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 = '767209' 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 = '767209' 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 CA050713004Actuator · malfunctioned(CAN) DURING CRUISE FWD CARGO DOOR LIGHT CAME ON. QRH FOLLOWED WITH A DESCENT AND DIVERSON TO YHZ. NO FLUCTUATION IN PRESSURIZATION. NO BUFFET. FWD CARGO LATCH/HOOK ACTUATOR REPLACED AS PER AMM52-33-0.SDR CA050706004Window · arcedBURNING SMELL DETECTED IN COCKPIT. ACFT DIVERTED. OVERWEIGHT LANDING BY 10,600 KL AND SMOOTH LANDING. FOUND CAUSE OF BURNING SMELL AT GROUND CONN OF RT NR 3 WINDOW. DE-ACT RT NR 3 AS PROCEDURES C/B P36-H7 PULLED AND COLLARED NR3 RT WINDOW HEAT INOP.SDR CA050614002Control Lever · failed(CAN) FAULT: EICAS MESSAGE (LDG GEAR MONITOR) LANDING GEAR IND 3 GREEN. ALSO RECEIVED A GRN PROX (TOO LOW GEAR) RECYCLED THE GEAR. LANDED WITH NORMAL INDICATIONS. REPLACED LDG GEAR CONTROL LEVER MODULE IAW AMM 32-31-01 PG 1-5. AND CABLE TENTION ADJUSTED IAW SDR CA040113002Actuator · failed(CAN) ON PRE-DESCENT CHECK WHEN FUEL CROSSFEED WAS CHECKED ON AND OFF, EICAS MESSAGE FUEL CROSSFEED AND VALVE LIGHT ON CROSSFEED SWITCH REMAINED ILLUMINATED. ON GROUND RECYCLED CIRCUIT BREAKER NIL FIX. TAKEN OFF LINE FOR INVESTIGATION FLT CANCLED PART: ELECTRSDR CA020806007Seal · failed(CAN) THIS ENGINE WAS REMOVED DUE TO HIGH OIL CONSUMPTION, REFURBISHED AND WITH BELOW 2000 HRS ON WING . BEARING SEALS FAILED. SEALS HAD JAMMED IN THEIR HOUSINGS IN REARWARD POSITION RENDERING THEM USELESS.SDR CA020807001Warning System · activated(CAN) REJECTED TAKE OFF RTO. AT 145 KTS. DUE CONFIGURATION WARNING.SDR CA010924008Screw · loose(CAN) UPON LANDING IN TORONTO THE BULK CARGO DOOR OPENED. AFTER INVESTIGATION, FOUND TO BE 2 SCREWS LOOSE INSIDE THE DOOR HANDLE MECHANISM. SCREWS TIGHTENED SECURED. DOOR CYCLED AND FOUND OPERATIONAL.SDR CA010321008Transceiver · odor(CAN) LEFT HIGH FREQUENCY (HF) RADIO FAILED WHILE TRANSMITTING DURING CRUISE. SHORTLY AFTER BURNING ACRID ELECTRICAL SMELL FILLED COCKPIT. QUICK REFERENCE HANDBOOK ELECTRICAL SMOEK DRILL CARRIED OUT. LEFT HF TURNED OFF, CIRCUIT BREAKERS PULLED, AND UTILITY BUSSDR CA010115008Access Door · damaged(CAN) ON WALK AROUND LEFT HAND WING NR1 SLAT ACTUATING ROD FAIRING PEELED BACK.NEW BRACKET AND DOOR INSTALLED.SDR CA000918011Proximity Switch · faulty(CAN) AIRCRAFT REJECTED TAKEOFF AT 76 KNOTS FOR AN (EICAS) ENGINE INDICATION AND CREW ALERT SYSTEM MESSAGE INDICATION. FOUND LT SLEEVE UNLOCK PROXIMITY SWITCH AT FAULT. REPLACED LT PROXIMITY SWITCH.SDR CA000918010Circuit Board · failed(CAN) REJECTED TAKEOFF AT 80 KNOTS FOR A FIRE/OVERHEAT SYSTEM FAULT. DISPLAYED ON THE (EICAS) ENGINE INDICATION AND CREW ALERT SYSTEM. (CARGO INDICATION) THE A FAULT CARDS WERE SWAPPED, NIL FIX PROBLEM REPEATED. SUSPECT TO BE THE AFT LOGIC TEST CARD. REPLACED SDR CA000530070Window · failed(CAN) DURING CRUISE AT FL 360 FIRST OFFICER WINDOW OUTER PANE FAILED. CREW COMMENTED ARCING ON WINDSCREEN. WINDOW AND CONTROLLER REPLACED.SDR CA000501033Fitting · corroded(CAN) ON HEAVY MAINTENANCE L DRAG STRUT SIDE BRACE FITTING BUSHING FOR SPINDLE PIN FOUND WITH EVIDENCE OF HAVING ROTATED, SEALENT CUT AROUND PERIPHERY OF BUSHING FLANGE. DRAG STRUT BUSHING REMOVED AND HEAVY CORROSION FOUND ON BOTH FLANGE SEAT AND BORE SURFACE SDR CA000501032Fitting · corroded(CAN) ON HEAVY MAINTENANCE LT DRAG STRUT SIDE BRACE FITTING BUSHING FOR SPINDLE PIN FOUND WITH EVIDENCE OF HAVING ROTATED, SEALENT CUT AROUND PERIPHERY OF BUSHING FLANGE. DRAG STRUT BUSHING REMOVED AND HEAVY CORROSION FOUND ON BOTH FLANGE SEAT AND BORE SURFACESDR CA000209043Fitting · leaking(CAN) IDG WARNING LIGHT FLICKER, IDG OIL COOLER FITTING LEAKING OIL.SDR CA000110090Oven · smoke(CAN) DURING TAKEOFF, OVEN IN REAR GALLEY BEGAN TO SMOKE, OVEN DEACTIVATED, OVEN REPLACED.SDR CA991231029Fseu · failed(CAN) AFTER DEPARTURE TRAILING FLAPS FAIL MESSAGE. UNABLE TO GET FLAPS TO RETRACT, A/C RETURNED. FLAPS OPERATED AND FLAPS FAILED TO RETRACT. A/C RTU. FLAPS OPERATED AND FLAPS FAILED ON RETRACTION FROM FULL DOWN WITH MESSAGE TRAILING EDGE FLAPS SHUT DOWN. FLAP SDR CA991103093Transducer · failed(CAN) BOTH HF RADIOS U/S. COULD BE HEARD BUT NOT RECEIVED. LEFT CONTROL PANEL, LEFT COUPLER AND LEFT TRANSDUCER REPLACED.SDR CA991103092Fcu · fluctuated(CAN) ENGINE EXPERIENCED EPR FLUCTUATIONS UP TO 21 EPR. N2 REMAINED STEADY, N1 FLUCTUATED UP TO 5 DEGREES. EEC'S REPLACED INDESCRIMINENTLY, SUBMITTER STATED FAILURE WAS DUE TO FCU TRIM CONTROL MAIN OVERRIDE PX.SDR CA990330068Generator · failed(CAN) DURING CRUISE, RT ENGINE GENERATOR FAULT, CREW DISCONNECTED INTEGRATED DRIVE GENERATOR. A/IRCRAFT RETURNED. RT GENERATOR OFF DISPLAYED, AUX POWER UNIT GENERATOR LIGHT EXITING BUS TIE RESET NORMAL. SNAG REPEAT. REPLACED RT BUS TIE BREAKER, RT INTEGRATSDR CA981216015Switche · failed(CAN) SMOKE IN COCKPIT AFTER RUNWAY TURN OFF LIGHTS SELECTED ON, LIGHTS TURNED OFF AND SMOKE DISSIPATED. BOTH RUNWAY TURN OFF LIGHT SWITCHES REPLACED.SDR CA981030008Actuator · failed(CAN) AILERON LOCK OUT MESSAGE ON ENGINE INDICATING AND CREW ALERT SYSTEM AT 11,500 FEET AT 260 KNOTS. CHECK LIST COMPLETED, MESSAGE DISAPPEARED AT FLAP SELECTION 1 AT 210 KNOTS. CHANGED LEFT AND RIGHT AILERON LOCK-OUT ACTUATORS, SYSTEM SERVICEABLE.SDR CA980827015Wire · missing(CAN) AIRCRAFT WAS UNABLE TO PRESSURIZE DURING CLIMB. FOUND GROUND WIRE MISSING ON PIN 11 OF D1872 COOLING CARD M867, WIRE W506-536-24 NOT CONNECTED TO P5552 CONNECTOR. WIRES INSTALLED.SDR CA980424010Skin · delaminated(CAN) RADOME DELAMINATED DUE TO LIGHTNING STRIKE. REPLACED.SDR CA970624026Actuator · intermittent(CAN) AFTER TAKEOFF UNABLE TO RETRACT NOSE LANDING GEAR. AIRCRAFT RETURNED. UNABLE TO DUPLICATE SNAG DURING GEAR SWING. REPLACED NOSE GEAR LOCK ACTUATORSDR CA960723544Electronic Unit · malfunction(CAN) ON APPROACH LEADING EDGE FLAPS DISAGREE LIGHT ON. FLAP ZERO DEGREE LANDING. REPLACED FLAP SLAT ELECTRONIC UNIT.SDR CA960723540Panel · missing(CAN) ON WALKAROUND FOUND RH WING TRAILING EDGE FALSEWORK PANEL MISSING, 9 FEET BY 1 FOOT.SDR CA960723536Actuator · malfunction(CAN) DURING FLIGHT AILERON LOCKOUT MESAGE ON EICAS. RH AILERON LOCKOUT ACTUATOR REPLACED.SDR CA960424506Flap Lever · adjusted(CAN)TRAILING EDGE FLAP DISAGREE MESSAGE ON EICAS AND TRAILING LIGHT ILLUMINATED INTERMITTENTLY IN ALL PHASES OF FLIGHT AND ALL FLAP SETTINGS. ADJUSTED FLAP LEVER POSITION TOWARD UPPER TOLERANCE BAND.SDR CA960424505Trim Actuator · intermittent(CAN)RUDDER TRIM STUCK LEFT 2 DEGREES, FAILED TO MOVE IN EITHER DIRECTION, AFTER MORE THAN A HALF DOZEN TRIES TRIM STARTED WORKING NORMAL. HAPPENED AGAIN THIS TIME LEFT 3 DEGREES TRIM; AFTER SEVERAL TRIES,BEGAN TO MOVE NORMALLY. REPLACED RUDDER TRIM ACTUATOR.
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