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 = '95B55' 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 = '95B55' 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 20000831SH017Cam · strippedENGINE FAILURE CAUSED BY TEETH BEING STRIPPED OFF OF CAMGEAR. ONE TOOTH APPEARS TO HAVE BEEN FRACTURED AND THE FOLLOWING 6 TEETH WERE STRIPPED. GEAR WAS STILL PROPERLY FASTENED TO CAMSHAFT. THE CRANKSHAFT GEAR WAS NOT DAMAGED. NO FOREIGN MATERIALS WERE FOSDR 20000809SH030Sump · crackedFOUND THE SUMP CRACKED, CENTER FORWARD SECTION. CRACK OVERALL LENGTH, 2.75 INCHES. TWO SHORT SPUR CRACKS CAME OFF THE MAIN CRACK. (X)SDR CA000712029Spring · broken(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTON.SDR CA000712028Spring · cracked(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. FEATHER SPRING FOUND CRACKED.SDR 20000724SH025Piston Pin · brokenPORTION OF THE NR 6 CYLINDER PISTON PIN PLUG BROKE OFF AND CAUSED THE PISTON TO DISINTEGRATE. THIS CAUSED DAMAGE TO THE CONNECTING ROD ON THE NR 5 CYLINDER AND DAMAGE TO THE CRANKCASE. NO RECOMMENDATION TO PREVENT THIS AT THIS TIME. (X)SDR 20000721SH020Wheel · crackedA CRACK APPEARED ON NOSE WHEEL 3 INCHES TO 4 INCHES LONG ON THE OUTER HALF OF THE WHEEL. AS THE WHEEL IS INSTALLED, THE CRACK IS ON THE HORIZONTAL SURFACE BETWEEN THE HUB AND THE WHEEL FLANGE. THE CRACK WAS DISCOVERED BEFORE FAILURE OCCURRED. THE WHEEL WAS RSDR 20000620SH008Relay · failedPILOT REPORTED LANDING GEAR MOTOR CIRCUIT BREAKER WOULD TRIP WHEN SELECTING GEAR DOWN. TRIED EMERG EXTENSION HANDLE AND FOUND TIGHT. AFTER SEVERAL TRIES, PILOT WAS ABLE TO EXTEND L/G GEAR WITH THE EMERG EXTENSION HANDLE AND LANDED WITHOUT PROBLEMS. WHEN MAISDR 20000523SH024Bolt · brokenBOLTS BROKE AT BASE OF THREADS. MOST LIKELY CAUSED BY OVERTORQUING. THE BOLTS ARE WHEEL THROUGH BOLTS ON THE MAIN TIRES. (X)SDR 20000425SH038Hub · crackedCRACK IN HUB WAS FOUND WITH EDDY CURRENT INSPECTION. (X)SDR AU000121Skin · cracked(AUS) LT AND RT ELEVATORS PN 96-61005-655 (LT) AND PN 96-61005-656 (RT) HAD CRACKS IN THE TOP AND BOTTOM SKINS.SDR CA000128056Pin · missing(CAN) DURING INITIAL RETRACTION WHEN THE GEAR WAS SELECTED UP THE LEFT GEAR STAYED DOWN. WHEN THE GEAR WAS SELECTED DOWN EVERYTHING WAS NORMAL ON THE INDICATOR.INSPECTION REVEALED THAT THE SHEAR PIN ON THE LEFT GEAR WAS MISSING.THE GEARS WERE LUBRICATED & THE SDR 99ZZZX3467Cylinder · crackedENGINE HAD 266.2 HOURS SINCE A FACTORY ZERO TIMED OVERHAUL 11-24-99. RIGHT ENGINE SHUT DOWN IN-FLIGHT DUE TO VIBRATION AND VISIBLE OIL LEAKAGE. UPON NORMAL SINGLE ENGINE LANDING, TOP COWL WAS REMOVED TO FACILITATE INVESTIGATION. FOUND NR 5 CYL CRACKED AT 7SDR 99ZZZX3379Drag Brace · brokenDURING LANDING AT BNA, PILOT HEARD A 'POP' AS THE NOSE WHEEL TOUCHED DOWN. THE NOSE GEAR THEN COLLAPSED. THE NOSE GEAR AFT DRAG BRACE BROKE WHERE THE NOSE GEAR RETRACT ROD ATTACHES. BOTH OF THE TANGS THAT THE RETRACT ROD END FITS BETWEEN BROKE ALLOWING THE SDR AU990699Cap · corroded(AUS) LEFT WING UPPER SPAR CAP CONTAINED EXFOLIATION CORROSION.SDR 99ZZZX2445Line · wornRIGHT WING BOOT DE-ICE LINE RUBBED/MELTED THROUGH BECAUSE OF CONTACT WITH PNEUMATIC OUTPUT LINE FROM RIGHT ENGINE PUMP. VERY DIFFICULT TO INSPECT.SDR 99ZZZX972Bearing · failedLANDING GEAR RETRACTED NORMALLY AFTER TAKEOFF. ON RETURN, LANDING GEAR FAILED TO EXTEND. PILOT TRIED TO LOWER GEAR USING THE EMERGENCY PROCEDURES OUTLINED IN PILOT HANDBOOK, EXTENSION HANDLE WOULD NOT ENGAGE THE ACTUATOR WORM GEAR SHAFT. THE 5201K BEARING HSDR 99ZZZX696Mount · broken635.9 HOBBS. WHILE CHANGING CABLES ON THE LEFT ENGINE, MAINTENANCE NOTICED THE AFT INBOARD MOUNT LEG WAS BROKEN. FURTHER INSPECTION REVEALED THE FORWARD INBOARD LEG ALSO BROKEN. A COMPLETE INSPECTION OF THE ENGINE AND PROPELLER SHOWED NO OTHER DAMAGE. MINOSDR CA990311011Bearing · corroded(CAN) DURING INSPECTION, WHEN PROP WAS TURNED, GRINDING NOISES COULD BE HEARD COMING FROM THE STARTER OR STARTER ADAPTER. IT WAS CONCLUDED STARTER ADAPTER WAS NOT DISENGAGING. THE STARTER AND STARTER ADAPTER WERE REPLACED,TESTED SERVICEABLE AND AIRCRAFT RETURSDR CA990311003Motor · failed(CAN) AFTER TAKEOFF, THE LANDING GEAR MOTOR FAILED TO RETRACT WHEN SELECTED. THE AIRCRAFT RETURNED TO AIRPORT WITHOUT INCIDENT. THE LANDING GEAR MOTOR WAS FOUND AT FAULT AND WAS REPLACED.SDR 99ZZZX107Meter · malfunctionedLANDING GEAR RELAY CIRCUIT BREAKER TRIPS. REPAIRED SHORTED HOBBS METER WIRE IN PILOT'S SIDE PANEL.SDR CA981207022Camshaft · worn(CAN) PRE-INSPECTION RUN-UP, FOUND THE ENGINE RUNNING ROUGH AT IDLE. COMPRESSION CHECK FOUND NR 1 AND NR 2 WITH LOW COMPRESSION. THE CYLINDERS WERE REMOVED FOR INSPECTION AND THE CAMSHAFT LOBES WERE FOUND WORN. THE INTAKE LIFTER ON NR 2 CYLINDER WAS ALSO FOUSDR AU981553Tread · separated(AUS) NOSE LANDING GEAR TIRE TREAD SEPARATED. TIRE REMAINED INFLATED.SDR AU981569Tappet · worn(AUS) LT ENGINE NR 6 CYLINDER EXHAUST VALVE HYDRAULIC LIFTER CHIPPED AND PITTED. CORRESPONDING CAM LOBE ALSO BADLY WORN. PART TC: 97.SDR 98ZZZX4256Citcuit Breaker · failedTECHNICIAN WAS CYCLING CIRCUIT BREAKERS DURING ANNUAL INSPECTION. TWO CIRCUIT BREAKERS WOULD NOT OPEN. A 1-AMP AND 3-AMP BREAKER POWERING AVIONICS AUDIO SYSTEM WERE REPLACED. AS A PRECAUTION TO PREVENT FIRE HAZARD FROM NOT TRIPPING, 1-AMP BREAKER DID DISENGSDR 98ZZZX4828Spar · bentDURING ANNUAL INSPECTION, THE DOUBLER WAS FOUND BENT DUE TO PRE-EXISTING DAMAGE TO FORWARD WEB OF FRONT SPAR CARRY-THROUGH STRUCTURE. SUBMITTER STATED AIRCRAFT HAS A HISTORY OF GEAR UP LANDING.SDR 98ZZZX4827Spar · bentDURING ANNUAL INSPECTION, THE DOUBLER WAS FOUND BENT AND PARTIALLY SEPARATED FROM AFT WEB OF FRONT SPAR CARRY-THROUGH STRUCTURE DUE TO PRE-EXISTING DAMAGE TO WEB. SUBMITTER STATED AIRCRAFT HAS A HISTORY OF PREVIOUS GEAR UP LANDING.SDR 98ZZZX4577Web · buckledDURING ANNUAL INSPECTION, THE FRONT SPAR CARRY-THROUGH STRUCTURE AFT WEB WAS FOUND BUCKLED IN THE LEFT LOWER WING ATTACH FITTING AREA. THE DAMAGE EXTENDED FROM THE LOWER OUTBOARD TO AND THROUGH THE UPPER INBOARD HUCK BOLTS. IT ALSO EXTENDED HORIZONTALLY BELOSDR 98ZZZX4068Web · buckledDURING ANNUAL INSPECTION, THE FRONT SPAR CARRY-THROUGH STRUCTURE FORWARD WEB WAS FOUND BUCKLED BELOW THE LT WING ATTACH FITTING. THE DAMAGE EXTENDED BETWEEN THE LOWER SKIN AND THE FITTING HORIZONTALLY FOR APPROX 12 INCHES. THERE WAS ADDITIONAL DEFORMATION INBOSDR AU981271Cap · corroded(AUS) LEFT WING UPPER SPAR CAP CONTAINED EXFOLIATION CORROSION LOCATED ADJACENT TO PITOT HEAD AND EXTENDING OUTBOARD THROUGH THE LEADING EDGE RIBS. FOUND DURING INSPECTION IAW AD/BEECH55/29 AMDT 1. PART TC: 29,054.SDR 99ZZZX679Rod · separatedENGINE DEVELOPED EXTREME VIBRATION CLIMBING THROUGH 2,500 FEET MSL. OIL OBSERVED COMING FROM COWLING. ENGINE SHUT DOWN AND SECURED. POST-FLIGHT INSPECTION REVEALED NR 4 CYLINDER CONNECTING ROD EXITED THROUGH CRANKCASE. PISTON BROKEN. SEVERAL INTERNAL PARTSDR 98ZZZX3218Tire · failedNLG TIRE TREAD AND CORDS DISINTEGRATED ON LANDING. TREAD IS MISSING AND ALL CORDS SEVERED. TIRE WAS STILL HOLDING AIR.SDR AU980934Rivet · missing(AUS) RIVETS MISSING FROM FUSELAGE IN AREA FROM DORSAL FIN FORWARD TO FIN STERN POST. SUSPECT RIVETS CORRODED. SKIN LAP JOINTS HAVE SEPARATED OVER A LENGTH OF APPROXIMATELY 2.1 METRES (7 FEET).SDR CA980724022Low Pitch Stop · stripped(CAN) LEFT SPINNER FOUND LOOSE. FURTHER INSPECTION FOUND THAT THE THREADS ON THE LOW PITCH STOP WERE STRIPPED. FORWARD END OF SPINNER IS SECURED ONTO THE LOW PITCH STOP.SDR CA980707043Low Pitch Stop · stripped(CAN) DURING INSPECTION, THE PROPELLER SPINNER WAS FOUND LOOSE. INVESTIGATION FOUND THE THREADS ON THE LOW PITCH STOP WERE STRIPPED. THE FORWARD END OF THE SPINNER IS SECURED TO THE LOW PITCH STOP. THIS LOW PITCH STOP WAS INSTALLED 24 HOURS PREVIOUSLY FOR TSDR 98ZZZX2129Alternator · failedAIRCRAFT LOST ALL ELECTRICAL POWER IN-FLIGHT. EMERGENCY LANDING MADE. MAINTENANCE FOUND BOTH FIELD FUSES BLOWN. INSPECTION OF ACFT REVEALED FOLLOWING: RT ALTERNATOR WAS MISSING COOLING FAN. ONE REGULATOR ONLY 26.5 VOLT OUTPUT. RT ALTERNATOR OUTPUT TERMINSDR CA980529008Rod · bent(CAN) RIGHT HAND GEAR COLLAPSED AFTER LANDING. SUBSEQUENT MAINTENANCE CHECK REVEALED THAT THE RIGHT HAND RETRACT ROD WAS BENT AT THE ACTUATOR END. POSSIBLE CAUSE FOR THE BENT ROD WAS DUE TO THE RT UPLOCK FAILING TO RELEASE CAUSING THE ROD TO BEND AS THE RETRSDR CA980525010Cable · broken(CAN) THROTTLE CABLE BROKEN AT ENGINE CONTROL END. CABLE REPLACED.SDR AU980931Bracket · worn(AUS) LEFT MAIN LANDING GEAR JAMMED DURING RETRACTION. AIRCRAFT LANDED WITH LEFT MLG RETRACTED CAUSING DAMAGE TO THE LT WINGTIP, LT FLAP , LT AILERON, LT STABILATOR, LT PROPELLER, AND LT ENGINE.SDR AU980168Encoder · failed(AUS) ALTITUDE ENCODER FAULTY. PERSONNEL/MAINTENANCE ERROR.SDR 98ZZZX81Bulkhead · crackedDURING ANNUAL INSPECTION, FOUND CRACKING IN TAIL AT FS 271.92 BULKHEAD. REPAIRED PER BEECHCRAFT SI 990. AREA VERY HARD TO INSPECT. SI 990 ALSO HAS INSPECTION CRITERIA. CRACKING FOUND ON 3 AIRCRAFT AT THIS STATION WHILE C/W SI 990. SUBMITTER SUGGESTED BULLSDR CA971216043Cable · separated(CAN) PILOT REPORTED LOSS OF MIXTURE CONTROL ON THE RIGHT ENGINE. INSPECTION FOUND THE MIXTURE CABLE HAD FAILED AT THE SWAGE OF THE ENGINE END OF THE CABLE. THIS IS THE THIRD FAILED CABLE ON THIS AIRCRAFT IN 85 HOURS OF OPERATION. CABLES FORWARDED TO MANUFASDR CA971121003Cable · broken(CAN) SHORTLY AFTER TAKEOFF, THE A/C CAPTAIN REPORTED THE RT MIXTURE WAS NOT RESPONDING NORMALLY. A/C RETURNED TO DEPARTURE POINT. MAINTENANCE INVESTIGATION FOUND THE MIXTURE CABLE HAD BROKEN AT THE ROD END TO ENGINE. THIS IS THE THIRD FAILURE OF THIS KINDSDR CA971121002Cable · broke(CAN) RT MIXTURE WAS REPORTED AS STICKING, NIL RESPONSE. MAINTENANCE INVESTIGATION FOUND THE MIXTURE CABLE HAD BROKEN AT THE ROD END TO THE ENGINE. THIS IS THE SECOND TYPE OF OCCURRENCE.SDR CA971121001Cable · broke(CAN) THE RT ENGINE FUEL MIXTURE CABLE FAILED ON APPROACH. THIS ACTION RESULTED IN THE RT ENGINE MIXTURE ROLLING BACK TO IDLE CUT-OFF STOPPING THE ENGINE. MAINTENANCE INVESTIGATION REVEALED THE MIXTURE CABLE FAILED AT THE SWAGE ATTACHMENT END TO THE ROD AT TSDR CA971015058Camshaft · worn(CAN) THE NR2 ENGINE OIL PAN WAS REMOVED TO FACILITATE THE REPAIR OF AN OIL LEAK. INSPECTION OF THE NOW EXPOSED AREA FOUND THE NR5 CYLINDER EXHAUST VALVE CAM LOBE BADLY WORN. THE ENGINE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.SDR 97ZZZX3162Pedal · wornWHILE INSPECTING THE PILOT'S RUDDER PEDALS AT THE ANNUAL INSPECTION, THE PILOT'S PEDAL ARMS WERE FOUND WORN AT THE PEDAL TO ARM ATTACH PIVOT HOLES; .0625 INCH OF ARM WAS LEFT IN THE AREA AROUND THE BUSHING AT THE PIVOT POINT. SUBMITTER STATED TIME ON AIRCRAFTSDR 97ZZZX3161Pedal · wornWHILE INSPECTING THE PILOT'S RUDDER PEDALS AT THE ANNUAL INSPECTION, THE PILOT'S PEDAL ARMS WERE FOUND WORN AT THE PEDAL TO ARM ATTACH PIVOT HOLES; .0625 INCH OF ARM WAS LEFT IN THE AREA AROUND THE BUSHING AT THE PIVOT POINT. SUBMITTER STATED TIME ON AIRCRAFTSDR 97ZZZX3542Bellcrank · failedRUDDER PEDAL INTERCONNECT REARWARD PROTRUDING ARM BROKE COMPLETELY OFF APPROXIMATELY 1 INCH FORWARD OF INTERCONNECT ROD PIVOT. BELLCRANK BROKE DURING GROUND OPERATIONS WHEN FLIGHT INSTRUCTOR APPLIED PRESSURE ON RUDDER PEDAL OPPOSITE OF THE STUDENT, IN ORDER TSDR 97ZZZX3450Selector Valve · leakTHIS VALVE INSTALLED TO REPLACE 2 OTHER PREVIOUS VALVES INSTALLED AS NEW THAT FAILED A SHORT TIME AFTER INSTALLATION.SDR AU970651Skin · corroded(AUS) RH WING LOWER SKIN CORRODED THROUGH AT FORWARD INBOARD END -CORROSION INITIATED BETWEEN SKIN AND DOUBLER INSTALLED AT INBOARD END OF SKIN BETWEEN WS 66.0 AND WS 80.0
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