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 = '402C' 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 = '402C' 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 AU981317Bracket · corroded(AUS) LEFT WING FLAP BELLCRANK UPPER AND LOWER BRACKETS CORRODED AND DAMAGED. SUSPECT THE LOWER BRACKET HAD FAILED ALLOWING THE FLAP ACTUATING BELLCRANK TO BE TORN OUT OF THE LOWER BRACKET AND DAMAGING THE UPPER BRACKET.SDR CA981001006Spring · broken(CAN) WHILE CARRYING OUT SERVICE BULLETIN CSB98-1B, THE OUTER VALVE SPRINGS ON NR 2 CYLINDER INTAKE AND EXHAUST, AS WELL AS ON NR 1 CYLINDER INTAKE VALVE WERE FOUND BROKEN. THE SPRINGS WERE REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE.SDR 98ZZZX3883Uplock Hook · failedTHE LT MAIN GEAR UPLOCK HOOK FAILED ON RETRACTION. FAILURE OCCURRED ACROSS THE UPLOCK HOOK BOSS SEPARATING THE UPLOCK ACTUATOR FROM THE HOOK PORTION OF THE UPLOCK ASSY CAUSING THE GEAR TO REMAIN LOCKED IN WHEEL WELL UPON EXTENSION. EMERGENCY PROCEDURES FAILESDR AU981427Gear · damaged(AUS) MAGNETO DISTRIBUTOR GEAR DAMAGED. EIGHT CONSECUTIVE TEETH STRIPPED.SDR AU981153Switch · leaking(AUS) HYDRAULIC PRESSURE SWITCH LEAKING FROM SWITCH BODY. SUSPECT FAILURE OF INTERNAL DIAPHRAGM.SDR 98ZZZX3933Bellcrank · crackedUPON INSPECTION OF LANDING GEAR SYSTEM, THE NOSE GEAR DOOR BELLCRANK WAS FOUND CRACKED AT LEFT DOOR EAR. THE NOSE GEAR DOORS WERE IMPROPERLY RIGGED CAUSING EXCESIVE STRESS ON BELLCRANK.SDR 99ZZZX655Pin · failedP/N'S AFFECTED: 514106-1 SHAFT; NAS561P5-18 PIN-SPRINGS TO HOLD 5141005-9 LINK ASSY. SAFETY PIN (NAS561P5-18) AND SAFETY WIRE (PER MM) THAT WAS TO SECURE PIN TO THE SHAFT (5141006-1) AND EXTERNAL APPEARANCE SHOWED NO DEFECTS. THE SAFETY WIRE REMAINED IN PLASDR AU981089Hose · deteriorated(AUS) LEFT MAIN LANDING GEAR EXTENSION HYDRAULIC HOSE DETERIORATED AND HOLED. LOSS OF HYDRAULIC FLUID. PART TC: 7.941.SDR 98ZZZX3610Web · crackedDURING HOSE INSPECTION, FOUND CRACKS ON WEB ASSEMBLIES AROUND THE ATTACH BOLTS FOR THE NOSE GEAR TRUNNION BEARINGS. SUBMITTER SUGGESTED CAUSE COULD BE SIDE LOADS ON NOSE GEAR DUE TO IMPROPER GROUND HANDLING PROCEDURES.SDR 98ZZZX3609Web · crackedDURING HOSE INSPECTION, FOUND CRACKS ON WEB ASSEMBLIES AROUND THE ATTACH BOLTS FOR THE NOSE GEAR TRUNNION BEARINGS. SUBMITTER SUGGESTED CAUSE COULD BE SIDE LOADS ON NOSE GEAR DUE TO IMPROPER GROUND HANDLING PROCEDURES.SDR 98ZZZX3433Web · crackedDURING NOSE INSPECTION, FOUND CRACKS ON WEB ASSEMBLIES AROUND THE ATTACH BOLTS FOR THE NOSE GEAR TRUNNION BEARINGS. POSSIBLY, SIDE LOADS ON NOSE GEAR DUE TO IMPROPER GROUND HANDLING PROCEDURES.SDR 98ZZZX3432Web · crackedDURING NOSE INSPECTION, FOUND CRACKS ON WEB ASSEMBLIES AROUND THE ATTACH BOLTS FOR THE NOSE GEAR TRUNNION BEARINGS. POSSIBLY, SIDE LOADS ON NOSE GEAR DUE TO IMPROPER GROUND HANDLING PROCEDURES.SDR AU981074Gear · stripped(AUS) RIGHT ENGINE MAGNETO DISTRIBUTOR GEAR TEETH STRIPPED.SDR AU980875Horn · failed(AUS) LANDING GEAR WARNING HORN INTERNAL CONTACT BETWEEN THE LEAF SPRING AND THE DIAPHRAGM HAD FALLEN OFF.SDR AU980904Frame · corroded(AUS) FORWARD CABIN DOOR FRAME CONTAINED SEVERE EXFOLIATION CORROSION IN THE AREA OF THE UPPER DOOR STRIKER PLATE.SDR 98ZZZX3207Wire · chafedTHE PILOT MADE A PRECAUTIONARY LANDING AT THE ROCHESTER, NY AIRPORT AS THE RIGHT HAND ENGINE'S CYLINDER HEAD TEMPERATURE BEGAN TO FLUCTUATE AND EVENTUALLY FELL TO ZERO BEFORE LANDING. AN INSPECTION OF THE ENGINE'S BAFFLING, EXHAUST MANIFOLD, AND CYLINDERS REVSDR AU980619Reduction Gear · failed(AUS) FLAP GEARBOX ASSEMBLY NOISY. STRIP INSPECTION FOUND THE REDUCTION GEAR TEETH STRIPPED.SDR 98ZZZX3208Spring · brokenTHE RIGHT ENGINE OIL PRESSURE DROPPED INTO THE YELLOW ARC DURING FLIGHT. THE AIRCRAFT MADE A PRECAUTIONARY LANDING (DID NOT SHUT DOWN ENGINE). INVESTIGATION REVEALED THE SPRING BROKE IN THE STARTER ADAPTER AND PIECES BECAME LODGED UNDER THE RELEIF VALVE. THSDR AU980573Tire · faulty(AUS) TIRE FAULTY. SIDEWALLS TOO SOFT AND SCRUBBING ON THE BRAKES. TIRE TREAD TOO SOFT. WITH THE CORRECT INFLATION PRESSURE, THE TIRE LOOKS FLAT.SDR AU980500Pipe · cracked(AUS) HYDRAULIC PIPE LOCATED BEHIND THE LT SIDE SPAR UNDER THE FLOOR SPLIT AND LEAKING. LOSS OF HYDRAULIC FLUID.SDR 98ZZZX1714Gusset · crackedDURING INSPECTION, FOUND GUSSET UNDER PILOT SEAT CRACKED. REPLACED WITH NEW PART.SDR 98ZZZX1713Support · crackedDURING INSPECTION, FOUND LEFT MAIN GEAR TRUNNION SUPPORT CRACKED ALONG WEBBING. REPLACED UNIT.SDR AU980387Circuit Breaker · failed(AUS) AVIONICS CIRCUIT BREAKER SWITCH SMOKING.SDR AU980451Warning System · faulty(AUS) LANDING GEAR WARNING HORN FAILED TO OPERATE CORRECTLY. AIRCRAFT LANDED WITH GEAR IN THE `UP' POSITION. INVESTIGATION COULD FIND NO FAULTS WITH THE SYSTEM.SDR 98ZZZX1661Valve · leakingDURING FLIGHT AT 10,000 MSL, PILOT NOTICED THAT OIL PRESSURE ON RIGHT ENGINE WAS DROPPING SLOWLY AND OIL TEMP WAS RISING SLOWLY FOLLOWED SHORTLY BY A COMPLETE LOSS OF MANIFOLD PRESSURE. THE PILOT TOOK PRECAUTIONARY MEASURES AND SHUT DOWN ENGINE. HE CONTINUEDSDR 98ZZZX1486Bolt · failedPILOT WAS LANDING ACFT WITH A CROSSWIND FROM THE RIGHT. PILOT TOUCHED DOWN ON RIGHT MAIN GEAR FIRST, AND THEN ON THE LEFT. AS ACFT DECELERATED WITH LITTLE OR NO APPLIED BRAKING ACTION, IT STARTED TO WOBBLE AND VEERED TO THE LEFT COMING TO A STOP OFF OF THE LSDR AU980279Valve · faulty(AUS) LANDING GEAR SELECTION VALVE FAULTY DUE TO HIGH RESISTANCE IN ELECTRICAL SOLENOID COIL. CAUSED BY INGRESS OF HYDRAULIC FLUID.SDR AU980277Master Switch · burnt out(AUS) AVIONICS MASTER SWITCH BURNED OUT. SUSPECT CAUSED BY WATER INGRESS VIA THE WINDOW SEAL.SDR 98ZZZX1316Bracket Assy · failedPILOT REPORTED NOSE GEAR WOULD NOT COME DOWN AND LOCK. A NOSE GEAR UP LANDING WAS MADE. INVESTIGATION REVEALED THE FORWARD LT NOSE GEAR GOOD RETRACTION ROD BRACKET ASSY FAILED ALLOWING THE NOSE GEAR TO IMPACT DOOR ON RETRACTION AND JAMMING NOSE GEAR IN WHEELSDR 98ZZZX989Valve Spring · brokenRIGHT ENGINE RUNNING ROUGH. FOUND 8 OF 12 VALVE SPRINGS BROKEN. REMOVED AND REPLACED ALL VALVE SPRINGS.SDR 98ZZZX988Valve Spring · brokenRIGHT ENGINE RUNNING ROUGH. FOUND 8 OF 12 VALVE SPRINGS BROKEN. REMOVED AND REPLACED ALL VALVE SPRINGS.SDR AU980187Gearbox · failed(AUS) FLAP GEARBOX IDLER GEAR TEETH SHEARED OFF.SDR 98ZZZX1125Line · failedFUEL REF LINE FROM FLOW DIVIDER TO BAFFLE BROKE CAUSING A ROUGH RUNNING ENGINE. AIRCRAFT LANDED WITHOUT INCIDENT.SDR AU980091Pipe · corroded(AUS) RH MAIN LANDING GEAR RETRACTION SYSTEM HYDRAULIC PIPE LOCATED IN AREA BELOW THE RH FLOOR CONTAINED PITTING CORROSION. SUSPECT DUETO CONTACT WITH DUCTING INSULATION.SDR AU980069Hose · deteriorated(AUS) HYDRAULIC PRESSURE HOSE LOCATED BETWEEN RH HYDRAULIC PUMP AND FIREWALL DAMAGED AND LEAKING. LANDING GEAR WOULD NOT EXTEND AND AIRCRAFT LANDED WITH GEAR UP. INVESTIGATION FOUND THAT THE HOSE FAILED DUE TO EXPOSURE TO HEAT WITH THE FIRE SLEEVING AND THE OUSDR 98ZZZX47Axle · crackedPILOT HAD DIFFICULTY DURING TAXI, RT WHEEL BINDING. MAINTENANCE FOUND BRAKE DISC CONTACTING LOWER BARREL OF STRUT. FOUND AXLE CRACKED UPON TIRE AND WHEEL REMOVAL.SDR CA971210014Clamp · improper(CAN) DURING 100-OUR INSPECTION WITH BOTH PROPELLER SPINNERS REMOVED, SEVERAL WIRES (P/N C15013-0604 LT AND RT) ON THE DEICE HARNESS WERE FOUND BROKEN. THIS FAULT HAS BEEN CAUSED BY THE HARNESS CLAMP (P/N MS21919WCF5) INSTALLED IN THE INVERTED POSITION.SDR 97ZZZX4962Potentiometer · failedAN ODOR OF ELECTRICAL SMOKE FILLED THE CABIN. AIRCRAFT LANDED WITHOUT INCIDENCE. FOUND THE DIMMER BOARD AT FAULT. DIMMER ASSY REPLACED AND AIRCRAFT RETURNED TO SERVICE.SDR CA980325019Valve · leaking(CAN) HEATER UNIT OBTAINED AS REPLACEMENT ITEM AND ON FIRST FLIGHT THE PILOTS COMPLAINED THAT THEY WERE NOT ABLE TO CONTROL HEATER. INVESTIGATION REVEALED THAT THE FUEL SOLENOID VALVE SEAL WAS NOT INSTALLED PROPERLY AND THIS ALLOWED FUEL TO LEAK OUT OF THE COSDR CA971104004Cable Assy · broken wires(CAN) DURING THE ROUTINE INSPECTION, BROKEN WIRES/STRANDS OF THE FLAP CONTROL CABLE ASSY WERE FOUND. DEFECTIVE CABLE ASSY AND PULLEY P/N S378-4 REPLACED AND SYSTEM CHECKED.SDR AU971351Pump · jammed(AUS) AUXILIARY FUEL PUMP CONTAMINATED BY ALUMINIUM SWARF. THE SWARF JAMMED THE PUMP VANES ALLOWING FUEL INTO THE MOTOR WINDINGS. THEAIRCRAFT HAD A SPAR CAP CHANGE IAW AD/CESSNA400/40 AMDT13 254.4 HOURS PREVIOUSLY.SDR P77A9700370Wheel Half · failedLEFT MAIN TIRE WENT FLAT ON TAXI OUT. REMOVED LEFT TIRE AND WHEEL ASSY. FOUND 5 INCHES OF INBOARD BEAD SUPPORT AREA OF WHEEL MISSING. SUSPECTED CAUSE OF DEFECT DUE TO AGE AND IMPROPER PROCEDURE OF DISMOUNTING TIRE, I.E., USING SCREWDRIVERS TO BREAK TIRE BEASDR AU971399Sight Glass · damaged(AUS) RH HYDRAULIC RESERVOIR SIGHT TUBE SPLIT AND LEAKING FLUID UNDER PRESSURE. HYDRAULIC CONTROL VALVE ALSO FOUND TO BE UNSERVICEABLE.SDR AU971637Engine · malfunction(AUS) RH ENGINE RUNNING ROUGH IN CRUISE. GROUND RUN COULD FIND NO FAULT.SDR 97ZZZX4797Brake Line · failedTHE LT MASTER CYLINDER BRAKE LINE CRACKED BECAUSE CONTINUAL FLEXING DURING BRAKING CAUSED THE LINE TO CRACK AT THE 180-DEGREE END.SDR 97ZZZX4251Channel · crackedDURING ROUTINE INSPECTION, TWO CHANNELS THAT SUPPORT THE NOSE LANDING GEAR ACTUATOR WERE FOUND CRACKED. AFTER REMOVING CHANNELS FOR REPLACEMENT, FORWARD SUPPORT ZEE P/N 5813045-1 WAS DISCOVERED CRACKED AND DAMAGED. AIRCRAFT HAD NO HISTORY OF PROBLEMS ASSOCIASDR 97ZZZX4331Rod End · brokeRIGHT LANDING GEAR DOOR CONTROL ROD BROKE AT ROD END, DOOR WOULD HANG DOWN WITH GEAR UP. INSTALLED NEW CONTROL ROD AND RIGGED. NO FURTHER TROUBLE.SDR 97ZZZX4003Crankcase · crackedCREW REPORTED OIL LEAK, RIGHT ENGINE. UPON FURTHER INSPECTION, FOUND 1.25 INCH TO 1.5 INCH LONG CRACK IN CRANKCASE JUST AFT OF NR 2 CYLINDER, SEVENTH STUD, LOCATED IN WEB BETWEEN OIL COOLER MOUNTING AREA AND CYLINDER ATTACH AREA.SDR CWTA064DUplock · crackedUPON RETRACTION OF LANDING GEAR, PILOT REPORTED LANDING GEAR CYCLING WITH UNSAFE LIGHT FLASHING. PILOT EXTENDED LANDING GEAR, ALL 3 GEAR LOCKED DOWN WITH 3 GREEN LIGHTS. LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTION REVEALED RIGHT MAIN UPLOCK CRACKED. (SDR 97ZZZX4144Gusset · crackedCRACKS FOUND IN PLT SEAT SUPPORT STRUCTURE BELOW FLOOR AT TOP SIDE OF GUSSETS. INBOARD AND OUTBOARD SUPPORT CRACKS WERE FOUND AT FLOOR LINE. SUBMITTER RECOMMENDS INSTALLING DOUBLERS INSIDE AT TOP AND AFT SIDES OF NEW GUSSETS OR MANUFACTURE GUSSETS OF HEAVIER
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