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 1409061Warning Light · illuminatedON 11/29/03, FLT 4624 CMH-PIT, AIRCRAFT N104CQ RETURNED TO GATE. PRIOR TO TAKEOFF WITH POWER LEVERS JUST ABOVE FLIGHT IDLE NR 2 ENGINE SUDDENLY MADE A LOUD ROARING SOUND AND ENGINE OVERTEMP LIGHT ILLUMINATED. AFTER MOVING NR 2 CONDITION LEVER TO FEATHER ENGINESDR 038431Control Column · vibrationDURING CLIMB OUT AND CRUISE FLT 4514 FROM PIT TO LYH EXPERIENCED ABNORMAL RAPID VIBRATION IN CONTROL YOKES. CREW WAS ADVISED TO RETURN TO PIT, NO INCIDENT.SDR 008181Connector · damagedAIRCRAFT ABORTED TAKEOFF WHEN ERRATIC TORQUE INDICATIONS WERE OBSERVED ON THE NR 2 ENGINE. ENGINE TORQUE INDICATION WAS FLUCTUATING FROM 50 TO 120 WITH CTOT ENGAGED. AT 1350Z, FWA MX REPORTED OF TIGHTENING A LOOSE BACKSHELL ON A ECU CONNECTOR. THE AIRCRAFT WSDR AUS20031219Engine · malfunctioned(AUS) DURING TAKEOFF RT ENGINE POWER WOULD NOT INCREASE TO TAKEOFF SETTINGS. THE RT ENGINE INDICATIONS REMAINED AT 85 PERCENT TO 90 PERCENT TORQUE AND THE RT PROPELLER WAS REPORTED TO REDUCE TO 1100 RPM. ENGINE GROUND RUNS AND FUNCTIONAL CHECKS COULD NOT CONFSDR 013042Yoke · vibrationON CLIMBOUT, A STRONG (FWD-AFT) VIBRATION WAS FELT ON THE CAPTAIN YOKE. CREW LEVELED OFF AT 2000 FT, VIBRATION CONTINUED FROM 150-200 KTS. CREW REDUCED SPEED TO 180 KTS, RETURNED TO FIELD WITH VIBRATION CONTINUING UNTIL FLAPS RETRACTED.SDR 009081Warning Light · illuminatedFLT 4528 FROM PIT TO HGR AFTER T/O ON GEAR RETRACT, FI STOP OPEN LIGHT ILLUM. CREW WAS ADVISED TO RETURN TO FIELD. AC RETURNED TO FIELD WITH NO INCIDENT.SDR MALA030505Warning System · false indicationAFTER START ON FLIGHT 3093, CREW REPORTED FIRE IN RT ENGINE. CREW TURNED ON THE HIGH PRESSURE BLEED THE ENGINE TEMP WAS 800, HP FELL OFF LINE, AND NG STARTED TO DROP TO 30 PERCENT, TEMP WENT TO 840 PROP STAYED AT 1040. CREW RECEIVED THE FIRE SIGNAL AND DID FSDR 34931Warning Light · illuminatedFLIGHT NR 4555 FROM FWA TO PIT. ON TAKE-OFF AIRCREW NOTICED THAT THE AUTOCOARSEN LIGHT FAILED TO ILLUMINATE (ARM). AIRCREW ABORTED TAKE-OFF AND RETURNED TO THE GATE.SDR MALA030504Detector · failedDURING FLT, YELLOW HEADING FLAG REPEATEDLY CAME ON, COULD BE FAILURE ON BOTH SIDES. AIR RETURN TO MSP. MAINTENANCE REPLACED NR 2 FLUX DETECTOR UNIT P/N 622-5812-001, S/N ON 29146, S/N OFF 10863. PERFORMED COMPASS SWING PROCEDURE IAW 34-21-00, ALL CHECKS GOOSDR 206571Panel · malfunctionedFLT NR 4645 FROM PIT TO SDF. ON TAKE-OFF, AIRCREW NOTICED CTOT DID NOT ARM. AIRCRAFT RETURNED TO GATE.SDR 206541Aileron · malfunctionedFLT NR 4568 FROM LYH TO PIT. ON TAKE-OFF, AFTER PASSING CONTROL OF AIRCRAFT FROM CAPTAIN TO FIRST OFFICER. AIRCREW EXPERIENCED GRINDING IN AILERONS. AIRCREW ABORTED TAKE-OFF AND RETURNED TO GATE.SDR 038463Engine · malfunctionedDURING TAKEOFF ROLL CREW NOTICED THAT LT ENGINE OIL PRESSURE AND TEMPERATURE BOTH INDICATED ZERO. CREW ABORTED T/O AND RETURNED TO GATE IN ERI. A/C TAKEN OUT OF SERVICE 11-20-03 AT 0835 (LT).SDR 037181Pump · failedDURING CLIMBOUT FROM YIP WITH HYDRAULIC PUMP FAILED WHILE IN OVERRIDE, IN OVERRIDE DUE TO HYD PUMP AUTO MODE MEL. GEAR WAS NOTED UP AND LOCKED WITH THE GEAR TRANSIT LIGHT STILL ILLUMINATED. CREW CYCLED PUMP SWITCH AND C/B. THE PUMP WAS STILL INOPERATIVE. TSDR CA031118003Casting · broken(CAN) AFTER LANDING, THE AIRCRAFT FELT A SHIMMY VIBRATION. AT THE GATE THE PILOT NOTICED A BROKEN PIECE MISSING OFF THE NOSE STEERING COLLAR YOKE ASSY. AFTER INVESTIGATION THE PART INSTALLED IS PRE SB32-099 WHICH CALLS FOR REGULAR INSPECTION DUE TO THAT SAME SDR 012071Engine · malfunctioned11/17/03 1715 (UTC) FLIGHT 4645 PIT-SDF. CREW REPORTED AN UNCOMMANDED POWER INCREASE OF THE LT ENGINE DURING CLIMB OUT. CREW REPORTED A RISE IN TQ AND ITT. CREW THEN FOLLOWED QRH, ENTERED TORQUE MOTOR LOCKOUT. ENGINE PARAMETERS NORMAL. AIRCRAFT RETURNED TO PITSDR 038191Control Column · vibrationSHORTLY AFTER TAKEOFF CREW EXPERIENCED SEVERE FLIGHT CONTROL VIBRATION PRIMARILY IN THE PITCH AXIS AND SOME IN ROLL, A MECHANIC WAS IN THE JUMPSEAT AND COMFIRMS THE YOKES WERE VIOLENTLY VIBRATING. CAPT REPORTED IT FELT LIKE HE WAS FIGHTING THE AUTOPILOT. AUTSDR 037023Connector · disconnectedMX CHECK FLIGHT 9404 A/C PERFORMING MX CHECK FLIGHT DUE TO LEVEL C MX INSPECTION LAN-LAN. RIGHT AFTER TAKEOFF LT ENGINE OIL TEMP, ITT, AND NG ALL PEGGED OUT THE ENGINE OVERTEMP LIGHT ILLUMINATED. CREW SHUT DOWN THE ENGINE AND DECLARED AN EMERGENCY. A/C TAKESDR 038181Connector · looseDURING CLIMBOUT ON FLT 9404, L ENG OVER TEMP LIGHT ILLUM, L END NG WENT TO 0, L ENG ITT PEGGED AT MAX, ENGINE WAS SHUT DOWN AND EMERGENCY DECLARED, AIRCRAFT RETURNED TO BLOCK WITH NO INCIDENT. FOUND ELECTRICAL CONNECTOR P4 LOOSE IN LT NACELLE, RESECURED CANNSDR 034691Bleed Valve · failedFLIGHT NR 8960 FROM PIT TO CLE. IN ROUTE, AIRCREW RECEIVED THE LT AIR VALVE LIGHT, LIGHT WAS ON AND STEADY. AIRCREW RETURNED TO PIT. WHEN MAINT. GOT TO THE A/C THEY FOUND THE LT ANTI-ICE START BLEED VALVE WAS BAD. REMOVED AND REPLACED VALVE A/C RETURNED TO SSDR 038161Warning Light · illuminatedFLIGHT 4593 PIT-TOL. DURING FLIGHT, THE RT AIR VALVE WARNING LIGHT ILLUMINATED. THE CREW FOLLOWED THE QRH AND RETARDED THE RT POWER LEVER AND THE WARNING LIGHT WENT OUT. AC RETURNED TO PIT AND TAKEN OUT OF SERVICE 11-11-03 AT 1655 (LT).SDR CA031113013Bearing Race · broken(CAN) AIRCRAFT ON LANDING FELT A VERY STRONG SHIMMY AT THE NOSE, THE PILOTS DID THEIR INVESTIGATION AND ONE OF THE NOSE WHEEL BEARINGS WAS COMPLETELY BROKEN AND THE WHEEL WAS LOOSE ON THE AXLE. TECHNICIAN WAS SENT TO REPLACE BOTH NWA'S. AFTER INVESTIGATION, LSDR 203121Warning Light · illuminatedON TAKEOFF AIRCREW RECEIVED TAILPIPE HOT LIGHTS FOR BOTH ENGINES. PILOT FOLLOWED QRH AND RETURNED TO PIT.SDR MALA030486Computer · malfunctionedDURING FLIGHT 3141, WHILE IN CRUISE, CAPT EADI & EHSI BOTH WENT DARK. RECEIVED A DCP FLAG. RAN QRH WENT TO DRIVE XFER. SCREENS CAME BACK ON. MAINTENANCE REMOVED AND REPLACED NR 1 DPU ALL CHECKS GOOD IAW SAAB MM CH 34. P/N 622-7713-004, S/N OFF 5248, S/N OSDR CA031104001Bolt · broken(CAN) THE PILOT REPORTED A RUDDER TRAVEL PROBLEM AND TEMPORARY STIFFNESS AT END OF TRAVEL. AFTER INVESTIGATION FROM MAINTENANCE, FOUND LEFT RUDDER STOP PAD ATTACHING BOLT CAME LOOSE AND BROKE. AREA INSPECTED AND BOLT REPLACED. REFERENCE IPC 55-50-00-02 ITEM 53SDR 29341Warning Light · illuminatedFLIGHT 4554 FROM PIT TO FWA, AFTER TAKEOFF AT 1000 FT, AIRCREW GOT A LT OIL PRESSURE LIGHT. A/C RETURNED SAFETY BACK TO PIT.SDR 202201Wire · damagedFLIGHT NR 4585 FROM PIT TO IPT. A/C WAS FLYING TO IPT WHEN AIRCREW NOTICE RT PROP OIL PRESSURE GAUGE WOULD FLUCTUATE INTERMITTENTLY FROM 80 TO 5 PSI. MAINTENANCE REPAIRED INSULATION ON WIRE TO PROP OIL PRESSURE TRANSDUCER. GROUND RAN A/C AND RETURNED TO SERVISDR MALA030474Battery Pack · dischargedSEVERAL CABIN EMERGENCY LIGHTS WOULD NOT COME ONLINE. MAINTENANCE REPLACED 22LN AND 24LN BATTERY PACKS PN 61-0478-9 SN/OFF ELB085, SN/ON ELB502, POWER SUPPLY PN 60-1321-1, SN/OFF 18246 SN/ON 14582. OPS CHECKS GOOD.SDR MALA030472Actuator · failedDURING FLIGHT NR 2790 RUDDER LIMITER OVER RIDE C/B TRIPPING INFLIGHT. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED RUDDER LIMITER OVERIDE ACTUATOR IAW SF340 MM 27-21-60 PN OFF 8618M2 SN/OFF 106374A PN/ON 8377M7 SN/ON M169 ALL OPS CHECKS GOOD.SDR 025291Warning Light · illuminatedFLT 4571 IN ROUTE FROM PIT TO LYH EXPERIENCED A STBY PITCH TRIM LIGHT IN FLT, CAPTAIN RETURNED TO PIT.SDR 025251Thermister · failedFLIGHT 4556 PIT-FWA. DURING CLIMBOUT AT APPROXIMATELY 5000 FT, THE RT ENGINE INTAKE HEAT WARNING LIGHT ILLUMINATED. A/C RETURNED TO PIT. A/C TAKEN OUT OF SERVICE 10-14-03 AT 1750 (LT). PIT MX SWAPPED TO A SPARE THERMISTOR ON THE RT INTAKE HEAT SYSTEM AND SSDR 150094Engine · malfunctionedFLIGHT 4580 BED-TTN. DURING TAKEOFF ROLL AFTER CTOT WAS ENGAGED THE CREW FELT THE RT ENGINE SURGE AND NOTICED THE RT TORQUE INDICATION WAS AT 120 PERCENT. THE CREW IMMEDIATELY RETARDED THE POWER LEVERS AND ABORTED THE TAKEOFF. TORQUE WAS AT 120 PERCENT FOR SDR MALA030452Control Rod · contaminatedDURING FLIGHT NR 2733, INFLIGHT BOTH POWER LEVERS EXTREMELY DIFFICULT TO MOVE. CONDITION LEVERS OK. POWER LEVERS SUPPOSELY STICKING CONSIDERABLY, EVEN WITH FRICTION LEVER OFF. MAINTENANCE CLEANED CONTAMINANTS OFF OF POWER LEVER AND CONDITION LEVER CONTROL RSDR 154931Autocoarsen Sys · will not armON 10/03/03 AT APPROX. 1040Z, FLT 4597 TOL-PIT, AIRCRAFT N43SZ ABORTED TAKEOFF FOR THE AUTOCOARSEN SYSTEM DID NOT ARM.SDR MALA030441Skin · dentedRT FORWARD EMERGENCY EXIT DOOR OUTER SKIN HAS SMALL DENT AFT OF LOWER RELEASE HANDLE THAT FAILED BOND MASTER INSPECTION. MAINTENANCE REPAIRED IAW EO S52028. A/C RELEASE DATE 10/2/03.SDR 155541Indicator · failedFLIGHT NR 4586 FROM PIT TO IPT. AFTER 15 MINUTES OF FLIGHT. THE LT SIDE TORQUE INDICATOR WENT TO ZERO WITH NO ENGINE ABNORMALITIES. AIRCRAFT RETURNED TO PIT SAFELY. MAINTENANCE TO AIRCRAFT REMOVED AND REPLACED TORQUE INDICATOR. AIRCRAFT RETURNED TO SERVICE.SDR MALA030434Connector · damagedDURING CLIMBOUT ON FLIGHT NR 2742, LT INTAKE HEAT LIGHT ILLUMINATED. AIR RETURN TO MSP. MAINTENANCE MOVED LT SHOE BOX THERMISTER CONNECTOR FROM NR 4 TO NR 2 20 MIN OPS CHECKS GOOD IAW AMM 30-00-00.SDR MALA030433Skin · dentedDURING 4Y/2Y INSPECTION IN CWA, LT FUSELAGE HAS DENT AT STA 560 BETWEEN STRINGER SL1516 & SL1517 6 INCH X 1INCH CREASE, MAINTENANCE REPAIRED DENT IAW EO NR S53035. REFER TO 409 NR 177009, LOG PAGE NR 1222281, FOR DETAIL.SDR 180131Motor · inoperativeFLT 4588 PIT-IPT. DURING CLIMB OUT AND DESCENT FLIGHT CREW NOTICED THAT THE MAIN ELEVATOR WARNING LIGHT WAS ILLUMINATED. THE CREW FOLLOWED THE QRH AND DISCONNECTED THE AUTO-PILOT, THEY THEN NOTICED THAT THE MAIN ELEVATOR TRIM WAS INOPERATIVE AND NOT TRIMMINGSDR 154691Engine · failedDURING TAKE-OFF ROLL AT 60 PERCENT TQ CTOT WAS NOT ARMED. THE CREW HEARD A LOUD BANG, AND THE RT ENGINE TQ STARTED TO DROP AND THE RT ENGINE ITT SPIKED AND THE ENGINE OVERTEMP WARNING LIGHT ILLUMINATED. PAX AT SEAT 10F SAW FLAMES FROM TAILPIPE. THE CREW IMMEDISDR 180401Warning Light · illuminatedFLT 4507 ON TAKEOFF FROM CRW TO PIT ON 9/9/03 EXPERIENCED A CONFIGURATION WARNING ON TAKEOFF. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO GATE. SUSPECT CONDITION LEVER BACKED OFF DURING ROLL AND CAUSED WARNING.SDR 141191Wire · brokenDURING FLIGHT THE RT AIR VALVE WARNING LIGHT ILLUMINATED. CREW FOLLOWED QRH AND REDUCED POWER BELOW 92 PERCENT, AND THE LIGHT STAYED ILLUMINATED. THE CREW RETURNED TO PIT A/C WAS TAKEN OUT OF SERVICE AT 2235 (LT). PIT MX T/S RT INTAKE HEAT SYSTEM AND FOUNDSDR MALA030397Computer · malfunctionedAUTOCOURSEN LIGHT ILLUMINATED ON TAKEOFF ROLL. ABORTED TAKEOFF. REPLACED AUTOCOURSEN COMPUTER. P/N ON AND OFF 8542M2, SN/ON 504, S/N OFF 215SDR 179152Chip Detector · contaminatedFLT 4451 FROM PIT TO CMH. AIRCREW RECEIVED A CHIP DETECTOR LIGHT IN FLIGHT ON THE LT ENGINE. ALL PERIMETERS WERE NORMAL. ON RETURN TO PIT, WITH POWER BROUGHT BACK TO 30 PERCENT, LIGHT WENT OUT. AIRCREW RETURNED TO PIT SAFELY WITH NO FURTHER INCIDENT. MAINTENASDR 189201Warning Light · illuminatedON 08/25/03, APPROX. 1143(UTC), FLT 4500, AIRCRAFT ABORTED TAKEOFF WHEN THE FLIGHT IDLE STOP OPEN LIGHT ILLUMINATED AFTER GEAR RETRACTION. AIRCRAFT RETURNED TO FIELD.SDR 189111Warning Light · illuminatedFLIGHT 4493 FROM PIT TO CLE. AIRCREW WAS IN THE PROCESS OF TAKING OFF WHEN THEY RECEIVED THE INDICATION OF THE AUTOCOARSEN NOT ARMING. AIRCREW ABORTED TAKEOFF AND RETURN TO THE GATE WITHOUT INCIDENT.SDR MALA030375Potentiometer · inoperativeDURING CLIMBOUT ON FLIGHT NR 3321, AT LEVEL FLIGHT THE FLAPS BEGAN UNCONTROLLED MOVEMENT CAUSING THE AIRCRAFT TO PITCH. THE FLAP MOVEMENT WAS CONFIRMED WITH THE FLAP INDICATOR. AIR RETURN TO MSP MAINTENANCE WITH FLAPS 0 DEG, SIMULATED AIR LOAD ON FLAPS AND NSDR 164771Wire · shortedCLIMBING AT AT 9K FT. WHEN THE LT ENGINE OIL PRESS. WARNING LIGHT ILLUMINATED. THE CREW NOTICED THAT THE LH PROP OIL PRESSURE WAS AT ZERO. THE CREW REDUCED POWER TO THE LT ENGINE AND RETURNED TO PIT. A/C REMOVED FROM SERVICE AT 2230 HDQ TIME. PIT MX T/S LT ESDR 160191Warning Light · false activationON DESCENT INTO PIT, AIRCREW RECEIVED A FLAP CAUTION LIGHT. FLAP INDICATOR WAS READING ZERO AND THE HANDLE WAS SET AT ZERO. AIRCREW DECLARED AN EMERGENCY AND LANDED SAFELY IN PIT. MAINTENANCE INSPECTED FAULT AND FOUND NOTHING WRONG. AIRCRAFT RETURNED TO SERVICSDR 194962Controller · malfunctionedFLT NR 4516 ON 8/12/03 LYH - PIT, ON TAKEOFF ROLL AUTOCOARSEN SYSTEM FAILED TO ARM WITH TQ ABOVE 80 PERCENT, CAPTAIN ABORTED TO AND RETURNED TO GATE.SDR 161971Interphone · inoperative08/11/03, AT APPROX. 1845(UTC) FLT 4506 PIT-CRW, AIRCRAFT 152CQ HAD PERFORMED A RETURN TO GATE FOR COCKPIT TO CABIN INTERPHONE INOPERATIVE. FLIGHT ATTENDANT COULD NOT TRANSMIT TO CREW.
Back to Saab SF340A