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 = '650' 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 = '650' 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 GMCR97001Window · shatteredTHIRTY MINUTES AFTER DEPARTURE FROM SLC, THE CREW HEARD A LOUD BANG, AND NOTICED THE OUTER PANE OF THE RIGHT COCKPIT WINDOW HAD SHATTERED. THE CREW DECLARED AN EMERGENCY AND HAD AN UNEVENTFUL LANDING BACK AT SLC. NO FRAGMENTS OF THE OUTER PANE HAD SEPARATED SDR CA970225002Controller · failed(CAN) DURING CRUISE FLIGHT, THE LEFT HAND STABILIZER ANTI-ICE FAIL LIGHT ILLUMINATED. FLIGHT LANDED AND CONTROLLER WAS CHANGED.SDR WG1R583KAlternator · bearing failedPILOT REPORTED VIBRATION COMING FROM NR 1 ENG WHICH VARIED WITH THROTTLE ALONG WITH A VOLTAGE SPIKE ON AC VOLTMETER. AFTER EXTENSIVE TROUBLESHOOTING, FOUND ALTERNATOR BEARINGS HAD FAILED, SHORTING OUT ALTERNATOR CONTROL UNIT, AC VOLT METER AND HORIZ STAB ANTISDR 96ZZZX5059Valve · faultyFLIHGT CREW REPORTED LEFT EMERGENCY PRESSURIZATION WOULD NOT WORK UNLESS WINDSHIELD AIR SELECTOR ON. INVESTIGATION REVEALED FAULTY ANTI-ICE MASTER VALVE. REPLACEMENT VALVE CLEARED PROBLEM.SDR 96ZZZX5058Fire Loop · faultyFLIGHT CREW REPORTED LEFT FIRE DETECTOR FAIL ANNUNCIATOR LIGHT ON. FIRE TEST NORMAL. INVESTIGATION REVEALED FIRE DETECTOR LOOP RUBBED THROUGH INBOARD SIDE UNDER AFT ENGINE SHROUD. REPLACEMENT LOOP CLEARED PROBLEM.SDR 96ZZZX5055Switch · failedFLIGHT CREW REPORTED COCKPIT PAC OVERHEAT LIGHT ON AT FL 410. LIGHT STAYED ON AFTER LANDING. INVESTIGATION FOUND FAULTY PAC OVERHEAT SWITCH. REPLACEMENT SWITCH CLEARED PROBLEM.SDR 96ZZZX5148Carrier · brokenNR 1 BRAKE MAKES NOISES WHILE TOWING AIRCRAFT. FOUND FIRST CARRIER AND LINING ASSY BROKEN IN THREE PIECES. BRAKE ASSY PN 2-15-02 B. F. GOODRICH. AIRCRAFT TOTAL TIME: 1,036.9 HOURS. 753 LANDINGS.SDR 96ZZZX5147Piston Tube · disconnectedNOSE GEAR PISTON-TUBE DISCONNECTED FROM UPPER BARREL. LOCKING ASSY, PN 6242124-1, BACKED OFF FROM PISTON TUBE, PN 6242122-2. THE AFT TORQUE LINK WAS THE ONLY THING WHICH PREVENTED THE PISTON TUBE, WHEEL FORK, AND NOSE WHEEL FROM SEPARATING FROM AIRCRAFT. LOSDR 96ZZZX5258Line · crackedRIGHT STAINLESS STEEL HYDRAULIC LINE COMPRESSED FITTING CRACKED, SOME HYDRAULIC FLUID WAS LOST AND SYSTEM PRESSURE DROPPED. REASON FITTING CRACKED IS UNKNOWN. LINE WAS REPAIRED BY CESSNA AIRCRAFT PERSONNEL AND DISPATCHED BY THEM.SDR 96ZZZX4828Gps System · errorsUNIT DOES NOT CONFORM TO ARINC 419 STANDARDS WHEN THE UNIT WAS PROPERLY INSTALLED AND CONFIGURED TO SUPPLY NAVIGATION INFO TO THE EFIS SYSTEM, SOME BITS OF INFORMATION WERE ERRONEOUS.SDR 96ZZZX4827Gps System · errorsUNIT DOES NOT CONFORM TO ARINC 419 DATABUS STANDARDS. WHEN UNIT WAS PROPERLY INSTALLED AND CONFIGURED TO SUPPLY NAVIGATION INFO TO THE EFIS SYSTEM, SOME UNITS OF INFORMATION WERE ERRONEOUS.SDR AU961070Friction Brake · contam-water(AUS) NOSE LANDING GEAR CENTERING AND FRICTION BRAKE DAMPER SYSTEM CONTAMINATED WITH WATER CAUSING LUBRICATION TO BE WASHED OUT AND PREVENTING NLG FROM RETRACTING - AIRCRAFT WAS LANDING AND TAKING OFF IN HEAVY RAINSDR 96ZZZX2964Tire · defectiveON TAKEOFF FROM PBI, GEAR UNSAFE LIGHT REMAINED ON WHEN GEAR WAS RETRACTED. OPERATOR FLEW BY TOWER FOR CONDITION CHECK. GEAR WAS REPORTED UP AND LOCKED. AFTER SEVERAL GEAR CYCLES, GEAR UNSAFE LIGHT WENT OUT. AFTER LANDING AT MORRISTOWN, NR 2 TIRE FOUND TO SDR 96ZZZX1949Filter · failedDURING MAINTENANCE INSPECTION OPERATION 10, ITEM CARD 27-20 INSPECTION REVEALED FILTER SEPARATED FROM MOUNTING FLANGE IN THE END OF ELBOW FITTING PERMITTING IT TO SLIDE BACK AND FORTH WITHIN THE FITTING. THIS NEGATES FILTERING. REPLACED ELBOW FILTER FITTING.SDR AU960415Actuator · failed(AUS) HORIZONTAL STABILISER PRIMARY TRIM ACTUATOR FAILED INTERNALLYSDR 96ZZZX1129Engine · oil lossENGINE EXHIBITED LOW OIL PRESSURE AND ENGINE WAS SHUT DOWN. AIRCRAFT MADE NORMAL LANDING ON SINGLE ENGINE. FOUND TWO QUARTS OF OIL IN ENGINE. NORMAL CAPAPCITY (6 QUARTS). COULD NOT DUPLICATE ANY MALFUNCTIONS DURING TROUBLESHOOTING, BUT SUSPECT OIL SYSTEM PSDR 96ZZZX1628N1 Monopole · failedAPPROXIMATELY 45 MINUTES INTO THE FLIGHT, CLIMBING OUT OF FL 387, A SUDDEN YAW WAS FELT, THE RIGHT ENGINE POWER HAD DECREASED, AND THE RT 'FUEL COMP MANUAL' LIGHT WAS ILLUMINATED. THE FUEL COMPUTER WAS CYCLED BACK PER CHECKLIST, BUT WOULD NOT REMAIN ON LINE SDR 97ZZZX530Wire · chafedINSP OF CB PANEL ASSY FOLLOWING FINDING CHAFED WIRING ON ANOTHER CE 650, FOUND LIKE CONDITION ON THIS ACFT. INSP CONDUCTED AT CESSNA SERVICE CENTER SACRAMENTO, CA.SDR 97ZZZX529Wire Harness · shortedRT HAND ENGINE FAN (N1) INDICATOR CIRCUIT BREAKER TRIPPED AND WILL NOT RESET. FOUND WIRING HARNESS IN PILOT'S CIRCUIT BREAKER PANEL ASSEMBLY CHAFING AND SHORTING TO GROUND. THE CHAFED WIRES AT THE AURAL WARNING NR 1 AND WARNING LIGHTS NR 1 CIRCUIT BREAKERS WSDR 96ZZZX558Transponder · failedREINSTALLED ADC AFTER MOD STATUS UPGRADE AND CERTIFICATION. WHILE COMPLYING WITH CFR SECTION 91.411/91.413 FUNCTION TEST, NOTED NR 2 TRANSPONDER ALTITUDE READ-OUT WAS INVALID FROM 500 FEET TO 1,000 FEET AND AT EACH ASCENDING 500 FOOT INCREMENT TO THE NEXT THOSDR 96ZZZX498Fuel Cell · contaminatedWHILE PERFORMING A PHASE 5 INSPECTION WHERE ALL THE FUEL PANELS ARE OPENED UP, THERE WERE APPROXIMATELY 8 FUEL IDENTIFICATION LABELS LOCATED LOOSELY INSIDE WING. IN THE SUMP AREA THERE WERE 2 LABELS STUCK IN A FLAPPER VALVE. THE LABELS ARE APPROXIMATELY 1 INSDR 96ZZZX751Actuator · water contamACFT FLEW 3 LEGS, NO PROBLEMS. ON 4TH TAKEOFF, AT 100 KNOTS, RUDDERS LOCKED. T/O ABORTED. DURING TAXI BACK, RUDDER & NOSE STEERING WORKING NORMALLY. RUDDER BIAS TESTED NORMAL. CNTRL LOCK RELEASED. T/O ATTEMPED & AT 100-105 KNOTS, RUDDER CNTRLS LOCKED AGASDR 96ZZZX381Brake Rotor · crackedFOUND ALL 3 ROTORS ON NR 4 BRAKE CRACKED FROM THE HOLES, OUTWARD. TWO OF THE ROTORS WERE BROKEN IN TWO.SDR 95ZZZX7021Brake Assy · brokenAIRCRAFT TT 738.7 HRS. DURING NR 3 RIGHT INBOARD TIRE CHANGE, FOUND INBOARD, FIRST CARRIER AND LINING ASSYS BROKEN IN 2 PIECES. BRAKE ASSY PN 21502 BF GOODRICH CESSNA PN 9914136-1. MANUAL NR 32-46-41, PAGE 1006, ITEM NR 90. APR 28/89 DATED. DEFECTED PART SDR 95ZZZX5533Blade · shroud missingONE BLADE TIP SHROUD FOUND MISSING DURING POST-FLIGHT ON NR 3 LOW PRESSURE TURBINE.SDR 95ZZZX4531Rotor Disk · crackedDURING ROUTINE TIRE CHANGES, WHEELS WERE REMOVED AND BRAKE ROTORS FELL OUT IN PIECES. REMOVED WHEELS FROM OPPOSITE GEAR AND BRAKE ROTORS WERE FOUND BROKEN ON THAT SIDE AS WELL. PILOTS SAY THEY ARE VERY 'GENTLE' ON THEIR BRAKES AS THEY DO NOT FLY INTO SHORT SSDR 95ZZZX4467Actuator · failedPITCH TRIM ACTUATOR, SN 187, FAILED 16 FLIGHT HOURS AFTER INSTALLATION. SN 186 WAS INSTALLED IN ITS PLACE, AND IT FAILED ON THE FOLLOWING DAY (EXACT NUMBER OF HOURS IN USE AFTER INSTALLATION UNKNOWN AT THIS STATION).SDR 95ZZZX4466Actuator · failedPITCH TRIM ACTUATOR, SN 187, FAILED 16 FLIGHT HOURS AFTER INSTALLATION. SN 186 WAS INSTALLED IN ITS PLACE, AND IT FAILED ON THE FOLLOWING DAY (EXACT NUMBER OF HOURS IN USE AFTER INSTALLATION UNKNOWN AT THIS STATION).SDR 95ZZZX5522Fitting · failedDURING MAINTENANCE INSPECTION, OPERATION 10, ITEM CARD 27-20, INSPECTION REVEALED SPOILER SHUTTLE VALVE FILTER SEPARATED FROM MOUNTING FLANGE IN THE END OF ELBOW FITTING PERMITTING IT TO SLIDE BACK AND FORTH WITHIN THE FITTING. THIS NEGATED FILTERING CAPABILISDR 95ZZZX4287Actuator · failedINTERMITTENT PITCH TRIM FAIL INDICATION. TIME IN SERVICE OF THIS REPAIRED PART - 16.8 HOURS. THIS IS THE FOURTH FAILURE OF THIS PART ON THIS AIRCRAFT.SDR 95ZZZX3821Actuator · failedREPAIRED UNIT FROM CRS-BS4R087M REINSTALLED, 6-8-95. TEST FLIGHT AT ALTITUDE FAILED. UNIT STILL GOING INOP AFTER COLD SOAKING. REINSTALLED RENTAL UNIT AND RETURNED S/N 222 TO VENDOR 6-14-95. CONDITION CAUSE UNKNOWN AT THIS TIME.SDR 95ZZZX3727Adapter Spline · strippedRIGHT ENGINE WOULD NOT ROTATE WHEN STARTER BUTTON ENGAGED. FOUND OUTER SPLINES ON ADAPTER STRIPPED. LEFT ENGINE SPLINE ADAPTER ALSO WORN EXCESSIVELY. MFG RECOMMENDS INSPECTION AT 2,100 HOUR INTERVALS. OPERATOR CONTROL NR 95-003.SDR 95ZZZX5239Bracket · crackedDURING A SCHEDULED INSPECTION, DISCOVERED THE RT MLG DOOR CRADLE BRACKET CRACKED APPROXIMATELY THREE-FOURTHS OF THE WAY THROUGH AT THE BEND WHERE IT ATTACHES TO THE FORWARD SIDE OF MAIN GEAR DOOR. NOTICED THE NEW BRACKET RECEIVED FROM CESSNA WAS MADE OF STAINSDR 95ZZZX5238Probe · lug shortedPILOT REPORTED ERRATIC FUEL QUANTITY INDICATION DURING FLIGHT. PROBLEM COULD NOT BE DUPLICATED ON THE GROUND. INVESTIGATION REVEALED THE LOA-Z WIRE LUG AT FUEL QUANTITY PROBE NR 7 WAS VERY CLOSE TO THE FORWARD FUEL VENT LINE AND WAS APPARENTLY, THROUGH TEMPESDR 95ZZZX3432Pitch Trim Act · failedREPAIRED UNIT FROM CRS-BS4R087M. REINSTALLED. 6-8-95 - TEST FLIGHT AT ALTITUDE FAILED. UNIT STILL GOING INOP AFTER COLD SOAKING. REINSTALLED RENTAL UNIT AND RETURNED SN 222 TO VENDOR 6-14-95. CONDITION CAUSE UNKNOWN AT THIS TIME. THIS OPERATOR - 135 CERTSDR 95ZZZX4452Line · crackedTHE CREW INDICATED THE LEFT ENGINE WOULD NOT MAKE POWER AT CRUISE ALTITUDE. UPON INVESTIGATION, FOUND THE P2T2 SENSE LINE WAS CRACKED AT THE PROBE. SUBMITTER RECOMMENDS THE LINE BE REPLACED WITH A SUITABLE FLEXIBLE LINE. THIS WILL ELIMINATE THE POSSIBILITY SDR 95ZZZX1325Sensor Fan · inopCABIN TEMP INDICATES MID-50'S REGARDLESS OF 'REAL' TEMP IN CABIN. SEEMS TO RUN FULL-HOT IN AUTOMATIC, OKAY IN MANUAL. DISCOVERED AFT SENSOR FAN DEAD. REPLACED AFT SENSOR FAN AND ON RUN-UP, TEMPERATURE CONTROL FUNCTIONED NORMAL IN AUTO AND MANUAL.SDR 95ZZZX908Line · chafedPOWER BRAKE METERING VALVE HYDRAULIC RETURN LINE RUNS CLOSE TO THE VALVES LOWER CONTROL ARM. THE CABLE ATTACH BOLT COTTER PIN MUST BE TRIMMED PROPERLY TO AVOID CONTACT WITH THE LINE.SDR 95ZZZX1200Inlet Assy · crackedLEFT ENGINE INLET ANTI-ICE RING FOUND FRACTURED AT THE 6:00 AND 9:00 POSITIONS. REPAIRED BY WELDING AND INSTALLING REINFORCING GUSSETS. SUBMITTER SUGGESTS REDESIGNING INLET ANTI-ICE RING WITH SLIP COUPLING OR FLEXIBLE CORRECTION TO ALLOW FOR EXPANSION AND COSDR 95ZZZX1023Windshield · crackedPILOT'S WINDSHIELD OUTER LAYER CRACKED WHILE TAXIING TO RAMP AFTER LANDING.SDR 95ZZZX684Inlet Tube · fracturedLEFT ENGINE INLET ANTI-ICE RING FOUND BROKEN AT 12:00 POSITION. REPAIRED ANTI-ICE RING BY WELDING AND INSTALLING REINFORCING GUSSET.
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