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 = '310R' 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 = '310R' 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 BSY2003F00003Engine · malfunctionedRT ENGINE ON CLIMB OUT, STARTED LOOSING POWER. RETURNED, MAINTENANCE INSPECTED ENGINE SUMPED OK, NO WATER NOTED. GROUND RAN ENGINE, OPS CHECKED OK. NO FURTHER ACTION TAKEN.SDR A592002F00000Brace · brokenRIGHT MAIN LANDING GEAR LOWER SIDE BRACE LOCK ASSEMBLY WORN EXCESSIVELY, CAUSING ADJUSTING SCREW PIN TO CARRY WEIGHT OF AIRCRAFT, ADJUSTING SCREW THEN BEANT AND BROKE. RECOMMEND INSPECTING LOWER SIDE BRACE LOCK ASSEMBLY FOR WEAR.SDR AUS20021219Hub · worn(AUS) ALTERNATOR GEAR DRIVE HUB SLIPPING. FOUND DURING INSPECTION IAW MEB01-3.SDR AUS20021275Torque Tube · cracked(AUS) LH MAIN LANDING GEAR TORQUE TUBE CRACKED AND TWISTED.SDR CA021016036Exhaust Valve · stuck(CAN) VIBRATION ON RT ENGINE WITH FIRE, ENGINE FEATHERED. - FUEL LINE MANIFOLD VALVE TO NOZZLE BROKEN DUE TO STICKING EXHAUST VALVE ON CYLINDER NR 6. THE EXHAUST VALVE WAS DISMANTLED FOR CLEANING. A REEMER (PULL THROUGH) WAS PASSED THROUGH THE VALVE GUIDE ANSDR AUS20020970Torque Tube · cracked(AUS) RT MAIN LANDING GEAR TORQUE TUBE CRACKED IN WELDED AREA AROUNDTHE FORK BOLT. TORQUE TUBE INTERNALLY CORRODED.SDR AUS20020961Torque Tube · cracked(AUS) LT MAIN LANDING GEAR TORQUE TUBE CRACKED IN WELDED AREA AROUND THE FORK BOLT. TORQUE TUBE INTERNALLY CORRODED.SDR AUS20020742Landing Gear · misrigged(AUS) LANDING GEAR INCORRECTLY RIGGED. LANDING GEAR COMPONENTS DAMAGED DUE TO THE EXTENT THAT THE LANDING GEAR WAS OUT OF RIG. THE DEFECTS INCLUDE BENT RETRACT RODS, DENTED AND BENT UNDERCARRIAGE DRIVE TUBES, CORROSION AND RUST ON DRIVE TUBES, SEIZED AND RUSTESDR 2002FA0000874Hub · crackedPROPELLER SENT TO OUR REPAIR STATION FOR RED DYE LEAK CHECK. PROPELLER WAS DISASSEMBLED AND INSPECTED NR 1 AND NR 3 BLADE FERRULE WERE DRILLED TOO DEEP. NR 2 BLADE SOCKET WAS FILLED WITH RTV. NR 2 BLADE BEARING AND BALLS AND FERRULE WERE CONDEMNED FOR RUST SDR 2002F01106Cylinder · failedCYLINDER FAILED, RESULTING IN NO BRAKING ON RIGHT SIDE OF AIRCRAFT. PILOT FAILED TO MAINTAIN CONTROL OF AIRCRAFT, AIRCRAFT WENT BEYOND PAVED AREA OFF TAXI WAY ON TO GRASS AREA. NO DAMAGE WAS DONE TO THE AIRCRAFT. WHEN PILOT REALIZED THAT BRAKES WERE NOT WORSDR AUS20020622Blade · corroded(AUS) PROPELLER BLADES CORRODED IN AREA OF BLADE SHANK RADIUS.SDR AUS20020719Governor · making metal(AUS) LT ENGINE GOVERNOR METAL CONTAMINATION.SDR AUS20021112Bolt · failed(AUS) NO6 CYLINDER UPPER THROUGH BOLT FAILED.SDR CA020620003Alternator · failed(CAN) LT ALTERNATOR FAILED LIGHT CAME ON IN FLIGHT. RETURN TO BASE. MECHANICS CHECKED CONNECTIONS ON ALTERNATOR AND FOUND ALL WIRING CORRECT. THEY REMOVED THE ALTERNATOR AND FOUND THAT THE FRONT BEARING ON THE ALTERNATOR HAD FAILED. THIS IN TURN HAD CAUSED THESDR 2002FA0000669Oil Cooler · damagedTHE LISTED OIL COOLER WAS OVERHAULED. PROBLEM: THE THREADS FOR THE OIL TEMP PROBE WAS 40 PERCENT DESTROYED OR GONE. THIS AREA WAS NOT INSPECTED OR OVERLOOKED, WAS NOT POSSIBLE TO INSTALL OIL TEMP PROBE. RETURNED OIL COOLER TO OVERHAUL COMPANY.SDR BSY2002F00008Bellcrank · brokenGOING INTO AIRPORT, HAD NO NOSE GEAR DOWN LIGHT. ROCKED AIRCRAFT, GEAR THEN SHOWED DOWN AND LOCK. LANDED, NO PROBLEMS. FOUND BELLCRANK BROKEN ON GEARBOX, REMOVED AND REPLACED BELLCRANK, CHECKED RIGGING. OPS CHECKED GOOD.SDR 2002FA0000446Boot · destroyedDURING FLIGHT, ONE PROP BOOT DEPARTED AIRCRAFT. UPON INSPECTION IT WAS DETERMINED THAT THE PAINT DID NOT ADHERE TO THE BLADE PROPERLY AND THE BOOT CAME LOOSE.SDR AUS20020090Pipe · corroded(AUS) RH INBOARD FUEL TRANSFER PIPE CORRODED AND LEAKING.SDR AUS20020132Torque Tube · damaged(AUS) LANDING GEAR TORQUE TUBE DAMAGED. SUSPECT DAMAGE ORIGINATED FROM CRACKING AROUND THE FORK BOLT AREA.SDR BSY2001F00022Magneto · failed(OMA)(MIR) RIGHT ENGINE ON CLIMB OUT, SURGED, THEN SHUT DOWN. FOUND LEFT MAGNETO ON RIGHT ENGINE INOPERATIVE. REMOVED AND REPLACED MAG OPS CHECKS GOOD.SDR BSY2001F00019Sensor · failed(MKE)(MIR) LOST BOTH ALTERNATORS, THEN, RIGHT SIDE CAME BACK ON. REMOVED AND REPLACED BOTH ALTERNATOR OUT SENSORS. OPS CHECKS GOOD.SDR CA020116001Bracket · broken(CAN) FIRE IN COCKPIT ON DESCENT FROM FLIGHT TO AIRPORT. SMOKE EMITING FROM RT DASH BY PROP DE-ICE GAUGE. SMOKE TURNED TO FLAME AND EXTINGUISHER EXERCISED. EXAMINATION REVEALED POST LIGHT PLASTIC BROKEN AND FELL DOWN TO METER. LINE POST LIGHT SHORTED ON METSDR AUS20011266Wire · misinstalled(AUS) RT MAIN LANDING GEAR DOWNLOCK MICROSWITCH WIRING INCORRECTLY ROUTED CAUSING A STRAIN ON THE MICROSWITCH.SDR AUS20011225Fitting · corroded(AUS) RH WING UPPER FORWARD ATTACHMENT FITTING CONTAINED INTERGRANNULAR CORROSION IN THE UPPER SURFACES AND TWO AREAS OF PITTINGCORROSION. FOUND DURING INSPECTION IAW AD/C310/53.SDR AUS20011188Exhaust Valve · burned(AUS) NR 1 AND NR 3 CYLINDER EXHAUST VALVES BURNED AND ERRODED.SDR AUS20011176Screw · broken(AUS) RH MAIN LANDING GEAR DOWNLOCK ADJUSTING SCREW FAILED IN THREADEDAREA. RH MLG COLLAPSED.SDR AUS20011169Gear · loose(AUS) RH ENGINE ALTERNATOR DRIVE GEAR TO CRANKSHAFT ATTACHMENT BOLTSPNO 649205 LOOSE AND GEAR PNO 632018 LOOSE AND TEETH DAMAGED. ALTERNATOR BEARINGS FAILED. METAL CONTAMINATION OF OIL FILTER.SDR 2001F00586Torque Tube · crackedAIRCRAFT YAW, UNABLE TO AFFECT NORMAL ACCELERATION, COCKPIT INDICATION NORMAL. SUSPECT LEFT MAIN GEAR DID NOT RETRACT. CYCLED GEAR DOWN, 3 GREEN LIGHTS. NORMAL LANDING. NO AD'S, SB'S STC'S PMA'S APPLICABLE. NO SUGGESTION EXCEPT INCREASED MAINTENANCE VIGILSDR AUS20011244Stud · broken(AUS) LH ENGINE CYLINDER HOLDDOWN STUD BROKEN. CRANKCASE CRACKED. SEE ALSO MDR 01/1243.SDR AUS20011243Bolt · broken(AUS) LH ENGINE CRANKCASE THOUGH BOLT BROKEN. SEE ALSO MDR 01/1244.SDR AUS20010991Door · separated(AUS) EMERGENCY EXIT SEPARATED DURING FLIGHT. NO DAMAGE TO AIRCRAFT.SDR AUS20010935Rod End · broken(AUS) LH LANDING GEAR INBOARD RETRACTION ROD OUTBOARD RODEND BALL SOCKET FRACTURED.SDR AUS20010825Rib · cracked(AUS) WING RIBS LOCATED IN LH WHEEL BAY CRACKED AS INDICATED IN CESSNASERVICE LETTER ME76-2.SDR CA010703031Diode · failed(CAN) ON JUNE 23/01 THE PILOT SNAGGED HIS A/C AS THE LT ALTERNATOR BEING U/S/. UPON INSPECTION THE ALTERNATOR HAD A HOLE ON THE SIDE OF IT. REMOVED THE ALTERNATOR & BEFORE INSTALLING A NEW ONE, INSPECTED INSIDE THE ENGINE FROM WHERE THE ALTERNATOR WS REMOVED.SDR AJP2001F00002Skin · crackedWHILE PERFORMING INSPECTION, CRACKS DISCOVERED IN LEFT AND RIGHT HAND UPPER INBOARD SKINS, THESE CRACKS ARE APPROX 2 INCHES LONG (RIGHT) AND 4.5 INCHES LONG (LEFT) CRACKS IN NEARBY LOCATION ADDRESSED BY SB, SUSPECTED CAUSE: EXCESSIVE YAW LANDING/TAXIING, EXCSDR AJP2001F00001Rib · crackedWHILE PERFORMING INSPECTION, SHORT CRACKS (.1250 - .3750) FOUND IN CENTER RIB, CRACKS ARE AS DESCRIBED AND ISSUSTRATED IN SB. SUSPECTED CAUSE: EXCESSIVE CYCLES, EXCESSIVE YAW WHILE LANDING/ TAXIING. NO AD OR STR RELATED TO FAILURE.SDR AJP2001F00000Rib · crackedWHILE PERFORMING INSPECTION, SHORT CRACKS (APPROX .1250 - .3750), FOUND IN CENTER RIB, CRACKS ARE AS DESCRIBED AND ILLUSTRATED IN SB. SUSPECTED CAUSE: EXCESSIVE CYCLES, EXCESSIVE YAW, WHILE LANDING AND TAXIING. NO AD OR STC RELATIONSHIP ADDRESSES INSPECTIONSDR 20010420CW012Housing · crackedLT ENGINE NOT PRODUCING POWER, LEAKING OIL OUT LEFT LEFT TOP GRATE. INSPECTED, FOUND CASE CRACKED BELOW NR 1 CYLINDER AROUND PUSH ROD HOUSING ASSEMBLY AND NR 1 CYLINDER BOTH TOP AND BOTTOM FORWARD CYLINDER DOWN NUTS BROKEN OFF. REMOVED AND REPLACED ENGINE.SDR AU010304Alternator · failed(AUS) ENGINE DRIVEN ALTERNATOR SUSPECT REAR BEARING FAILED. DAMAGE TO ENGINE CRANKSHAFT DRIVE GEAR.SDR AU010328Alternator · failed(AUS) RT ALTERNATOR DISINTEGRATED. SEVERE INTERNAL DAMAGE. SUSPECTCAUSED BY BEARING FAILURE.SDR 20010430CW005Starter · failedTHIS STARTER WAS SUPPLIED WITH A ZERO TIME OVERHAULED ENGINE. THE ENGINE WAS INSTALLED JULY 20, 2000. STARTER FAILED MARCH 23, 2001 AFTER ACCUMULATING ONLY 396.7 HOURS. DID NOT DISASSEMBLE STARTER DUE TO WARRANTY.SDR AU010316Bearing · failed(AUS) RT ENGINE ALTERNATOR BEARING FAILED.SDR 20010430CW003Bellcrank · brokenPILOT HEARD POPPING NOISE OUT OF GEAR, WHEN GEAR WAS RETRACTED. SELECTED GEAR DOWN AND DID A FLYBY. TOWER SAID NOSE GEAR HALF WAY DOWN, FLEW TO AIRPORT AND LANDED, NOSE GEAR COLLAPSED. LIFTED AIRCRAFT ON TO RUNWAY. NOSE GEAR SWUNG DOWN AND LOCKED, ZERO RSDR AU010220Collar · mismanufactured(AUS) LT ENGINE CRANKSHAFT OIL TRANSFER COLLAR HAD INCORRECT CLEARANCE. THE MEASURED CLEARANCE WAS 0.0254MM (0.001IN) WITH THE CORRECTMANUFACTURERS LIMITS BEING 0.127MM TO 0.4572MM (0.005IN TO0.0018IN).SDR AU010164Tube · corroded(AUS) OUTBOARD PUSH-PULL TUBE LOCATED IN RT WHEEL WELL CORRODED INTERNALLY.SDR AU010158Bracket · broken(AUS) LH MAIN LANDING GEAR DOOR BRACKET FAILED.SDR AU010157Gear · damaged(AUS) LH ENGINE ALTERNATOR DRIVE GEAR DAMAGED AND OUTER SHELL DISTORTED. EVIDENCE OF VICE MARKS ON OUTSIDE OF SHELL. FURTHERDAMAGE FOUND:-1. OIL SEAL INSTALLED BACKWARDS.2. SUPPRESSOR CAPACITOR LOOSE INSIDE OF ALTERNATOR AND SCREW LOOSE. 3. PITTING IN CASE HARSDR AU010170Switch · worn(AUS) RT MAIN LANDING GEAR MICROSWITCH ARM WORN. ARM BROKE OFF DURING FLIGHT.SDR 2001FA0000095Pump · intermittentON THE LEFT SIDE OF AC, WE HAVE REPLACED THE CIRCULATING PUMP NUMEROUS TIMES WHILE RIGHT SIDE HAS BEEN FINE. MOST RECENT DATES OF REPLACEMENT AS FOLLOWS: 12-9-99 TACH 3443.5, 9-18-2000 3715.3, 12-29-2000 3882.4. AS STATED EARLIER ALL 3 OF THESE WERE ON THE LSDR AU010003Arm · cracked(AUS) RT MAIN LANDING GEAR INNER DOOR BELLCRANK IDLER ARM CRACKED.
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