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 20000907SH039Tire · unserviceableCREW REPORTED UNUSUAL NOISE ON TAXI. FOUND CHUNK OF AFT TIRE MISSING. MAINTENANCE DISPATCHED TO CHANGE TIRE. FOUND LARGE PORTION OF RECAP HAD SEPARATED FROM CORE TIRE. MAINTENANCE REMOVED AND REPLACED TIRE AND RELEASED AIRCRAFT BACK INTO SERVICE. (X)SDR 20000808SH014Pin · destroyedON LANDING, AFT BRAKE LOCKED UP, AND MAIN WHEEL SEIZED. MAINTENANCE FOUND ONE CALIPER ANCHOR PIN SHEARED. REMOVED AND REPLACED MAIN WHEEL ASSY, BRAKE CALIPER, AND BRAKE BACKPLATE ASSY, THEN RETURNED AIRCRAFT TO SERVICE. AT THIS TIME, ALL ANCHOR PINS ARE BEISDR 20000721SH032Drag Brace · crackedON PRE-FLIGHT, CREW FOUND SUSPECTED CRACK AT DRAG BRACE TO ACTUATOR ATTACH LUG AREA. MAINTENANCE PERFORMED NDT. FOUND TO BE CRACKED AT SUSPECTED AREA. REMOVED AND REPLACED DRAG BRACE AND ROD END (PN ADNE4JW) WITH NEW AND RETURNED AIRCRAFT TO SERVICE. (X)SDR AU000443Pipe · cracked(AUS) LEFT HYDRAULIC FILTER HOUSING PRESSURE PIPE SPLIT AT OUTBOARD RADIUS OF BEND. LOSS OF HYDRAULIC FLUID.SDR AU000426Fuel Tank · fod(AUS) RIGHT WING FUEL TANK FOD. ON REMOVAL OF THE RIGHT WING FUEL TANK ACCESS PANEL, A PIECE OF RAG MEASURING APPROXIMATELY 300 MM BY 300 MM (11.8 INCHES BY 11.8 INCHES) WAS FOUND IN THE BOTTOM OF THE TANK COVERING ONE FUEL TANK FLOW VALVE AND THE MAIN FUEL SSDR 20000907SH038Bearing · destroyedPILOT REPORTED LOSS OF POWER ON TAKEOFF. MAINTENANCE FOUND PROPELLER GOVERNOR LEAKING OIL AND CONFIRMED POWER LOSS. CHANGED GOVERNOR AND RETURNED AIRCRAFT TO SERVICE. TEAR DOWN OF GOVERNOR REVEALED INTERNAL FAILURE CAUSED BY BEARING FAILURE. (X)SDR 20000531SH023Bearing · groovedRELEVANT INDICATION IN BEARING GROOVE. (X)SDR AU001274Trunnion · cracked(AUS) MAIN LANDING GEAR FORWARD TRUNNION CRACKED IN THE TOP WEB ADJACENT TO THE GEAR ATTACHMENT BEARING. FOUND DURING FLUORESCENT DYE PENETRANT INSPECTION IAW MEB85-11 R4.SDR AU001272Trunnion · cracked(AUS) RT MAIN LANDING GEAR FORWARD TRUNNION CRACKED ON THE TOP WEB ADJACENT TO THE GEAR ATTACHMENT BEARING. FOUND DURING FLUORESCENT DYE PENETRANT INSPECTION IAW MEB85-11 R4.SDR AU001271Strut · cracked(AUS) RT MAIN LANDING GEAR UPPER BARREL ASSEMBLY CRACKED ON THE INNER RADIUS OF THE TORQUE LINK COLLAR LUG. FOUND DURING FLUORESCENT MAGNETIC PARTICLE INSPECTION (MAGNAFLUX) IAW MEB89-2 R1.SDR AU000444Pipe · cracked(AUS) RIGHT HYDRAULIC FILTER PRESSURE PIPE SPLIT AND LEAKING AT OUTBOARD RADIUS. LOSS OF HYDRAULIC FLUID.SDR AU000259Piston · failed(AUS) NR 2 CYLINDER PISTON HOLED.SDR AU000228Bushing · contaminated(AUS) EMERGENCY LANDING GEAR BLOW DOWN BOTTLE HANDLE WOULD NOT OPERATE. INVESTIGATION FOUND THE TEFLON BUSHING LOCATED BETWEEN THE FIRING PLUNGER AND THE OUTLET LINE BLOCK WAS SWOLLEN AND JAMMED PREVENTING THE BOTTLE FROM FIRING. OIL CONTAMINATION WAS FOUND SDR 20000508SH024Flyweight · crackedRELEVANT CRACK INDICATION ON BASE OF FLYWEIGHT DISC. (X)SDR AU000137Structure · fractured(AUS) NOSE LANDING GEAR NACELLE STRUCTURE FAILED IN THE AREA OF THE UPPER ACTUATOR ATTACHMENT POINT. NLG COLLAPSED DURING LANDING CAUSING DAMAGE TO THE SURROUNDING STRUCTURE AND BOTH PROPELLERS. SUSPECT STRUCTURE HAD BEEN DAMAGED FOR SOME TIME BEFORE FINAL FSDR CA000320011Valve · inoperative(CAN) AFTER TAKEOFF, THE LANDING GEAR WAS SELECTED UP AND THE GEAR IN TRANSIT LIGHT FAILED TO EXTINGUISH. THE PILOT SELECTED THE GEAR DOWN AND FAILED TO GET A SAFE GEAR DOWN INDICATION (3 GREEN LIGHTS). THE GEAR SELECTOR SWITCH WAS LEFT IN THE DOWN POSITION ANSDR 20000331SH005Resistor · failedCREW TURNED ON HEATER PRIOR TO DEPARTURE FROM HYA. ON CLIMB-OUT, PILOT NOTICED FUNNY SMELL, TURNED OFF HEATER. PASSENGERS INFORMED CREW OF SMOKE IN CABIN. RETURNED TO HYA FOR UNEVENTFUL LANDING. MAINTENANCE FOUND HEATER FAN DROP RESISTOR BURNED. REMOVED ASDR P77A9902726Engine · making metalRIGHT ENGINE SHUT DOWN AFTER TURNING ONTO TAXIWAY AFTER LANDING. PILOT COULD NOT RESTART ENGINE. AFTER PARKING, PILOT NOTICED OIL ON COWLING AND WING. INSPECTION FOUND OIL LEAK IN VICINITY OF CYLINDERS 2 AND 4. ALSO, FOUND HEAVY METAL CONTAMINATION IN OIL.SDR 99ZZZX4609Drag Brace · failedNOSE GEAR DRAG BRACE, P/N 5142002-5, (NEW, HEAVY DUTY STYLE), FAILED ON GEAR EXTENSION APROXIMATELY ONE INCH AFT OF THE NOSE GEAR ACTUATOR ROD END ATTACH LUG. AIRCRAFT LANDED WITH MINOR DAMAGE TO THE NOSE AREA OF THE AIRCRAFT.SDR 99ZZZX4606Wastegate · lack of lubeTHE RIGHT ENGINE DID NOT DEVELOP FULL POWER FOR TAKEOFF. INSPECTED ENGINE AND CONTROLLER AND WASTEGATE. LUBED WASTEGATE VALVE SHAFT. GROUND RUN-UP CHECKED GOOD. NO OCCURRENCE SINCE THEN.SDR CA990927048Control Cable · broken(CAN) DURING PRE-FLIGHT INSPECTION, FLAPS WERE EXTENDED AND WOULD NOT RETRACT. PROBLEM WAS TRACED TO A BROKEN FLAP PRESELECT/FOLLOW-UP CABLE UNDER CABIN FLOOR.SDR AU990929Pipe · cracked(AUS) LEFT MAIN LANDING GEAR HYDRAULIC PIPE CRACKED ON THE BEND OF THE PIPE. CRACK LENGTH 15 MM (0.590 INCH). LOSS OF HYDRAULIC FLUID.SDR 99ZZZX3741Bracket · brokenON RT ENGINE START, PILOT NOTICED SMOKE FROM RT COWL, SHUT DOWN ENGINE PER NORMAL PROCEDURE AND EVACUATED PASSENGERS. MAINTENANCE FOUND ALTERNATOR POWER CABLE CHAFED BY BROKEN ENGINE BAFFLE BRACKET. REPAIRED BRACKET, REPAIRED MINOR COWL DAMAGE, AND ALTERNATOSDR 99ZZZX4252Circuit Breaker · failedCREW DECLARED EMERGENCY EN ROUTE ACK/BOS WHEN SMOKE CAME FROM AFT SIDE PANEL AFTER RE-SETTING AVIONICS MASTER SWITCH, FOR AVIONICS FAILURE. USING EMERGENCY AVIONIC SWITCH, RESUMED COMMUNICATIONS WITH BOS. APPROACH, LANDED WITHOUT INCIDENT. MAINTENANCE REPLASDR 99ZZZX3400Solenoid · stuckDURING FIGHT, PILOT REPORTED SMOKE IN THE COCKPIT AND RETURNED TO AIRPORT FOR AN UNEVENTFUL LANDING. THE MAINTENANCE DEPARTMENT WAS DISPATCHED. POSSIBLE CAUSE WAS HYDRAULIC MANIFOLD SOLENOID STUCK AND CAUSED SYSTEM TO OVERHEAT CAUSING A PIN HOLE IN THE HYDRASDR AU990677Wheel · cracked(AUS) WHEEL HALF BEAD SECTION CRACKED AND SEPARATED. LENGTH OF SEPARATED SECTION APPROXIMATELY 152.4 MM (6 INCHES).SDR 99ZZZX2933Bracket · wrinkledDURING A ROUTINE INSPECTION, MECHANIC FOUND THAT MOUNT BRACKET P/N'S 5654111-1 AND 5654111-2 WERE WRINKLED. MOUNT ASSEMBLY WAS DISASSEMBLED AND INSPECTED. NO OTHER DAMAGE WAS FOUND. DAMAGE CAUSE UNKNOWN.SDR 99ZZZX2507Line · crackedDURING A RETURN FLIGHT, LEFT AND RIGHT HYDRAULIC FLOW LIGHTS BEGAN TO FLICKER ON AND OFF. CYCLED GEAR DOWN AND MADE AN UNEVENTFUL LANDING. MAINTENANCE PERSONNEL FOUND HYDRAULIC RESERVOIR EMPTY. PERFORMED HYDRAULIC PRESSURE CHECK AND FOUND L-H PRESSURE LINE,SDR 99ZZZX3267Drag Brace · crackedNOSE LANDING GEAR DRAG BRACE CRACKED AT REAR ATTACH POINT CAUSING COLLAPSE OF NOSE GEAR ASSEMBLY DURING TAXI. (X)SDR 99ZZZX2512Engine · failedIN CRUISE FLIGHT, RIGHT ENGINE HAD A CATASTROPHIC FAILURE. FOR UKNOWN REASONS, CONNECTING RODS, NR 1, NR 2, NR 4, FAILED. TCM HAS BEEN NOTIFIED AND WILL INSPECT ASAP. AN UNEVENTFUL LANDING WAS MADE.SDR AU991064Trunnion · faulty(AUS) LEFT MAIN LANDING GEAR TRUNNION ASSEMBLY ACTUATOR ATTACHMENT LUG CONTAINED A FAULT LINE. CONFIRMED USING DYE PENETRANT AND EDDY CURRENT INSPECTIONS.SDR CA990907044Spring · broken(CAN) STICKING VALVES AND BROKEN VALVE SPRING.SDR AU990443Drag Brace · fractured(AUS) NOSE LANDING GEAR DRAG BRACE FRACTURED.SDR AU990367Buckle · broken(AUS) SEAT BELT BUCKLE LOCKING MECHANISM SPRING BROKEN.SDR AU990318Cable · failed(AUS) LANDING GEAR EMERGENCY EXTENSION SYSTEM ACTUATOR CABLE ASSEMBLY SLIPPING UNDER THE CABLE CLAMP PREVENTING ACTIVATION OF THE NITROGEN BLOW-DOWN BOTTLE. DURING AN EXTENSION PROBLEM WITH THE LANDING GEAR, THE EMERGENCY UNDERCARRIAGE EXTENSION HANDLE WAS PUSDR 99ZZZX1745Circuit Breaker · failedAFTER LANDING IN ACK, CREW SHUT OFF ALL EXTERNAL LIGHTS EXCEPT BELLY STROBE AND NAV LIGHTS. NOTICED SMOKE COMING FROM NAV LIGHT SWITCH/BREAKER. SHUT OFF SWITCH, TAXIED TO GATE, AND NOTIFIED MAINTENANCE. FOUND RT WING NAV LIGHT POWER WIRE SHORTED TO GROUND, SDR AU990303Switch · faulty(AUS) LEFT HYDRAULIC SYSTEM PRESSURE SWITCH FAULTY.SDR 99ZZZX1459Cylinder · leakingDURING ROUTINE ENGINE, 100-HOUR INSPECTION FOUND CYLINDER NR 3 COMPRESSION 15/80 LEAKING BY INTAKE VALVE AND RINGS.SDR 99ZZZX2100Cap · leakingCREW REPORTED FUEL/FUEL PUDDLE ON COCKPIT FLOOR ON THE FIRST OFFICER'S SIDE. DIVERTED TO HYA EN ROUTE FROM BOS TO ACK. MAINTENANCE COULD NOT CONFIRM PUDDLING OF FUEL. FOUND FUEL STAIN (BLUE DYE) ON FUEL FLOW BLEEDER LINE ASSY. TIGHTENED AN 929-2 CAP. C/W SDR AU991099Split Pin · failed(AUS) ELEVATOR TRIM TAB DISCONNECTED FROM TRIM JACK. INVESTIGATION FOUND THAT THE SPLIT PIN HAD SEPARATED ALLOWING THE NUT, WASHER AND BOLT TO VIBRATE FREE SEPARATING THE ACTUATING ROD FROM THE TRIM JACK.SDR AU990128Strut · cracked(AUS) MAIN LANDING GEAR STRUTS CRACKED. EXCESSIVE PLAY IN TORQUE LINKS AND WHEEL MISALIGNMENT WAS ALSO FOUND. PART TC: 9,597.SDR AU990034Pipe · cracked(AUS) DURING LANDING, THE PILOT NOTED A STRONG HYDRAULIC OIL SMELL. INVESTIGATION FOUND THE HYDRAULIC PRESSURE LINE LOCATED IN THE AREA BEHIND THE RIGHT ENGINE FIREWALL WAS TWISTED AND SPLIT. THE ELBOW FITTING P/N AN837-6 WAS LOOSE IN THE FIREWALL AND TIGHTESDR AU990022Lug · cracked(AUS) WHILE CHARGING THE LEFT LANDING GEAR STRUT, IT WAS NOTICED THAT THE RETRACT LUG ON THE STRUT P/N 5141103-13 EXHIBITED SIGNS OF CRACKING. A DYE PENETRANT CHECK CONFIRMED THE DEFECT. PART TC: 32.SDR 99ZZZX538Slinger · missingDURING PHASE INSPECTION, DIQSCOVERED L.E. LEFT MAGNETO HAD OIL INTERNALLY. DISSAMBLED MAGNETO IAW OM. FOUND OIL SLINGER WAS NOT INSTALLED.SDR 99ZZZX644Fuel Pump · leakingAFTER TAKEOFF, CREW TURNED ON AIRCRAFT HEATER, CABIN FILLED WITH FUEL ODOR. CREW TURNED OFF HEATER, VENTED CABIN AND RETURNED TO BASE. MAINTENANCE FOUND HEATER FUEL PUMP PARTING HALVES LOOSE. RE-TORQUED HARDWARE AND RE-INSTALLED PUMP HOUSING COVER. RETURNESDR CA990202004Oil Cooler · failed(CAN) OIL COOLER (P/N 649479) WAS DELIVERED AND INSTALLED WITH AN OVERHAULED ENGINE. AS WINTER APPROACHED THE ENGINE OIL TEMPERATURE, DURING CRUISE, BEGAN TO DROP. WITH AMBIENT AIR TEMPERATURE -20 DEGREES CELSIUS, THE ENGINE OIL TEMPERATURE WAS BELOW THE BOTSDR AU981666Bolt · separated(AUS) LEFT MLG CENTER TORQUE LINK BOLT DETACHED.SDR AU981557Engine · making metal(AUS) ENGINE FILTERS CONTAINED A LARGE AMOUNT OF METAL CONTAMINATION. LIMITED INFORMATION PROVIDED.SDR AU981443Strut · cracked(AUS) LEFT MAIN LANDING GEAR STRUT CRACKED IN AREA OF TORQUE LINK ATTACHMENT. CRACK CONFIRMED USING DYE PENETRANT INSPECTION. PART TC: 10,036.SDR AU981442Strut · cracked(AUS) RIGHT MAIN LANDING GEAR STRUT CRACKED IN AREA OF TORQUE LINK ATTACHMENT. CRACK CONFIRMED USING DYE PENETRANT INSPECTION. PART TC: 10,036.
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