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 = 'SF340A' 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 = 'SF340A' 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 CHQA20000037Power Supply · dischargedCREW REPORTED THE EMERGENCY LIGHTS CAME ON WHEN IN GROUND POSITION AND WERE VERY DIM. MAINTENANCE REPLACED THE BATTERY POWER SUPPLIES, GROUND TESTED NORMAL.SDR CHQA20000036Connector · dirtyFLIGHT CREW RETURNED TO THE FIELD AFTER THE RIGHT ENGINE TORQUE STARTED TO FLUCTUATE. MAINTENANCE INSPECTED THE SYSTEM, CLEANED THE ECU CANNON PLUGS, GROUND RAN WITH NO FLUCTUATIONS NOTED.SDR AU000922Warning System · faulty(AUS) GROUND PROXIMITY WARNING SYSTEM (GPWS) FALSE WARNING. INVESTIGATION COULD FIND NO FAULTS.SDR CHQA20000035Swivel · shearedFLIGHT CREW REPORTED THAT ALL HYDRAULIC PRESSURE WAS LOST AND HAD TO PUMP DOWN THE LANDING GEAR. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE BRAKE LINE SWIVEL HAD SHEARED ON THE RIGHT MLG. THE SWIVEL WAS REPLACED, GEAR SWUNG WITH ALL INDICATIONSSDR CHQA20000034Fuel Cap · missingFLIGHT CREW RETURNED TO THE FIELD AFTER THE PILOT NOTICED THE FUEL CAP DOOR FLAPING IN FLIGHT. MAINTENANCE INSPECTED THE DOOR, INSTALLED A NEW FUEL CAP, CLOSED THE DOOR, NO DEFECTS NOTED.SDR CHQA20000033Battery · dischargedFLIGHT CREW REPORTED THE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE FOUND THE BATTERIES HAD BEEN LEFT ON. THE BATTERIES WERE REPLACED, SYSTEM OPS CHECKED NORMAL.SDR AU000868Ecu · faulty(AUS) LT ENGINE ELECTRICAL CONTROL UNIT FAULTY.SDR AU000918Blade · split(AUS) RT PROPELLER NR 1 BLADE TRAILING EDGE SPLIT FROM THE BLADE TIP. LENGTH OF SPLIT 355.6MM (14IN).SDR CHQA20000031Gcu · failedFLIGHT CREW RETURNED TO THE FIELD AFTER THE RIGHT ENGINE GENERATOR FELL OFF LINE. MAINTENANCE REPLACED THE GENERATOR CONTROL UNIT, GROUND RAN, OPS CHECKED NORMAL.SDR AU000834Harness · shorted(AUS) RT LANDING GEAR EMERGENCY EXTENSION ELECTRICAL HARNESS OPEN CIRCUITED. INVESTIGATION FOUND A BROKEN WIRE IN THE HARNESS.SDR MALA000553Power Unit · failedGPU DROPPED VOLTAGE TO 15 VOLTS DURING START OF RT ENGINE. MOTORED RIGHT ENGINE FOR APPROXIMATELY 15 SECONDS AND DIGITAL AND ANALOGUE ITT WERE NOT INDICATING TO TEMPERATURE. RELEASED STARTER, AND SAW DIGITAL ITT INDICATED OF 950 FOR 1-2 SECONDS, CONTINUED TOSDR REXA00012Smoke · detectedAFTER TAKEOFF, PILOT REPORTED THERE WAS SMOKE SMELL THROUGHOUT THE CABIN AND COCKPIT. AFTER IN-DEPTH VISUAL INSPECTION, THE AIRCRAFT WAS GROUND RUN FOR 20 MINUTES CHECKING NUMEROUS AVIONICS COMPONENTS, RECIRCULATION FANS, AND AIR CONDITIONING COMPONENTS, WITHSDR REXA00011Packing · deterioratedLEFT ENGINE OIL PRESSURE DECREASED TO THE RED ARCH WITH A CENTRAL WARNING PANEL LIGHT. CREW FOLLOWED CHECKLIST AND SHUT ENGINE DOWN. FOUND OIL LOSS DUE TO C-SUMP COVER O-RING LEAK. C/W GE SB 79-19 BY REPLACING THE POWER TURBINE STRUT AND C-SUMP COVER O-RINGSDR AU000653Relay · faulty(AUS) AUTO-COARSEN SYSTEM FAILED. INVESTIGATION FOUND AN INTERMITTENT RELAY.SDR MALA000541Downlock Switch · failedNOSE GEAR WOULD NOT INDICATE DOWN AND LOCKED WHEN THE GEAR HANDLE WAS SELECTED DOWN, ON THIRD ATTEMPT GEAR SELECTED DOWN AND LOCKED. MAINTENANCE INSPECTED NOSE GEAR BAY AND GEAR ASSEMBLY FOUND NO DEFECTS. AC FERRIED FROM EAU TO MSP FOR FURTHER EVALUATION. MSDR CHQA20000029Bolt · shearedFLIGHT CREW RETURNED TO THE FIELD AFTER THE LANDING GEAR WOULD NOT RETRACT. MAINTENANCE FOUND THE LOWER BOLT HOLDING THE RETRACT ACTUACTOR BRACKET SHEARED, AND THE BRACKET BENT. THE BOLT AND BRACKET WERE REPLACED, GEAR SWUNG, WITH ALL INDICATIONS NORMAL.SDR PLGA000827Chip Detector · malfunctionedFLT 4655 - BOS-YOW - THE RIGHT ENGINE CHIP LIGHT ILLUMINATED. FOLLOWING THEIR CHECKLIST, THE CREW DIVERTED TO BGR AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE RIGHT ENGINE CHIP DETECTOR AND FOUND NO EVIDENCE OF METAL CONTAMINATION. THE FAULTY CHIPSDR AU000754Fitting · corroded(AUS) LANDING GEAR SUPPORT FITTINGS CORRODED IN BEARING BORES AND LINK ATTACHMENT HOLES. DEPTH OF CORROSION BETWEEN 0.152MM AND 1.092MM(0.006IN AND 0.043IN).SDR MALA000539Indicator · malfunctionedLEFT ENGINE OVERTEMP LIGHT ILLUMINATED ON TAKEOFF. MAINTENANCE VERIFIED OVERTEMP LIGHT COMING ON EARLY USING TT1000A TEST BOX. REMOVED ITT INDICATOR PN523347, INSTALLED SERVICABLE TEMP INDICATOR. ITT INDICATOR AND OVERTEMP LIGHT OP CHECK GOOD.SDR MALA000534Frame · corrodedFWD CABIN FRAME AND ANGLE CORRODED AT STA 258. COMPLETED PERMANENT REPAIR IAW E053071.SDR MALA000519Wire · brokenAFTER T/O IN HEAVY PRECIP, RIGHT TAILPIPE HOT WENT ON FOR 1 MINUTE, EXTINGUISHED WHEN RIGHT POWER LEVER WAS REDUCED. MAINTENANCE FOUND O/B SENSOR CANNON PLUG WIRE BROKE. REPAIRED WIRE, OPS CHECK GOOD.SDR PLGA000815Wheel · damagedLGA - FLT 4604 - AFTER LANDING, THE LEFT INBOARD TIRE WAS FOUND TO BE FLAT. MAINTENANCE INSPECTED THE WHEEL AND FOUND THE INBOARD WHEEL HALF FLANGE HAD CRACKED AND A SECTION 0(APPROX .75 BY 6 INCHES LONG) WAS MISSING. THE DAMAGED WHEEL ALSO CAUSED DAMAGE TO SDR REXA00015Engine · leakingCOCKPIT FILLED WITH SMOKE AND STROND ODOR. REMOVED AND REPLACED RIGHT ENGINE IAW 71-10-00-4, DUE TO OIL LEAK AT INLET FRAME. THIS WAS THE CAUSE AND TERMINATING ACTION OF SMOKE AND ODORS NOTED IN PREVIOUS SDR 00-013, AND SDR 00-014. (M)SDR MALA000504Structure · bird strikeON DEPARTURE, CREW REPORTED BIRD STRIKE OUTBOUND MSP, DUE TO MAINTENANCE AVAILIBILITY AT OUTSTATION CREW DID A AIR TURNBACK TO MSP. NO EVIDENCE OF BIRD STRIKE WAS FOUND. MAINTENANCE PERFORMED A COMPLETE INSPECTION OF ENTIRE EXTERIOR OF AC, NO BIRD STRIKE EVISDR REXA00007Panel · corrodedDURING REFURB OF PAINT, SEVERE CORROSION WAS NOTED ON VARIOUS PANELS THROUGHOUT THE FUSELAGE. AFTER CLOSER INVESTIGATION, THE CORROSION WAS FOUND TO BE BEYOND ALLOWABLE LIMITS. REPAIRED AND REPLACED VARIOUS FUSELAGE PANELS. (M)SDR MALA000503Sump · fluctuatesAFTER TAKEOFF, RT ENG OIL PRESS LIGHT, TRIPLE CHIMES WENT OFF AND IMMEDIATELY OUT. RT ENG PSI WAS BOUNCING BETWEEN 40-50 PSI ALL THE WAY THROUGH CLIMBOUT. MAINTENANCE REPACK RT ENG C-SUMP IAW SAAB 340 7920-301 RT ENG GAUGE OIL PSI. RAN AC, OPS CHECK GOOD.SDR CHQA20000021Shutoff Valve · dirtyAIR VALVE LIGHT ILLUMINATED IN FLIGHT, ICING CONDITIONS REPORTED, SO FLIGHT CREW RETURNED TO THE FIELD. THE GARRETT VALVE WAS CLEANED AND THE CANNON PLUG RE-SECURED. GROUND RUNS INDICATED ALL SYSTEMS OPERATING NORMALLY.SDR PLGA000729Relay · failedBGR - FLT 4662 - BOS-YHZ, DURING FLIGHT, THE LEFT MAIN BUSS LIGHT ILLUMINATED IN FLIGHT. THE AIRCRAFT DIVERTED INTO BGR AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT BUSS RELAY 67PC TO BE AT FAULT. AFTER REPLACING THE RELAY, AND PERFORMING ALL REQSDR MALA000450Swivel · failedAFTER TAKEOFF, LOST HYDRAULIC FLUID AS PER ORH APPLIED HYD LOSS PROCEDURE, EMERGENCY GEAR EXTENDED WAS SUCESSFUL. AIR TURNBACK, AC LANDED NORMALLY. MAINTENANCE REPLACED LT BRAKE SWIVEL, AND RESET EMERGENCY GEAR SYSTEM. SERVICED HYD SYSTEM, ALL CHECK GOOD.SDR MALA000449Cooler · failedAFTER TO NOTICED LT ENGINE OIL TEMP EXCEEDED RED LINE TEMP, ITT TEMP ON LT WAS OVER 60C SPLIT FROM RIGHT SIDE. MAINTENANCE DRAINED AND REPLENISHED POWER UNIT OIL SYSTEM, REPLACED OIL COOLER P/N 5034T31P02, COMPLETED GPA RUNS LT/RT ENGINE. MARGIN CHECKS GOOD SDR MALA000444Resistor · failedFUNCTIONAL TEST OF RT ENGINE FIRE BOTTLE, HAD NO VOLTAGE AT 10WB-PL-A&B, AND 10WBP2-A&B. MAINTENANCE FOUND RESISTORS 5WB AND 7WB OPEN. REPLACED RESISTORS, OPS CHECK GOOD.SDR CHQA20000018Bearing · seizedRIGHT NOSE TIRE DEPARTED AIRCRAFT ON TAKEOFF. AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND WHEN THE TIRE DEPARTED CAME IN CONTACT WITH THE RIGHT MAIN GEAR BRAKE LINE, BRAKING THE LINE. THE WHEEL WASDR MALA000447Transmitter · failedLT PROP OIL PRESSURE FLUCUATES. AIR RETURN TO DTW. MAINTENANCE REPLACED LG PGD OIL TRANSMITTER. OPS CHECK GOOD.SDR CHQA20000017Connector · dirtyENGINE TORQUE FLUX AFTER TAKEOFF. MAINTENANCE CLEANED CANNON PLUGS ON THE CTOT AND ECU, GROUND RAN, ALL INDICATIONS NORMAL. RETURNED AIRCRAFT TO SERVICE.SDR CHQA20000016Clamp · looseENGINE OVERTEMP INDICATION ILLUMINATED AFTER TAKEOFF AND THE ENGINE WAS SHUTDOWN. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE HP BLEED LINE CLAMP HAD COME OFF AND DISCONNECTED THE BLEED LINE. THE CLAMP WAS REPLACED, LINE REATTACHED, ENGINE GROUND RAN WISDR CHQA20000015Indicator · fluctuatesENGINE TORQUE FLUX AFTER TAKEOFF. MAINTENANCE REMOVED AND REPLACED THE CTOT PANEL, GROUND RAN WITH NO FLUCTUATIONS NOTED. AIRCRAFT RETURNED TO SERVICE.SDR MALA000442Smoke Detector · malfunctionedON TAXI OUT, CREW GOT A CARGO SMOKE LIGHT. BLEW BOTTLE AND RETURNED TO GATE. MAINTENANCE REPLACED THE CARGO SMOKE DETECTOR (AFT). OPS CHECKED GOOD.SDR AU000614Relay · burned(AUS) AFTER TAKE-OFF WHEN ANTI-ICE WAS SELECTED 'ON', THE RH ENGINE INTAKE CAUTION LIGHT ILLUMINATED. GROUND INVESTIGATION FOUND THE RELAY WHICH CONTROLS AC POWER TO THE ELECTRICALLY HEATED ENGINE INTAKE DUCT IN A BURNT CONDITION. IN ADDITION, THE CONTACTS ASDR CHQA20000011Swivel · brokenRETURNED TO THE FIELD AFTER LOST HYDRAULIC PRESSURE. CREW PUMPED GEAR DOWN. MAINTENANCE FOUND HYDRAULIC SWIVEL ON RT MAIN GEAR UPPER STRUT BROKEN. THE SWIVEL WAS REPLACED, SYSTEM SERVICED, GEAR SWUNG WITH ALL INDICTIONS NORMAL.SDR CHQA20000010Switch · dirtyLANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO THE FIELD. MAINTENANCE CLEANED THE CANNON PLUGS ON THE WEIGHT ON WHEELS SWITCH, TEST FLEW AIRCRAFT WITH ALL INDICATIONS NORMAL.SDR CHQA20000008Engine · lowLEFT ENGINE OIL PRESSURE FLUCUATION WITH A LOW OIL PRESSURE WARNING FLICKERING. AIRCRAFT DIVERTED TO PIT AND LANDED WITH OUT INCIDENT. MAINTENANCE INSPECTED THE ENGINE, SERVICED WITH 3 QTS OF OIL, GROUND RAN WITH NO PROBLEMS NOTED.SDR CHQA20000007Smoke Detector · defectiveCARGO SMOKE LIGHT AFTER TAKEOFF. THE CARGO COMPARTMENT BOTTLE WAS DISCHARGED AND THE AIRCRAFT RETURNED TO THE FIELD. AIRCRAFT WAS INSPECTED, NO SMOKE OBSERVED, THE SYSTEM DEFERRED AND THE AIRCRAFT RETURNED TO SERVICE. THE SMOKE DETECTOR, FIRE BOTTLE AND SQUSDR CHQA20000006Switch · false activationFLIGHT CREW RETURNED TO THE FIELD AFTER RECEIVING A CARGO DOOR LIGHT INDICATION. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE DOOR WAS INSPECTED, FOUND TO BE CLOSED, THE SYSTEM DEFERRED AND AIRCRAFT RETURNED TO SERVICE. MAINTENANCE INSPECTED THE SYSTEM FOUND ASDR MALA000424Warning Light · false indicationCARGO SMOKE LIGHT ILLUMINATED. DIVERTED FLIGHT TO RHI. LIGHT WAS ON MOMENTARILY. CREW DECIDED TO USE EXTINGUISHING SYSTEM. MAINTENANCE REPLACED CARGO EXTINGUISHER FIRE BOTTLE.SDR MALA000383Hmu · failedAFTER T/O ABOUT 450 - 500 AGL, CTOT DIALED DOWN AND WENT TO REDUCE POWER TO CLIMB POWER, GOT FOUR LOUD COMPRESSOR STALLS ON RT ENGINE. PERFORMED MEMORY, TEMS, AND QRH. MAINTENANCE COMPLETED BORESCOPE PER GE7200. NO DISCREPANCIES NOTED. REPLACED HMU. OPS CSDR MALA000380Switch · failedRIGHT IGNITION LIGHT CAME ON AFTER T/O. LIGHT WOULD NOT GO OUT, BUT WENT BACK AFTER LANDING. MAINTENANCE REPLACED PRESS SWITCH, CHOCK ENGINE AT ALL PARAMETERS. NO DEFECTS NOTED.SDR MALA000375Downlock Switch · failedWHEN LANDING GEAR WAS EXTENDED THREE GREEN LIGHTS ILLUMINATED AND AMBER INTRANSIT LIGHT STAYED ON, LH BATTERY VENT CB WAS FOUND POPPED (K-2). WHEN BREAKER WAS RESET, AMBER LIGHT WENT OUT INFLIGHT. AFTER SHUTTING DOWN AT GATE AMBER INTRANSIT LIGHT CAME ON AGAISDR CHQA20000002Engine · malfunctionedFLIGHT CREW RETURNED TO THE FIELD AFTER THE RIGHT ENGINE TORQUE STARTED TO FLUX AFTER TAKEOFF AND HAD A COMPRESSOR STALL. MAINTENANCE INSPECTED THE AIRCRAFT, PERFORMED ENGINE GROUND RUNS AND COULD NOT DUPLICATE THE PROBLEM. THE AIRCRAFT WAS RETURNED TO SERVISDR CHQA20000001O-Ring · brokenFLIGHT CREW REPORTED THAT THE LEFT ENGINE OIL PRESSURE DROPPED AND OIL CAPTION LIGHT ILLUMINATED AFTER TAKEOFF. THE ENGINE WAS SHUTDOWN AND RETURNED TO THE FIELD. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE O-RING ON THE OIL FLAPPER VALVE IN THE OIL SERSDR AU000496Switch · damaged(AUS) LT ENGINE AUTO COARSEN P3 SWITCH HAD HIGH RESISTANCE ACROSS THE CONTACTS.
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