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 = '1900D' 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 = '1900D' 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 GUUA10200602Unknown · odorFLIGHT: 9165, DURING FLIGHT FUEL ODOR COMING THROUGH AIR VENTS. CHECKED INSPECTED AND CLEANED RT ENGINE PURGE TANK NO DEFECTS NOTED.SDR GUUA10200601Warning Horn · malfunctionedFLIGHT: 5402 PBI/FL - AFTER TAKEOFF, CANNOT SILENCE LANDING GEAR WARNING HORN WITH LANDING GEAR UP AND POWER LEVERS REDUCED. CLEANED LANDING GEAR HORN SILENCE SWITCH PERFORMED NUMEROUS OPERATIONAL CHECKS OF LANDING GEAR. COULD NOT DUPLICATE OPERATIONAL CHECKSDR AMWA080281Brake Cable · wornUPON LANDING, THE LT BRAKE BLED OFF PRESSURE. CREW NOTICED THE LT BRAKE WASN'T WORKING. AIRCRAFT MADE IT TO THE GATE WITHOUT FURTHER NOTICE. MAINTENANCE HAD TO DRIVE IN. TO BLEED BRAKES, OPS CHECKED NORMAL. WHEN AIRCRAFT ARRIVED IN MAINTENANCE, MAINTENANCE RESDR NSVA200600180Pin · poppedCARGO DOOR LIGHT ILLUMINATED IN FLIGHT, EXTINGUISHED WITH CABIN DEPRESSURIZATION. FOUND POP OUT PIN STICKING LUBED PIN FOUND TO FUNCTION FINE AT THIS TIME.SDR NSVA200600179Module · cracked50-100 LBS TQ FLUX ON NR 2 ENG WITH ACCOMP PROP RPM FLEX PROP SYNC ON/OFF. FOUND RT ENG AIRFRAME BLEED LINE CRACKED, REPLACED LINE IAW 71-00-00. FOUND R BRAKE DEICE PNEUMATIC TUBE LOOSE AT FWD FIREWALL, RECONNECTED AND TIGHTENED LINE. INSPECTED PRECOOLER, PSDR GUUA10150601Fire Bottle · defectiveFLIGHT: 6002 PBI/ASD DURING CLIMB RIGHT ENGINE FIRE EXTINGUISHER DISCHARGE INDICATOR FLICKERED. RETURNED TO PBI LANDED WITHOUT INCIDENT. REPAIRED BROKEN WIRE AND REPLACED RIGHT ENGINE FIRE BOTTLE OPERATIONAL CHECK NORMAL.SDR AMW1061011025Spar Cap · corrodedFOUND CHAFING AREA, LT WING LOWER MAIN SPAR CAR, FORWARD SURFACE AT APPROX. WS 72.0. REPAIRED IAW MFG FR-CO-01437 REV. 1.SDR AM1060904005ASpar Cap · corrodedBIOCORROSION ON RT WING MAIN SPAR FWD SPAR CAP FLANGE NEAR WING STATION 126.00. MAINTENANCE COMPLIED WITH MFG REPAIR FR-CO-01417 REV. 2.SDR GUUA10120602Wire · looseFLIGHT: 9286 EYW/FLL DURING FLIGHT NR 1 ENGINE DISCHARGE LIGHT ILLUMINATED. FOUND WIRE SPLICE LOOSE AT NR 1 ENGINE FIRE BOTTLE. RESPLICED WIRE FROM FIRE EXTINGUISHER BOTTLE, OPERATIONAL CHECK GOOD.SDR AMWA080101Switch · out of adjustFLAP HANDLE WAS SELECTED TO 17 DEGREES AND THEY WENT TO 35 DEGREES UNCOMMANDED. AIRCRAFT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE CLEANED AND ADJUSTED FLAP SWITCH, OPS CHECKED NORMAL NO PARTS WERE USED.SDR GLBA20060837Spar · crackedRIGHT WING AT BL 114.25 AND F.S. 330 FOUND A .094 CRACK ON AFT SPAR, REPAIR PENDING.SDR CA061220005Bolt · sheared(CAN) IN CRUISE FLIGHT, ENGINE OIL PRESSURE WAS SEEN TO FLUCTUATE AND THEN DECAY TO ZERO. THE ENGINE WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INVESTIGATION REVEALED A SHEARED 1ST STAGE REDUCTION GEAR BOX CARRIER BOLT. (TC NR 20061220005)SDR 1060731037DSpar · unknownINSTALLED SHIM FILLER BETWEEN MAIN SPAR LOWER FLANGE AND SKIN. INSTALLED DOUBLER ON LOWER MAIN SPAR SKIN. REPAIRED IAW MFG ENG. REPORT NR 6386-1 REV. 1R DATED 10/04/06.SDR GUUA10100601Unknown · odorDURING FLIGHT, STRONG LUBRICATION SMELL PRESENT IN THE COCKPIT AND CABIN. INSPECTED UNDER FLOORBOARDS IN CABIN AND COCKPIT CLEANED HYDRAULIC FLUID DUE TO OVERSERVICE NO LUBRICATION SMELL NOTED AT THIS TIME.SDR AMWA080040Control System · out of adjustON APPROACH, CREW PLACED THE FLAP HANDLE TO 17 DEGREES. THE FLAPS CONTINUED TO EXTEND TO 35 DEGREES THUS CAUSING THE OVERSPEED OF THE FLAPS. THE AIRCRAFT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE CAME AND C/W WITH THE FLAP INSPECT IAW BMM 05-50-00 PG 201. SDR NSVA200600175Autofeather Sys · no testLEFT ENGINE AUTOFEATHER TEST FAILED, REF FLT FORM 108390. PERFORMED AUTOFEATHER OPERATIONAL CHECKS IAW BEECH 1900 MM. AUTOFEATHER CHECKS SATISFACTORY AT THIS TIME.SDR GLBA20060833Angle · crackedRT HEAVY DOUBLERS CRACKED (ANGLE) AT F.S. 288.0 PN NR 114-430002-7180 (RT)SDR CA061103013Turbine Blades · damaged(CAN) ON TAKEOFF ROLL THE ENGINE EMITTED A LOUD NOISE ACCOMPANIED BY A LOSS IN POWER. TAKEOFF WAS ABORTED. SUBSEQUENT INSPECTION REVEALED DAMAGED POWER TURBINE BLADES. MFG WILL MONITOR INVESTIGATION OF THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TSDR GLBA20060840Stringer · crackedSTRINGER 8R - 8L CRACKED, CANTED BULKHEAD F.S. 588.10 - REPAIR PENDINGSDR GLBA20060832Skin · corrodedCORROSION FOUND ON BELLY OF AIRCRAFT FS 223-75 TO 232.75, 3.5 INCHES O/B OF STRINGER 15R TO 4 INCHES LEFT OF STRINGER 16, REPAIR PENDING.SDR NSVA200600167Torquemeter · stuckRT TQ GAUGE STUCK AT 2400 WITH NO POWER OR ENGINES RUNNING. REMOVED AND REPLACED RT TORQUE GAUGE PER BMM 31-10-00. RUN UP CK NORMAL.SDR GLBA200606842Spar · crackedHORIZONTAL SPAR WEB CRACKED AROUND DEICE TUBE HOLE - REPAIR PENDING.SDR GUUA10040601Uplock Switch · out of adjustFLT 9292 JAX/TPA DURING FLIGHT THE LANDING GEAR HANDLE LIGHT ILLUMINATED AFTER TAKEOFF AND FLICKERED DURING FLIGHT WITH THE GEAR RETRACTED. CONTINUED, LANDED WITHOUT INCIDENT. ADJUSTED THE RT MAIN LANDING GEAR UPLOCK SWITCH, LANDING GEAR OPERATIONAL CHECK NOSDR GLBA20060841Hinge · crackedCARGO DOOR HINGE LUGS CRACKED. REPAIR PENDING EO 05-02.SDR GLBA20060843Stringer · crackedSTRINGER 10R CRACKED AT F.S. 450.00 - REPAIR PENDINGSDR NSVA200600154Fuel Control · malfunctionedRT TORQUE FLUCTUATION OF 75LBS ALONG WITH NP AND N1 AND FUEL FLOW ABOVE 90% N1. REMOVED AND REPLACED RT FCU PN ON/OFF 8063-005, SN OFF 248757 ON, 12361735 IAW CWC 73-20-01, OPS AND LEAKS CK GOOD.SDR 1060731037CFrame · corrodedCORROSION, FRAME AFT FACE. FS 288.0 AT APPROX. LBL 26.0 AND RBL 25.0. FOUND DURING INSPECTION REPAIRED IAW MFG FR.CO.01399 REV. 1.SDR 1060731037BFrame · corrodedCORROSION FUSELAGE FRAME AT FS 213.25 (LBL 8.4) CORROSION FOUND DURING INSPECTION. REPAIRED IAW MFG FR.CO.01423 REV. 1.SDR 1060731037ASpar Cap · corrodedCORROSION FOUND ON WING LOWER MAIN SPAR CAP, FORWARD FACE AT APPROXIMATELY LBL 19.75 / RBL 16.4. FOUND DURING INSPECTION. REPAIRED IAW MFG FR-CO-01398-REV. 2SDR NSVA200600164Wire · brokenFLAPS WILL NOT RETRACT LESS THAN 17 DEGREES. UPON INSPECTION FOUND LT FLAP SAFETY SWITCH TO HAVE ONE BROKEN WIRE AND WORN ROLLER. REPAIRED WIRE IAW BAMM 20-13-00 AND REPLACED WORN CAM BY REMOVING BOLT AND NUT AND REINSTALLING. OPS CHECK GOOD, P/N OFF/ON 101SDR NSVA200600151Connector · unsecureRT T-HANDLE WILL NOT TEST. REMOVED AND RESECURED RT FIRE LOOP CONNECTOR ON RT ENGINE. OPERATIONAL CHECK GOOD IAW 26-10-00.SDR CA061003004Angle · cracked(CAN) WHILE COMPLETING A PRESSURIZATION CHECK OF THE CABIN, AIR WAS FOUND TO BE LEAKING OUT AROUND SPAR/ FUSE JOINT AREA. CRACKS WERE FOUND ON THE LT AND RT WING-FUSELAGE CLOSING ANGLES AT FS 288 IN THE SAME SPOTS MEASURING 1.7500 INCHES EACH. LT ANGLE IS P/SDR NSVA200600152Circuit Breaker · smokeSMOKE IN COCKPIT COMING FROM F/O'S C/B PANEL AT THE LANDING GEAR C/B. REMOVED AND REPLACED C/B GEAR INDICATOR PLT 7277-2-5, LTS WORKS AT THIS TIME. NO SMOKE IN COCKPIT OLD C/B BURNED AND INOP PER BMM 24-00-01.SDR NSVA200600159Power Lever · out of adjustRIGHT PROP AUTOFEATHERED INFLIGHT DURING APPROACH TO LANDING UPON MOVING PROPS FULL FORWARD. PERFORMED ENGINE RUNS IAW 71-00-00, 3/4 KNOB SPLIT WITH TEST SWITCH ON 1500 RPM, 1800 FT. ADJUSTED POWER LEVERS IAW 76-10-00. NO OTHER DEFECTS NOTED, OPS CHECK GOODSDR NSVA200600156Unknown · unknownRIGHT PROP AUTOFEATHERED INFLIGHT, DURING APPROACH TO LANDING UPON MOVING PROPS FULL FORWARD. CLEANED AND INSPECTED ALL RT ENGINE NOSE SECTION CONNECTOR PLUGS, NO DEFECTS NOTED AT THIS TIME. CLEANED AND INSPECTED ALL RT ENGINE NOSE SECTION WIRING HARNESS FORSDR CA060926004Control Cable · broken(CAN) CREW REPORTED DIFFICULTY WITH CHANGING THE ELEVATOR TRIM ON APPROACH. MAINTENANCE FOUND THAT THE ELEVATOR TRIM CABLE HAS BROKEN AT THE TRIM SERVO/CAPSTAN LOCATION. THIS SERVO/CAPSTAN COMPONENT IS ONLY INSTALLED ON AUTOPILOT EQUIPPED 1900D`S OF WHICH THESDR S2YA06008Spar Cap · crackedON 08/30/06 DURING INSPECTION REQUIRED BY AD 2006-18-51 FOUND CRACK ON RT WING AFT SPAR, LOWER SPAR CAP AFT FLANGE AT WING STATION 117 INCHES. THE CRACK RAN STRAIGHT FROM THE AFT EDGE TO A RIVET HOLE. THE DAMAGE WAS REPAIRED IAW MFG RDO FIELD REPAIR FR-CO-0140SDR GUUA09190601Valve · malfunctionedFLIGHT: 9220 PBI/TPA DURING APPROACH LANDING GEAR CIRCUIT BREAKER POPPED GEAR WOULD NOT COME DOWN MANUALLY EXTENDED LANDING GEAR. LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR SERVICE VALVE, LANDING GEAR OPERATIONAL CHECK NORMAL.SDR CA061006012Engine · leaking(CAN) DURING TAKE-OFF CLIMB, THE ENGINE LOW OIL PRESSURE WARNING ACTIVATED AND OIL PRESSURE DECREASED TO ZERO. THE ENGINE WAS SHUTDOWN IN FLIGHT AND THE AIRCRAFT DIVERTED TO POINT OF DEPARTURE. INSPECTION REVEALED OIL IN THE ENGINE EXHAUST DUCT. MFG WILL INSDR 1060918030Oil System · low pressureAFTER TAKEOFF ON CLIMBOUT LEFT OIL PRESSURE ANNUNCIATOR ILLUMINATED & OIL PRESSURE WAS BELOW 60 PSI ON INDICATOR AT 3500 LB TORQUE. CREW SHUT ENGINE DOWN AND RETURNED TO FIELD WITHOUT FURTHER INCIDENT. NOTE: INFORMATION IN COMPUTER BLOCKS IS FOR GAS GENERATOSDR NSVA200600144Circuit Breaker · trippedRT FIRE T-HANDLE FAILS TO ILLUMINATED DURING AMP TEST. FOUND RT FIRE T-HANDLE MONITOR C/B POPPED, RESET C/B. OPS CHECK OK IAW BEECH MM 26-11-02.SDR AMWA079616Powerpack · underservicedAFTER DEPARTURE, THE CREW RETRACTED THE GEAR AND THE INTRANSIT LIGHTS REMAINED ILLUMINATED. THE CREW THEN CYCLED THE GEAR AND THE LIGHT REMAINED ILLUMINATED. CREW EXTENDED THE GEAR AGAIN AND HAD NORMAL DOWN AND LOCKED INDICATION. THE CREW THEN DECIDED TO RETURSDR GUUA09150601Circuit Board · malfunctionedFLIGHT: 9299 TLH/TPA AFTER TAKEOFF LANDING GEAR CIRCUIT BREAKER POPPED WHILE RETRACTING THE LANDING GEAR. RESET CIRCUIT BREAKER CONTINUED TO TPA LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR TIME DELAY PC BOARD LANDING GEAR OPERATIONAL CHECK NORMAL.SDR GUUA09140602Line · looseFLIGHT: 9247 FLL/BIM DURING TAXI COMPLETE LOSS OF BRAKE PRESSURE ON THE RIGHT BRAKES. TIGHTENED RIGHT BRAKE LINE OPERATIONAL CHECK GOOD.SDR GUUA09140601Unknown · malfunctionedFLIGHT: 9302 GHB/FLL DURING APPROACH LANDING GEAR RELAY CIRCUIT BREAKER POPPED, MANUALLY EXTENDED LANDING GEAR. LANDED WITHOUT INCIDENT. INSPECTED LANDING GEAR SWITCHES AND WIRING PERFORMED LANDING GEAR EXTENSION AND RETRACTION. OPERATIONAL CHECK NORMAL, NOSDR NSVA200600141Limit Switch · malfunctionedFLAPS WILL NOT RETRACT BEYOND 17 DEGREES. FOUND INBD UPLIMIT SWITCH IN RT INBD WING STICKING FROM CORROSION. CLEANED, INSPECTED AND LUBED. OPS CK NORMAL.SDR CA060921004Engine · leaking(CAN) THE CREW REPORTED A LOW OIL PRESSURE INDICATION WHILE TAXING, SOME OIL WAS NOTED ON THE FUSELAGE SO AN AME WAS DISPATCHED. THEY COULD FIND NO AREA OF LEAKAGE DURING INSPECTION AND THE AIRCRAFT WAS REPLENISHED AND NUMEROUS GROUND RUNS DID NOT REVEAL ANYTHSDR CA061006017Engine · leaking(CAN) IN FLIGHT THE ENGINE LOST OIL PRESSURE. THE ENGINE WAS SHUTDOWN IN FLIGHT AND THE AIRCRAFT DIVERTED TO POINT-OF-DEPARTURE. POST-FLIGHT INSPECTION REVEALED A LOW ENGINE OIL LEVEL AND NOISES FROM THE ENGINE POWER SECTION ON ROTATION. MFG WILL INVESTIGATSDR NSVA200600135Vane · contaminatedON ROTATION AT115KIAS, STALL HORN SOUNDED, AND WOULDN`T TURN OFF UNTIL LNDG GEAR RETRACTED PULLED STALL WARNING CB TO EXTINGUISH WARNING HORN. FOUND BUG/DEBRIS LODGED IN VANE. CLEANED AND INSPECTED LUBED AND FUNCTIONAL CHECKED NORMAL ON GROUND IAW 27-31-00.SDR NSVA200600139Actuator · malfunctionedFLAPS STOPPED AT AN INTERMEDIATE POSITION. ALSO, POSSIBLE SLIPPAGE OF NR 3 FLAP DRIVE. REMOVED AND REPLACED FLAP MOTOR AND GEARBOX ASSY WITH SERVICEABLE UNIT IAW 27-50-03, PN ON/OFF 100-524073-1, SN ON 3776, SN OFF 3741. ALSO REMOVED AND REPLACED NR 3 FLAP
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