONTAL STABALIZER LOWER SPAR CAP AT STN. 90.00. MFG RDO OFFICE CONTACTED FOR REPAIR.SDR CA090220004Turbine Blades · erodedTHE TREND MONITORING PROGRAM STARTED TO SHOW SIGNS OF HOT SECTION DISTRESS ON THE GRAPHS. BOROSCOPE INSPECTION REVEALED SOME EROSION AND IMPACT DAMAGE ON THE CT BLADES. AN HOT SECTION INSPECTION WAS CARRIED OUT AND THE COMPONENTS REPLACED. WHEN THE CT BLADESDR YADA122908Pump · damagedON AN OPS CHECK FLIGHT, PILOT REPORTED LOW PRESSURE FUEL LIGHT ON THE NR 1 ENG, LIGHT WENT OUT WITH AUX PUMP ON. REPLACED PUMP. TEARDOWN OF REMOVED PUMP REVEALED THAT THE PRESSURE CONTROL DIAPHRAGM HAD FAILED POSSIBLY DUE TO AN IMPROPERLY MFG PN RA5361 SPRINSDR CA081210011Engine · shutdown(CAN) NR 1 ENGINE SHUTDOWN CARRIED OUT AFTER TAKEOFF. HERE IS THE DEFECT ENTERED BY THE FLIGHT CREW "LT PROP RPM ONLY GOES TO 1500 RPM ON TAKEOFF AS POWER REDUCED RPM DROPS". THE INCIDENT IS UNDER INVESTIGATION.SDR CA081215006Line · corroded(CAN) WHILE PERFORMING A WING SPAR INSPECTION, THE TECHNICIAN NOTICED A POOL OF HYDRAULIC OIL UNDER CENTER FLOORBOARDS. FURTHER INVESTIGATION REVEALED THAT THE LT BRAKE LINE UNDER THE MID CABIN FLOOR WAS CHAFED (FRETTING CORROSION) THROUGH IN SEVERAL SPOTS WHSDR TIMA20080008Relay · burnedTHE LANDING GEAR MOTOR DID NOT RUN WHEN THE PILOT SELECTED 'GEAR UP'. PILOT RETURNED TO AIRPORT AND LANDED WITHOUT INCIDENT. INVESTIGATION REVEALED THAT THE 60 AMP CIRCUIT BREAKER WAS OPEN AND THE LANDING GEAR MOTOR RELAY HAD BURNED CONTACTS. CLOSING THE CBSDR YADA120108Windshield · crackedLT WINDSHIELD BROKE IN CRUISE - RED GLOW FROM HEATER ELEMENTS UNTIL WINDSHIELD HEAT TURNED OFF. UNEVENTFUL LANDING MADE AT ORIGINAL DESTINATION. MX REPLACED THE LT WINDSHIELD DUE TO OUTER PANE FAILURE.SDR YADA112808Boot · shortedOBSERVED SPARKS FROM RT PROP INFLIGHT, SPARKS STOPPED WHEN PROP DEICE WAS TURNED OFF. A/C LANDED UNEVENTFULLY. MAINT REPLACED PROP DUE TO SHORTED DEICE BOOT.SDR YADA111708Skin · corrodedDURING INSP, THE MECHANIC NOTICED THE BELLY BEACON FRONT FASTENER WAS LOOSE. UPON INSP, THE MECHANIC DETERMINED THAT THERE WAS CORROSION UNDER THE BEACON MOUNT. THE BELLY SKIN REQUIRED A PATCH REPAIR TO REMOVE THE DAMAGED AREA.SDR CA081112009Engine · failed(CAN) DURING CRUISE AT FL180, THE CREW FELT A STRONG JOLT AND VIBRATIONS THROUGH THE AIRFRAME. A QUICK REVIEW OF THE GAGES SHOWED A POWER LOSS ON NR 2 ENG. THE ENG WAS SECURED AND THE CREW PERFORMED A SINGLE ENGINE LANDING. GROUND INSP FOUND NOTHING OF SIGNIFSDR TIMA20080007Limit Switch · brokenTHE LANDING GEAR DID NOT EXTEND WHEN SELECTED. THE PILOT MANUALLY PUMPED THE GEAR DOWN AND LANDED. INVESTIGATION REVEALED THAT THE LT UP-LIMIT ELECTRICAL SWITCH HAD PHYSICALLY BROKEN, OPENING THE CIRCUIT TO THE LANDING GEAR CONTROL.SDR FFSA200800006Brake Sys · malfunctionedPILOT’S RT BRAKE PEDAL WENT TO THE FLOOR WITH LITTLE OR NO BRAKING ACTION UPON LANDING. CO-PILOT’S BRAKE OPERATION WAS NORMAL. PRESSURE TESTED SYSTEM NO LEAKS NOTED. SERVICED HYDRAULIC RESERVOIR AND BLED BRAKE SYSTEM. BRAKE SYSTEM OPS CHECK SATISFACTORY.SDR YADA101408Shaft · brokenPILOT COULD NOT OPEN THE FORWARD PASSENGER/CREW DOOR FROM THE INSIDE, HANDLE WAS BROKEN (DOOR SEEMED FROZEN).SDR CA081017001Seal · failed(CAN) PILOTS SHUT DOWN NR 1 ENGINE, DUE TO OIL PRESSURE FLUCTUATION AND OIL PRESS. ANNUNCIATOR ILLUMINATION. ACFT RETURNED TO YXS MX BASE. OIL LOSS WAS FOUND TO BE COMING FROM THE HP PUMP DRAIN. OIL SEAL REPLACED, OIL CONSUMPTION ELIMINATED. EXPLORATORY WORK SDR YADA100708Line · rupturedPILOT REPORTED LEFT BRAKE "FLAT". REPLACED SEEPING FLEXIBLE BRAKE LINE - DATE CODE 2Q06.SDR CA081016012Compressor · seized(CAN) ACFT WAS EN ROUTE WHEN THE LT ENGINE LOST POWER. THE CREW COMPLETED EMERGENCY PROCEDURES, SECURED THE ENGINE AND FEATHERED THE PROPELLER. THEY DECLARED AN EMERGENCY AND CONTINUED TO DESTINATION, WHERE THE ACFT PERFORMED A SINGLE ENGINE LANDING. POST FSDR CA080930009Line · ruptured(CAN) AFTER LANDING A HYDR LEAK WAS DISCOVERED BY THE MX CREW. IT TURNED OUT TO BE THE RT MLG "REGULAR EXTEND" HYDR LINE. THE LINE HAD RUPTURED ABOUT 1 INCH FROM THE END FITTING RESULTING IN A SUBSTANTIAL FLUID LOSS. THE LINE WAS REPLACED WITH NO FURTHER ISSDR YAD2008F00003Brake Sys · weakPILOT REPORTED LT BRAKE FLAT ON TAXI AND LANDING. MX BLEED BRAKES.SDR YAD2008F00002Relay · contaminatedPILOT REPORTED IT TOOK 3 ATTEMPTS TO GET THE LANDING GEAR MOTOR TO OPERATE. THEN IT WORKED FINE. MX VERIFIED THAT FREEZING THE HYDRAULIC POWER PACK RELAY WOULD CAUSE THIS PROBLEM. REPLACED THE HYDRAULIC POWER PACK RELAY.SDR CA080912005Wire · burned(CAN) LT ENGINE FAILED TO ROTATE ON START UP. MAINT DISCOVERED LT STARTER GEN WIRE FEED THRU ASSY (CONSISTS OF 3 PARALLEL HEAVY GUAGE WIRES) TERMINAL ENDS BURNED OFF AT START CONTROL PANEL TERMINAL. NEW WIRE FEED THRU ASSY ON ORDER. START CONTROL PANEL ON ORDESDR FFSA200800005Windshield · crackedATA 56-10-00 PILOT’S WINDSHIELD OUTER PANE CRACKED ENROUTE TO BRW. ACFT MADE NORMAL LANDING IN BRW AND RETURNED TO FAI, PART 91, IAW POH/AFM LIMITATIONS SECTION GUIDANCE, PAGE 2-16.SDR YAD2008F00001Squat Switch · intermittentDURING A PILOT TRAINING FLT MLG WAS EXTENDED USING ALTERNATE EXTENSION PUMP IAW QRH AND POH. AFTER EXERCISE, PILOT RESET MLG CONTROL CIRCUIT BREAKER & SELECTED GEAR UP. PILOT REPORTED THAT ALTHOUGH THEY COULD HEAR MLG MOTOR/PUMP RUNNING, MLG DID NOT RETRACT,SDR CA080902004Barrel · cracked(CAN) DURING SCHEDULED INSP THE LT MLG ACTUATOR (FRISBY) WAS SEEN TO BE LEAKING. THE ACTUATOR WAS REPLACED ON THE ACFT. WHILE IN REPAIR THE BARREL OF THE ATUATOR FAILED NDT FOR A CRACK IN THE THREADED AREA. THIS AREA IS NOT INCLUDED IN SB 32-3870 WHICH CALLS FSDR CA080826001Light · inoperative(CAN) LANDING GEAR MOTOR CONTROL CIRCUIT BREAKER FOUND POPPED WHEN THE GEAR WAS SELECTED DOWN FOR LANDING. GEAR WAS LOWERED BY EMERGENCY EXTENSION INDICATING (3) GREEN BUT THE IN TRANSIT LIGHT WAS STILL ON. ACFT EXPERIENCED A NOSE GEAR COLLAPSE ON LANDING. UPSDR CA080806003Gearbox · disconnected(CAN) DURING FINAL APPROACH, THE ENGINE FLAMED OUT. RELIGHT ATTEMPT WAS UNSUCCESSFUL. AN UNEVENTFUL SINGLE ENGINE LANDING FOLLOWED. POST EVENT TROUBLESHOOTING, FOUND THAT THE ENGINE COULD NOT BE RE-STARTED. ACCESSORIES GEARBOX DE-COUPLE IS CONFIRMED. THE AFFECSDR YAD2008F00000Switch · failedPILOT REPORTED NOSE GEAR UNSAFE WARNING AFTER VARIOUS ATTEMPTS AT GEAR EXTENSION. GREEN LIGHT CAME ON AT TOUCHDOWN. VERIFIED NOSE GEAR DRAG BRACE SWITCH PLUNGER WAS "STICKY" AND WAS DEFLECTING STRIKER PLATE INSTEAD OF DEPRESSING SWITCH PLUNGER. REPLACED FAISDR CA080818002Controller · frozen(CAN) APPROXIMATELY 50 MIN OUT, AUTOPILOT BEGAN TO CLIMB, THE A/P WAS DISCONNECTED AND ACFT MANUALLY BROUGHT BACK TO ALTITUDE. A/P WAS REENGAGED AND THEN BEGAN TO DESCEND FOLLOWED BY THE AP TRIM FAIL ANN. A/P DISCONNECTED, ELECTRIC TRIM CHECK AND APPEARED SERVSDR FFS2008F00000Skin · dentedBIRD STRIKE ON TAKEOFF RESULTING IN DENTING OF FUSELAGE NOSE SKIN BEYOND MFG ALLOWABLE CONTOUR CHANGE LIMITS. AC RETURNED TO AIRPORT FOR UNEVENTFUL LANDING. (K)SDR ACE0519080Nipple · crackedPILOT REPORTED LOSS OF OIL PRESSURE, NR1 ENGINE. ENGINE SECURED IN FLIGHT AND AC RETURNED TO DEPARTURE AIRPORT AND MADE AN UNEVENTFUL LANDING. MAINT REPLACED THE NR1 ENGINE TORQUE PRESSURE LINE DUE CRACKED NIPPLE IN HOSE END. INSPECTION OF CRACKED HOSE NIPPSDR CA081203005Turbine · damaged(CAN) ACFT CRASHED UNDER UNKNOWN CIRCUMSTANCES. DURING THE FLT, THE PILOT RADIOED THAT HE HAD A LOSS OF PWR FROM ONE ENG FOLLOWED BY A "MAYDAY" CALL, APPROX 14 MIN LATER, DURING WHICH HE SAID THE SECOND ENGINE STOPPED OPERATING. THE ACFT WAS EQUIPPED WITH A FDSDR HSYA20080430Trim System · stuckDURING A TRAINING FLIGHT 25 MILES EAST OF AIRPORT, AT 5000 FT, THE ELEVATOR TRIM CONTROL BOUND AND JAMMED UP. AFTER ATTEMPTS TO FREE UP THE TRIM WERE UNSUCCESSFUL, THE CREW DECLARED AN EMERGENCY WITH CONTROL AND LANDED ON WITHOUT INCIDENT. MX PERFORMED A VISUSDR FFSA200800002Bearing · disintegratedRT OB (NR 4) MAIN WHEEL AND TIRE ASSEMBLY SEPARATED FROM AIRCRAFT ON LANDING ROLL. WHEEL BEARINGS FAILED ALLOWING WHEEL TO SEPARATE OVER THE AXLE NUT. THERE WERE 285 HOURS AND 256 CYCLES ON THE ASSEMBLY SINCE SCHEDULED BEARING INSPECTION AND LUBRICATION.SDR CA080423014Line · fractured(CAN) OPERATOR REPORTS (2) EVENTS OF POWER LOSS FOLLOWED BY ENGINE SHUT DOWN. ONE EVENT APRIL 17, 2008, THE OTHER APRIL 18, 2008. BOTH CAUSED BY FRACTURE OF THE PY LINE. AIRCRAFT RETURNED TO SERVICE FOLLOWING 2ND REPLACEMENT OF THE PY LINE. (TC# 20080423014)SDR FFSA200800001Door Frame · crackedDURING CONFORMITY INSPECTION, A CRACK WAS DISCOVERED IN THE OUTER FLANGE RADIUS RUNNING VERTICALLY DOWN FROM THE CUTOUT FOR THE AIRSTAIR DOOR SEAL JOGGLE. THE (2) RIVETS ATTACHING THE CENTER OF THE DOOR HINGE TO THIS STRUCTURE HAD BEEN WORKING.SDR EPUA33108Skin · corrodedDURING ROUTINE CAMP UNDERFLOOR INSPECTION, DISCOVERED CORROSION ON SKIN AND BETWEEN SKIN AND DOUBLER AT FS 523 TO FS 531. A REPLACEMENT SKIN APPROX 18 INCH BY 30 INCH WAS FABRICATED AND INSTALLED IN ACCORDANCE WITH THE BEECH SRM AND AIRCRAFT WAS RETURNED TO SSDR YADA032708001Tube · splitNOSE TIRE LOOSING AIR PRIOR TO DEPARTURE. REPLACED NOSE TIRE ASSY (FOUND INNER TUBE SPLIT ON CENTER SEAM .1250 INCH). THIS IS AN ADDITIONAL FAILURE OF A MFG INNER TUBE. THIS WAS A CANADIAN MANUFACTURED TUBE AND THE DEFECT WAS AT THE CENTER SEAM.SDR CA080402018Governor · misriggedTAKEOFF WAS ABORTED WHEN THE ENGINE WOULD NOT PRODUCE FULL POWER. INVESTIGATION REVEALED IMPROPER RIGGING OF THE PROP GOVERNOR.SDR EPUA031608Rib · crackedCRACK DISCOVERED DURING ROUTINE INSP ON VERT STAB RIB FLANGE AT RIB STRINGER INTERSECTION 39.5 AND RIB 54.026 CANT STAB STA, RT SIDE. REPAIRED CRACK IAW WITH APPROVED DATA, AIRCRAFT RETURNED TO SERVICE.SDR CA080208001Window · departed(CAN) DURING CLIMBOUT AT APPROX 3PSI DIFFERENTIAL, THE LT COCKPIT SIDE WINDOW BLEW OUT OF AIRCRAFT. IT IS DIFFICULT TO DETERMINE THE CAUSE AS THERE IS VERY LITTLE REMAINING OF THE ORIGINAL WINDOW. (TC NR 20080208001)SDR ACE020508Tube · splitNOSE TIRE LOOSING AIR AFTER LANDING (BET) REPLACED NOSE TIRE ASSY (FOUND INNER TUBE SPLIT ON SEAM 1/8). THIS IS THE LATEST IN A STRING OF INNER TUBE FAILURES FOR UNDETERMINED REASONS. THIS WAS A CANADIAN MANUFACTURED TUBE AND THE FAILURE SEEMS TO BE AT A DSDR CA080220005Engine · making metal(CAN) DURING DESCENT, THE PROPELLER AUTO-FEATHERED UNCOMMANDED. THE CREW ELECTED TO SHUTDOWN THE ENGINE AND PERFORMED A SINGLE ENGINE LANDING. POST FLIGHT INSP REVEALED A GRINDING NOISE WHEN TURNING THE PROP BY HAND. REDUCTION GEARBOX WAS CONTAMINATED WITH OILSDR CA080116007Line · chafed(CAN) FUEL FLOW INDICATION LINE FOUND CHAFED AND LEAKING. NEW LINE INSTALLED. (TC NR 20080116007)SDR ACE011208Tube · leakingPILOT REPORTED NOSE TIRE FLAT ON LANDING. REPLACED TIRE ASSEMBLY DUE FAILED INNER TUBE. WE ARE EXPERIENCING MULTIPLE FAILURES, BURST TUBES FROM THIS MFG. MFG PREVIOUSLY NOTIFIED.SDR ACE011108Tube · blownPILOT REPORTED NOSE TIRE FLAT ON LANDING. REPLACED TIRE ASSY DUE FAILED INNER TUBE. WE ARE EXPERIENCING MULTIPLE FAILURES / BURST TUBES FROM THIS MFG. MFG PREVIOUSLY NOTIFIED.
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