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 = '310Q' 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 = '310Q' 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 98ZZZX4244Hinge · brokenDURING ANNUAL INSPECTION, OUTBOARD, MAIN GEAR DOOR HINGE HALF (ATTACHED TO WING) HAD ONE SECTION BROKEN OFF. REPLACED HINGE HALF. THIS APPLIES TO BOTH WINGS.SDR 99ZZZX978Circuit Breaker · failedDURING IFR NIGHT-TIME FLIGHT, PILOT NOTICED RT ALTERNATOR FAILURE LIGHT HAD ILLUMINATED. PILOT NOTICED LIGHTS AND OTHER ELECTRICAL EQUIPMENT DIMMED AND PROCEEDED TO TERMINATE FLIGHT AT NEAREST AIRPORT. UPON EXAMINATION, FOUND RT ALTERNATOR BELT MISSING TEETHSDR 98ZZZX1241Bearing · wornREMOVED RMLG STRUT TO REPAIR LEAKING SEALS. FOUND INNER BEARING, WHICH HAD BEEN REPLACED IN C/W AD 90-02-13, WORN APPROXIMATELY .037 INCH. BRASS SHAVINGS MAY HAVE CAUSED SEALS TO FAIL.SDR 98ZZZX804Pump · failedOPERATOR HAS PURCHASED 3 NEW PUMPS FROM CESSNA BETWEEEN NOV 1996 - DEC 1997. ONE PUMP DEVELOPED A DIRECT SHORT, ONE PUMP WAS INTERMITTENT, THE OTHER PUMP FAILED. SUBMITTER STATED THIS IS A MANUFACTURER'S DEFECT. WEST STAR FURTHER STATED THAT SEVERAL PUMPS WSDR 98ZZZX488Bellcrank · failedLANDING GEAR WAS SELECTED 'UP'. LOUD BANG WAS HEARD. UPON INSPECTION, NOSE GEAR IDLER BELLCRANK WAS BROKEN OUT WHERE MAIN DRIVE TUBE FROM GEAR MOTOR ATTACHES TO IT. PART IS HARD TO PROPERLY INSPECT. RECOMMEND REMOVAL AND AND TESTING AT AT ANNUAL INSPECTION.SDR AU971627Rod End · seized(AUS) RH NOSE LANDING GEAR DOOR RETRACTION RODEND BROKEN. DOOR CAUGHT THE NOSE GEAR DURING RETRACTION AND JAMMED THE NLG HALFWAY UP.RODEND BEARING PARTIALLY SEIZED DUE TO LACK OF LUBRICATION.SDR AU971345Control · jammed(AUS) AILERON CONTROL SYSTEM JAMMED. EVIDENCE OF FOD LODGED BETWEEN CHAIN AND SPROCKET.SDR 97ZZZX3401Bellcrank · brokenPILOT REPORTED LOOSENESS IN RIGHT, INBOARD FLAP DURING PRE-FLIGHT. INSPECTION REVEALED INBOARD BELLCRANK ARMS, 2 EACH, BROKEN LOOSE FROM ASSY. SUBMITTER RECOMMENDS THOROUGH INSPECTION OF FLAP CONTROL SYSTEM DURING ANNUAL INSPECTION.SDR AU970371Blade · faulty(AUS) INCORRECT PROPELLER BLADES FITTED TO PROPELLER - BLADES FITTED ARE NOT THE BLADES LISTED IN THE LOG BOOK - REDUCED DIAMETER PROPELLER FITMENT NOT RECORDED - PROPELLER BLADE ANGLES VARIED BETWEEN BLADES - BLADE PROFILE INCORRECT - NO2 BLADE ACTUATING PIN SDR AU970266Propeller · faulty(AUS) LH PROPELLER SUSPECT OUT OF BALANCE - LH ENGINE FORWARD ENGINE MOUNT LOOSE - INVESTIGATION FOUND PROBLEM CAUSED BY BLADE ANGLES AND PROFILESSDR 97ZZZX1636Bellcrank · brokenDISCOVERED BELLCRANK BROKEN AFTER RIGHT MAIN LANDING GEAR COLLAPSED ON LANDING ROLL OUT.SDR 97ZZZX1245Switch · dirtyRIGHT ENGINE FUEL PUMP FAILED DURING FLIGHT. BOOST PUMP WOULD NOT RUN AND ENGINE STOPPED, UNEVENTFUL LANDING WAS MADE. FOUND FUEL PUMP DRIVESHAFT SHEARED. FOUND BOOST PUMPS WOLD PRIME ENGINE AND ALLOW ENGINE TO RUN, BUT WOULD NOT RUN IN HIGH OR LOW BOOST PUSDR 97ZZZX1244Pump · shaft shearedRIGHT ENGINE FUEL PUMP FAILED DURING FLIGHT. BOOST PUMP WOULD NOT RUN AND ENGINE STOPPED, UNEVENTFUL LANDING WAS MADE. FOUND FUEL PUMP DRIVESHAFT SHEARED. FOUND BOOST PUMPS WOLD PRIME ENGINE AND ALLOW ENGINE TO RUN, BUT WOULD NOT RUN IN HIGH OR LOW BOOST PUSDR 97ZZZX628Mount Bracket · crackedINSP FOUND LT ENG, FWD LT MOUNT, AFT BRACKET CRACKED.SDR 97ZZZX1181Belt · failedPILOT LOST RADIO CONTACT AND DIVERTED TO ALTERNATE AIRPORT. INVESTIGATION REVEALED ELECTRICAL POWER LOSS DUE TO ALTERNATOR, ALTERNATOR SENSOR, AND ALTERNATOR BELT FAILURE.SDR 97ZZZX1180Sensor · failedPILOT LOST RADIO CONTACT AND DIVERTED TO ALTERNATE AIRPORT. INVESTIGATION REVEALED ELECTRICAL POWER LOSS DUE TO ALTERNATOR, ALTERNATOR SENSOR, AND ALTERNATOR BELT FAILURE.SDR 97ZZZX1179Alternator · failedPILOT LOST RADIO CONTACT AND DIVERTED TO ALTERNATE AIRPORT. INVESTIGATION REVEALED ELECTRICAL POWER LOSS DUE TO ALTERNATOR, ALTERNATOR SENSOR, AND ALTERNATOR BELT FAILURE.SDR EY2R9601300Blade · corrodedBLADE, SN K95983YS, FOUND CORRODED.SDR EY2R9601299Blade · corrodedBLADE, SN F90225YS, FOUND CORRODED.SDR EY2R9601298Blade · corrodedBLADE, SN F84468YS, FOUND CORRODED.SDR EY2R9601297Ferrule · corrodedFERRULE FOUND CORRODED.SDR EY2R9601296Hub · corrodedHUB FOUND WITH CORROSION.SDR EY2R9601295Ferrule · corrodedFERRULE FOUND CORRODED.SDR EY2R9601290Blade · corrodedBLADE, SN F26156YS, FOUND CORRODED.SDR EY2R9601289Blade · corrodedBLADE, SN F26088YS, FOUND CORRODED.SDR EY2R9601288Blade · corrodedBLADE, SN F26105YS, FOUND CORRODED.SDR EY2R9600190Hub · crackedPROP ASSY HUB CRACKEDSDR 97ZZZX518Alternator · loose terminalALTERNATOR'S LOOSE CONNECTION CAUSED TERMINAL TO ARC AND BURN, AND DISCONNECT.SDR 96ZZZX6107Connect Rod · failedAFTER DEPARTURE, OIL PRESSURE ON RIGHT ENGINE DROPPED. ENGINE BEGAN TO SMOKE POSSIBLE BLEED OIL FIRE AND SMOKE WERE NOTED. ENGINE WAS SHUT DOWN AND FEATHERED. NORMAL LANDING WAS MADE. DAMAGE TO AIRCRAFT RESTRICTED TO ENGINE AND PROP. FIRST INSPECTION REVESDR 96ZZZX5960Bellcrank · failedPILOT HEARD A POP DURING GEAR EXTENSION. PILOT RETRACTED AND EXTENDED GEAR AND NOSE GEAR WAS NOT DOWN AND LOCKED. NO GREEN LIGHT, GEAR TRAILING AT A 45 DEGREE ANGLE. UPON LANDING, THE NOSE GEAR FOLDED AFT. INVESTIGATION REVEALED THAT THE BELLCRANK NEAR THESDR 96ZZZX5471Gasket · leakRED DYE LEAKAGE FROM THE PROP CYLINDER 'DOME' GASKETS. SPECIFICALLY WHERE THE DOWL PINS ARE. HAS BEEN A RECURRING PROBLEM JUST AFTER OVERHAUL. SUBMITTER STATES THIS SHOP HAS SEEN 7 PROPS LEAK AFTER THE OIL-FILL MOD. THESE OVERHAULS WERE PERFORMED BY 4 DIFFSDR 96ZZZX5121Bellcrank · brokenLEFT MLG INBD DOOR CAME OPEN AFTER TAKEOFF, REPORTED BY CONTROL TOWER. LANDING MADE WITHOUT INCIDENT. FND GEAR RETRACT IDLER BELLCRANK BROKEN 2 INCHES FROM END OF ARM THAT RUNS GEAR DOOR EXTEND/RETRACT LINKAGE. BELLCRANK SHOWS EVIDENCE OF HAVING BEEN CRACKESDR 96ZZZX5120Mount Assy · misinstalledEXCESS WIND NOISE FORM EMERGENCY EXIT WINDOW HAS BEEN A RECURRING PROBLEM. EACH TIME MAINTENANCE PERSONNEL HAVE TO RESECURE FORWARD PIN WHICH IS CONNECTED TO WINDOW RELEASE CABLE, THE CABLE HAS BEEN TOO SHORT AND THE PIN WOULD BARELY REACH. CLOSER INVESTIGATSDR EY2R9600984Hub · corrodedHUB CORRODED.SDR 96ZZZX5004Support · deformedDURING INSTALLATION OF LANDING GEAR KIT SK-414, FOUND SUPPORT DEFORMED AND STRUCTURE AT POINT OF ATTACH CRACKED. SUBMITTER URGENTLY RECOMMENDS THIS MODIFICATION BE MADE AN AIRWORTHINESS DIRECTIVE FOR ALL CESSNA 300 AND CESSNA 400 SERIES AIRCRAFT USING ELECTRISDR 96ZZZX5032Torque Tube · crackedDURING FLIGHT, PILOT NOTED THE ACFT SEEMED SLOWER AND YAWING TO THE LEFT. FLYBY INDICATED THE LEFT MAIN LANDING GEAR WAS DOWN WHILE THE RT AND NOSE WERE RETRACTED GEAR. SELECTED DOWN, ALL THREE INDICATED DOWN AND LOCKED. ACFT LANDED AT MAINTENANCE BASE WITHSDR AU961152Retention Nut · loose(AUS) NO3 PROPELLER BLADE RETENTION NUT LOOSE AND LOCK PLUGS MISSING - SUSPECT RETENTION NUT UNDERTORQUED - PERSONNEL/MAINTENANCE ERRORSDR 96ZZZX5002Torque Tube · crackedDURING 100-HOUR INSPECTION, FOUND BOTH LT AND RT TORQUE TUBES CRACKED (SMALL CRACKS) AT THE AREA WHERE THE FORK BOLT BOSS IS WELDED TO THE TUBE. HAVE SEEN THIS PROBLEM IN THE AIRWORTHINESS ALERTS BEFORE AND PAID CLOSE ATTENTION TO THIS AREA. THE PROBLEM WAS SDR 96ZZZX5001Torque Tube · crackedDURING 100-HOUR INSPECTION, FOUND BOTH LT AND RT TORQUE TUBES CRACKED (SMALL CRACKS) AT THE AREA WHERE THE FORK BOLT BOSS IS WELDED TO THE TUBE. HAVE SEEN THIS PROBLEM IN THE AIRWORTHINESS ALERTS BEFORE AND PAID CLOSE ATTENTION TO THIS AREA. THE PROBLEM WAS SDR EY2R9600861Nut · corrodedNUT CORRODED.SDR EY2R9600860Feather Cylinder · corrodedFEATHER CYLINDER CORRODED.SDR EY2R9600859Blade · corrodedBLADE, SN F19644YS, FOUND CORRODED.SDR EY2R9600858Blade · corrodedBLADE, SN F23333YS, FOUND CORRODED.SDR EY2R9600857Ferrule · corrodedFEATHER CYLINDER CORRODED.SDR EY2R9600097Hub · crackedHUB CRACKEDSDR EY2R9600096Hub · crackedHUB CRACKEDSDR 96ZZZX3347Bolt · looseGEAR SUPPORT LOCK NUTS WORKING LOOSE FROM BOLTS. SUBMITTER STATED ALSO HAVE FOUND BOLTS LOOSE ON OTHER AIRCRAFT. LOOSENING MAY BE CAUSED BY FLEXING OF THIS AREA.SDR 96ZZZX3346Bolt · looseGEAR SUPPORT LOCK NUTS WORKING LOOSE FROM BOLTS. SUBMITTER STATED ALSO HAVE FOUND BOLTS LOOSE ON OTHER AIRCRAFT. LOOSENING MAY BE CAUSED BY FLEXING OF THIS AREA.SDR AU960829Rib · mis mfg(AUS) LH WING END RIB NOT RIVETTED TO THE MAIN SPAR - SUSPECT RIVETS NOT INSTALLED AT MANUFACTURESDR AU960777Cylinder · separated(AUS) RH ENGINE NO5 CYLINDER HEAD SEPARATED FROM BARREL - SUSPECT PRE-EXISTING CRACK
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