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 = '1900C' 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 = '1900C' 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 AUS20040474Circuit Board · faulty(AUS) AIRFRAME DE-ICE SYSTEM PRINTED CIRCUIT BOARD (PCB) TIMER INOPERATIVE.SDR CA040518007Hose · cracked(CAN) AFTER TAKE OFF CREW OBSERVED SPARKS AND GLOW FROM RT ENGINE COWL. CREW SHUTDOWN RT ENGINE AND RETURNED TO AIRPORT. MAINTENANCE FOUND THE FLEXIBLE HOSE FROM THE EXHAUST STACK TO THE LIP HEATER HAD CRACKED AND SEPERATED FROM THE COWLING. THIS ALLOWED THESDR CA040518003Hose · kinked(CAN) AFTER TAKE OFF, CABIN BEGAN TO FILL WITH FUMES AND OIL VAPOR. CREW TURNED OFF ENGINE BLEED AIR AND RETURNED TO AIRPORT. MAINTENANCE FOUND NR 1 ENGINE BREATHER HOSE HAD BEEN KINKED AND PINCHED CAUSING THE ACCESSORY CASE TO PRESSURIZE AND FORCE OIL TO PASSSDR CA040518008Selector Valve · intermittent(CAN) DURING APPROACH THE CREW NOTICED THAT THE LANDING GEAR WAS LOUDER THAN USUAL ANDSLOWER TO EXTEND. MAINTENANCE FOUND THE POWER PACK SELECTOR VALVE TO BE INTERMI TTENT AND THE POWER PACK TO BE NOISY. WITH THE AIRCRAFT ON JACKS THERE WERE TIMES WHEN THE GEASDR ACE050504Pump · leakingPILOT REPORTED FUEL LEAKING FROM ENGINE DRAIN. MAINTENANCE REPLACED LOW PSI FUEL PUMP.SDR GLBA20030617Circuit Breaker · trippedGEAR WILL NOT TRANSIT UP OR DOWN, RESET 60 AMP C/B OPS CK GOODSDR 106041Display · inoperativeCAPTAINS VSI DISPLAY UN-USEABLE AND DISCHARGING BURNED ODORS IN CABIN REMOVED AND REPLACED CAPTAINS VSI PERFORMED SATISFACTORY STATIC CHECK IAW AMM 34-10-06.SDR ACE032304Diaphragm · rupturedFOUND DIAPHRAGM LEAKING (RUPTURED) - THIS PUMP WAS BEING INSPECTED DUE TO AN ABORTED TAKEOFF AFTER ENGINE FLAME OUT. 1384 HOUR & 6 MONTHS AFTER INSTALL.SDR ACE032204Engine · flamed outNR 2 ENGINE FLAMED OUT ON TAKEOFF. ABORTED TAKEOFF. MAINTENANCE COULD NOT DUPLICATE.SDR 072041Screw · looseDURING FLIGHT CONTROL CHECK, CONTROL COLUMN WOULD NOT RETURN TO FULL FORWARD POSITION. INSPECTED AND FOUND ONE SCREW MIGRATED FROM LEFT ELEVATOR, RESET SCREW AND SECURED WITH SPEED TAPE, FERRIED AIRCRAFT TO HEF, FOUND BALANCE WEIGHT ASSY AT O/B ELEVATOR L/E WSDR AUS20040165Transducer · unserviceable(AUS) RT ENGINE OIL PRESSURE TRANSDUCER FAULTY.SDR CA040309001Control Cable · severed(CAN) AFTER LANDING AND SUBSEQUENT TAXI THE RT ENGINE SPOOLED UP AND DID NOT RESPOND TO POWER LEVER MOVEMENT. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT COMPLETED TAXI TO THE TERMINAL ON THE LT ENGINE. MAINTENANCE INVESTIGATED AND DISCOVERED THAT THE POWER LEVESDR AUS20040058Hinge · corroded(AUS) RUDDER CENTER HINGE CONTAINED EXFOLIATION CORROSION IN THE HINGE BRACKET WEB.SDR ACE013104Indicator · failedPILOT REPORTED CAPTAIN'S ALTIMETER FAILED (FLAGGED) AT 600 FT AFTER TAKEOFF. RETURNED TO AIRPORT. MAINTENANCE REPLACED THE FAILED ALTIMETER.SDR CA040203004Relay · failed(CAN) LANDING GEAR FAILED TO EXTEND ON APPROACH. EMERGENCY EXTENSION WAS CARRIED OUT AND AIRCRAFT LANDED SAFELY. MAINTENANCE FOUND THAT THE LANDING GEAR MOTOR WAS NO LONGER RUNNING. THE LANDING GEAR RELAY WAS FOUND INTERNALLY DAMAGED WITH THE CONTACTS STUCK INSDR ACE012504Diaphragm · rupturedMAINTENANCE NOTICED FUEL DRAINING FROM ENGINE GANG DRAIN - REPLACED LOW PSI FUEL PUMP DUE RUPTURED DIAPHRAGMSDR FFS2004F00000Wire · shortedWHEN PERFORMING BUSS SENSE TEST, LOW VOLTAGE (11V-18V) WAS STILL PRESENT ON CENTER BUSS WITH BUSS TIE RELAYS OPEN. IT WAS DETERMINED SOURCE OF VOLTAGE WAS RT GENERATOR BUSS. WHILE SYSTEMATICALLY OPENING CB POWERED OFF RT GENERATOR BUS, VOLTAGE ON CENTER BUSSSDR 2004F00226Skin · crackedDURING A SCHEDULED INSPECTION, A CRAC WAS DISCOVERD IN THE RUDDER SKIN. THE CRACK LOCATION WAS ABOUT 4 INCHES DOWN FROM THE TOP OF THE RUDDER. THE CRACK SPLIT THE TRAILING EDGE FOR ABOUT 1.5 INCHES THEN CRACKED TO OPPOSITE SIDES OF THE RUDDER FROM EITHER ENDSDR 015042Computer · odorR ENVIR OFF LIGHT FAILS TO ILLUMINATE WITH BLEED AIR VALVE IN OFF POSITION, ELECTRICAL ODOR IN MAIN CABIN. SOURSE OF ODOR YAW DAMP COMPUTER, YAW DAMP COMPUTER DEFERRED PER MEL 22-1 CAT C.SDR 018041Actuator · maladjustmentNOSE GEAR UNSAFE, NOSE GEAR WOULD NOT EXTEND AND LOCK, NO GREEN LIGHT, AND RED LIGHT IN THE HANDLE REMAINED ILLUMINATED. RESET CIRCUIT BREAKER, NOSE GEAR CAME DOWN. REPLACED ALL THREE RETRACT ACTUATORS, HYD SERVICE VALVE, AND FLUSHED SYSTEM.SDR 016041Computer · malfunctionedRT ENVIR OFF LIGHT FAILS TO ILLUMINATE WITH BLEED AIR VALVE IN OFF POSITION ELECTRICAL ODOR IN MAIN CABIN. SOURSE OF ODOR YAW DAMP COMPUTER. YAW DAMP COMPUTER DEFERRED PER MEL 22-1 CAT C.SDR 015043Computer · malfunctionedRIGHT ENVIR OFF LIGHT FAILS TO ILLUMINATE WITH BLEED AIR VALVE IN OFF POSITION, ELECTRICAL ODOR IN MAIN CABIN. SOURSE OF ODOR YAW DAMP COMPUTER. YAW DAMP COMPUTER DEFERRED PER MEL 22-1 CAT C.SDR 013041Handle · lack of lubePAX DOOR HANDLE HARD TO TURN. LUBED DOOR HANDLE, OPS CHECKED GOOD.SDR CA040121004Windshield · broken(CAN) WINDOW SHATTERED IN CRUISE, INSIDE AND OUT SIDE PANE.SDR ACE122403Exhaust Duct · disconnectedPILOT REPORTED EXHAUST SMELL IN CABIN ON TAKEOFF AND CLIMB. MAINTENANCE LOCATED A DISCONNECTED NR 1 ENGINE INTAKE HEATED LIP (EXHAUST DUCT) TUBE. EXHAUST COULD HAVE BEEN INGESTED BY THE ENGINE AND THEN MIXED WITH THE BLEED AIR. NO PART FAILURE WAS OBSERVED.SDR AUS20031295Seal · split(AUS) CABIN DOOR SEAL SPLIT ALONG TOP SECTION. LENGTH OF SPLIT APPROXIMATELY 50MM (1.96IN).SDR CA040107005Heater · cracked(CAN) OIL PRESSURE ANNUNCIATOR ILLUMINATED FOLLOWED BY OIL PRESSURE FLUCTUATIONS. CREW THEN SHUT ENGINE DOWN AND LANDED WITH NO FURTHER PROBLEMS. UPON INSPECTION BY MAINTENANCE IT WAS CLEAR THAT THERE WAS AN EXCESSIVE OIL LEAK AND LOW OIL LEVEL. THIS WAS THE CSDR CA031218003Latch · failed(CAN) AFTER COMPLETING FLIGHT AND TAXIING THE PILOT WAS UNABLE TO OPEN THE AIRSTAIR DOOR TO DISEMBARK PASSENGERS. THEY WERE REQUIRED TO EXIT THE AIRPLANE USING THE OVER WING EMERGENCY EXIT. BEFORE MAINTENANCE PERSONNEL WERE ABLE TO ARRIVE ON THE SCENE THE PILSDR AUS20031218Cap · cracked(AUS) NOSE LANDING GEAR ACTUATOR END CAP CRACKED.SDR ACE112503Warning System · malfunctionedNOSE GEAR FAILED TO SHOW DOWN AND LOCKED UNTIL GEAR WAS CYCLED TWICE. MAINTENANCE COULD NOT DUPLICATE FAULT.SDR JIKA200300002Line · chafedAFTER SHUT DOWN OF LT ENGINE GROUND CREW OBSERVED FUEL LEAKING FROM LT ENGINE COWLING. UPON INVESTIGATION MAINTENANCE FOUND THE FUEL FLOW TRANSDUCER INLET LINE CHAFED AND LEAKING FROM THE CHAFED AREA. THE STARTER GENERATOR COOLING DUCT SCAT TUBING WAS THE CASDR TIM2003F00001Bulkhead · crackedBULKHEAD FOUND TO BE CRACKED AT INSPECTION. (CNTRL NR 81)SDR 297031Circuit Card · malfunctionedDURING TAKEOFF ROLL MASTER CAUTION ILLUMINATED TO INDICATE THAT BOTH THE LEFT AND RIGHT GEN TIES WERE OPEN ONE ATTEMPT WAS MADE TO RESET. DID NOT RESET, THE TAKEOFF WAS ABORTED.SDR CA031027008Shaft · sheared(CAN) ELECTRIC TRIM (ELEVATOR) DRIVE SHAFT SHEARED. THIS CAUSED ONE CAPSTAND TO OPERATE AND THE OTHER TO MOVE FREELY ON ITS OWN. THIS MOVEMENT CAUSED THE BRIDAL CABLES TO UNWIND AND CREATE RESTRICTION. THE TRIM WAS RESTRICTED FROM GOING NOSE DOWN. MANUAL MOVEMSDR 2004F00207Windshield · crackedCO-PILOT OUTER WINDSHIELD PANE CRACKED. CRACKS OCCURRED DURING THE APPROACH PHASE OF THE FLIGHT AT ABOUT 3,000 FEET MSL WITH MINIMAL CAIBN DIFFERENTIAL PRESSURE. WINDSHIELD HEAT WAS ON AND WORKING AT THE TIME. OUTSIDE AIR TEMPERATURE WAS WITHIN A COUPLE OF SDR CA031016003Line · cracked(CAN) ON APPROACH INTO SEATTLE THE RT ENGINE POWER DECREASED SLOWLY ON ITS OWN. THE CREW SHUTDOWN AND SECURED THE ENGINE. THE AIRCRAFT LANDED UNEVENTFULLY AND WAS TOWED FROM THE RAMP. DURING INVESTIGATION BY MAINTENANCE IT WAS FOUND THAT THE ENGINE WOULD ACTUSDR AUS20031030Engine · fluctuates(AUS) LT ENGINE TORQUE FLUCTUATIONS. FUEL FLOW, N1 AND ITT STABLE. GROUND RUN CARRIED OUT. UNABLE TO FAULT. DEFECT NOT CONFIRMED.SDR ACE093003Csd · failedPILOT REPORTED NR 2 ENGINE TORQUE STARTED TO SURGE (1500 LBLS) AND WAS SHUT DOWN PER THE QRH. MAINTENANCE REPLACED THE NR 2 ENGINE CONSTANT SPEED GOVERNOR AND OVERSPEED GOVERNOR FOR TROUBLESHOOTING (THE REPORTED PROBLEM COULD NOT BE DUPLICATED ON THE GROUND).SDR CA030924001Seal · detached(CAN) SEAL BECAME DETACHED FROM RETAINER AT UPPER AFT CORNER OF AIRSTAIR DOOR CAUSING RAPID DEPRESSURIZATION OF AIRCRAFT IN FLIGHT.SDR ACE0918021Diaphragm · perforatedON PREFLIGHT INSPECTION, PILOT NOTICED FUEL LEAKING FROM THE ENGINE GANG DRAIN. MAINTENANCE REPLACED THE LOW PSI FUEL PUMP DUE TO FUEL DRAINING FROM THE DRY SIDE OF THE PRESSURE RELIEF VALVE ASSEMBLY. DISASSEMBLY OF THE PUMP REVEALED MULTIPLE HOLES IN THE DISDR JIKASkin · corrodedDURING MAINTENANCE FOR A PRESSURIZATION SQUAWK FOUND THE LOWER BELLY SKIN AT FUSELAGE STATION 258.25 HAD A CRACK EMINATING FROM A RIVET HEAD AND THE SKIN AROUND THE RIVET WAS BULGED OUT. UPON FURTHER INSPECTION UNDER THE FLOOR BOARDS FOUND HEAVY CORROSION ON SDR ACE091103Pump · leakingPILOT NOTICED FUEL LEAKING FROM ENGINE DRAIN ON PRE-FLIGHT. MAINTENANCE REPLACED THE DEFECTIVE PUMP.SDR AUS20030924Bearing · collapsed(AUS) LT ENGINE STARTER-GENERATOR DRIVE END BEARING COLLAPSED.SDR AUS20030887Indicator · inoperative(AUS) LT ENGINE PERCENT RPM INDICATOR FAULTY.SDR ACE082503Fuel Control · faultyNR 2 ENGINE STARTED TO SURGE AND THEN LOST POWER - PILOTS SECURED THE ENGINE AND MADE AN UNEVENTFUL LANDING AT THE AIRPORT OF ORIGIN. REPLACED FCU.SDR ACE081603Relay · contaminatedPILOT REPORTED THAT IT TOOK MULTIPLE ATTEMPTS TO EXTEND THE GEAR WITH THE ELECTRO/HYDRAULIC SYSTEM. GEAR DID EXTEND AND UNEVENTFUL LANDING ACCOMPLISHED IN ANC. MAINTENANCE REPLACED THE HYD. POWER PACK RELAY (HEAVY CONDENSATION).SDR AUS20030731Uplock Switch · unserviceable(AUS) RT MAIN LANDING GEAR UPLOCK SWITCH UNSERVICEABLE.SDR ACE071903Fire Loop · defectiveRIGHT ENGINE FIRE LIGHT CAME ON IN FLIGHT REQUIRING ENGINE SHUTDOWN. PILOT REPORTED THAT WARNING DISCONTINUED 15 MINUETS AFTER ENGINE SHUTDOWN. SYSTEM OPS CHECKED GOOD ON GROUND AFTER LANDING. MAINTENANCE INSPECTED WARNING SYSTEM AND REPLACED FORWARD LOOP DSDR 1850301Handle · out of adjustEMERGENCY EXIT LOOSE IN LOCKED POSITION. ADJUSTED EXIT DOOR HANDLE TENSION.SDR 113AX62603Intercostal · crackedWHILE C/W STRUCTURAL INSPECTION 53-10-02, FOUND .5 INCH CRACK IN OUTER FLANGE RADIUS OF INTERCOSTAL PN 114-430116-7 AT STATION NR 498.25 AND ADJACENT TO THE CARGO DOOR AFT UPPER GAS STRUT ATTACH BRACKET MOUNTED TO THE DOOR FRAME.
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