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 = '7372T7' 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 = '7372T7' 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 CA030505003Window · cracked(CAN) F/O,S NR 1 WINDOW OUTER (POSS MIDDLE) PANE CRACKED AT 31000 WINDOW SLOWLY DELAMINATED AND AFTER WE TURNED HEAT OFF WINDOW CRACKED. WINDOW REPALCED AS PER AMM.SDR CA030327003Bearing · failed(CAN) DURING CLIMB IN MANUAL FLIGHT , BEOND 5 DEG. LT WHEEL DEFLECTION AILERONS FELT VERY HEAVY 9 AS IF IN MANUAL REVERSION ) AT THIS POINT IN TIME RUDDER TRIM 0 UNITS AND ADI BALL CENTERED. AILERON TRIM 1/2 UNIT LT IN STABLE CRUISE. AILERON TOWER SHAFT UPPER SDR CA020731013Control Cable · failed(CAN) NR 5 FLAP ACTUATOR ROLLER TRACK DISENGAGED AND WENT THROUGH THE INBOARD SIDE OF NR 5 FLAP FAIRING. NR 5 FLAP TRACK FITTING FOUND DAMAGED (SNAPPED) DUE BOOM CABLE BROKEN. CABLE, TRACK FITTING, PULLEYS, BOOM ASSY, AND CAM FOLLOWER GUARD ADJUSTED AS PERSDR CA020725004Windshield · arced(CAN) FIRST OFFICER NR 1 WINDSHIELD ARCING, UPPER MID SECTION DISCOLOURED BY WIRING LEADS REPLACED WINDSHIELDSDR CA010924006Actuator · failed(CAN) ON DEPARTURE YYZ ATTEMPTED FORWARD HORIZONTAL STAB TRIM USING CONTROL WHEEL SWITCHES. NO FORWARD TRIM AVAILABLE, FULL AFT TRIM OK. AUTO PILOT SEEMED ABLE TO TRIM FORWARD. STABILIZER TRIM MAIN ACTUATOR REPLACED AS PER AIRCRFT MAINTENANCE MANUAL 27-41-71. SDR CA010924004Connector · failed(CAN) ON APPROACH TO YVR NR 2 ENGINE FIRE WARNING INDICATED. BOTH FIRE BOTTLE FIRE DISCHARGED. FIRE WARNING REMAINED ILLUMINATED. NO EXTERNAL EVIDENCE OF FIRE ON LANDING YVR. FOUND CONNECTOR D1098 SHORTING INTERNALLY. REPLACED CONNECTOR 5256.SDR CA010910009Seal · leaking(CAN) NR 2 LOW OIL PRESSURE FLICKERING FOR THE LAST 4 MINUTES OF FLIGHT WITH THE PRESSURE GAUGE IN AND OUT OF CAUTION RANGE. TEMPERATURE NORMAL, ENGINE OPERATED AT REDUCED THRUST AND SHUTDOWN AFTER LANDING. FOUND TO BE THE STARTER DRIVE PAD CARBON SEAL TO BESDR CA010910008Relay · failed(CAN) DURING SRVICE CHECK, WITH NO A/C POWER & BATTERY SELECTED TO DC, THE AMP METER WENT TO 40 AMPS, AFTER APU START, THE D.C. AMPS METER STOCKED AT 100 AMPS. FOUND HIGH RESISTANCE BETWEEN TERMINAL B2 AND A2 OF R1 BATTERY BUS RELAY, WHEN RESISTANCE SHOULSDR CA000110017Fitting · damaged(CAN) REMOVED FITTING FOR BEARING REWORK AND FOUND HIDDEN DAMAGE. THREE OF FOUR BOLTS FROZEN IN BORES, TWO BOLTS SHEARED, EVIDENCE OF EXTENSIVE CORROSION TO SHEAR FACE. FWD INBD BOLT CUT FOR REMOVAL. FITTING REPLACED.SDR CA000110016Window Post · cracked(CAN) INSP REVEALED CRACKS OF C-D WINDOW POST UPPER OTBD CORNERS OF LT AND RT WINDOWS. ROUTED OUT TO REVEAL UNDER SKIN ALSO CRACKED FROM SITE MARKS. REPAIRED PER BOEING TELEX.SDR CA990416013Trunnion · damaged(CAN) FOUND MLG OUTER TRUNNION ATTACHMENT LINK SHEARED. GEAR REPLACED.SDR CA990416007Pcu · failed(CAN) PILOT REPORTED VIBRATION THROUGHOUT THE AIRCRAFT WITH B-PUMPS ON. RUDDER OBSERVED TO OSCILLATE 1 TO 1.5 INCH RANGE, RUDDER FUNCTIONED, VIBRATION QUIT. RUDDER PCU REPLACED.SDR CA990330008Tire · failed(CAN) NR 4 TIRE TREAD SEPARATED AND FRAGMENTS DAMAGED. THE RIGHT INBOARD FLAP, REPLACED.SDR CA990310057Frame · corroded(CAN) DURING INSPECTION OF FUSELAGE DENT, THE FORWARD LEFT LAVATORY WAS REMOVED FOR ACCESS. THE CHORD AT STA 245 AND STA 260 FOUND CORRODED, REPLACED.SDR CA980317039Valve · dirty(CAN) AT TAKEOFF, PRESSURIZATION SYSTEM AUTO FAIL LIGHT CAME ON. THROUGH 5,000 FEET, RESET SYSTEM AND OPERATED NORMALLY FOR REST OF FLIGHT. OUTFLOW VALVE REPLACED.SDR CA971113019Hose Assembly · ruptured(CAN) AIRCRAFT DIVERTED DUE TO EXCESSIVE LEAKAGE IN CREW OXYGEN SYSTEM. HOSE RUPTURED. REPLACED.SDR CA970922016Csd · failed(CAN) CLIMBING THROUGH 8000 FEET, THE NR2 GENERATOR "HIGH OIL TEMPERATURE LIGHT" CAME ON. COMPLETED CHECK LIST AND SHUTDOWN CONSTANT SPEED DRIVE (CSD) AND STARTED APU. JUST LEVELING OFF AT 31,000 FEET WHEN APU "HIGH OIL TEMPERATURE" AND "LOW OIL PRESSURE" LIGHSDR CA970904011Strobe · burnt(CAN) AIRCRAFT DIVERTED DUE TO SMOKE IN CABIN. UPPER ANTI COLLISION BEACON BURNT OUT. CIRCUIT BREAKER PULLED AND COLLARED. TERMINAL STRIP CHECKED FOR ARCING.SDR CA961216002Detector · damaged(CAN) ON CLIMB #2 ENGINE FIRE WARNING, AIRCRAFT RETURNED, FIRE WARNING STAYED ON FOR SEVERAL SECONDS, ENGINE SHUT DOWN AND FIRE BOTTLE FIRED. CONDITION REMAINED THE SAME WITH FIRE WARNING INTERMITTENT. FIRE SENSING ELEMENT DAMAGED, REPLACED.SDR CA960925005Gyro · jamming(CAN) F/OS A.D.I. HORIZON CARD KEEPS JAMMING. VG CHANGED AND RESET OF C/B HAD NO EFFECT. F/OS A.D.I. AND GYRO REPLACED. #2 VG TRANSFER RELAY REPLACED AS PER MAINTENANCE REQUEST.SDR CA960723003Structure · damaged(CAN) AIRCRAFT DECLARED AN EMERGENCY AND DIVERTED. EXTENSIVE DAMAGE TO LEADING EDGES, HORIZONTAL STAB, VERTICAL STAB, RADOME, #1 WINDSHIELD CRACKED. ALL SLATS REPAIRED OR REPLACED. UPPER ANTI COLLISION LIGHT DAMAGED.SDR CA960625001Seal · leaking(CAN) AIRCRAFT DIVERTED DUE TO LOSS OF HYDRAULIC FLUID. ATTENUATOR SEAL REPLACED.SDR CA960604016Seal · leaking(CAN) AFTER TAKEOFF WITH THE LANDING GEAR AND FLAPS UP, THE HYDRAULIC QUANTITY WAS 3.0 GALLONS. ONE HOUR INTO FLIGHT HYDRAULIC QUANTITY WAS 1.8 GALLONS. SEVENTEEN MINUTES LATER QUANTITY WAS 1.5. QUANTITY DROPPED 1.4 GALLONS IN 10 MINUTES. AIRCRAFT DIVERTED. ON
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