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 = '58' 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 = '58' 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 AU981075Rib · cracked(AUS) RIGHT MAIN LANDING GEAR DOOR RIBS AND ADJACENT STRUCTURE CRACKED.SDR AU981031Fitting · cracked(AUS) RT LOWER SPAR FITTING CRACKED.SDR 98ZZZX2808O-Ring · failedDROP OF APPROXIMATELY 800 RPM ON TAKEOFF. PHASING COIL O-RING ENTANGLED WITH FLYWEIGHT ASSEMBLY.SDR 98ZZZX3070Starter · failedSTARTER FAILED IN 8 DAYS OF SERVICE AND 29 HOURS FLIGHT TIME. ELECTROSYSTEMS OVH UNIT. WIRE BROKE INSIDE.SDR GLBR98101Support · brokeAFTER TAKE OFF PORT SIDE PASSENGER WINDOW SUPPORT BROKE. REMOVED /REPLACED PORT AND STARBOARD TORQUE TUBES AND ONE EACH EMERGENCY CATCH SUPPORT ON PORT (FORWARD) WINDOW IAW MANUFACTURER'S SPECS. PART TOTAL TIME: 7,570.7 HOURS. (X)SDR 98ZZZX3048Pump · failedPILOT NOTICED BURNING SMELL IN COCKPIT. TURNED OFF AVIONICS AND SMELL CONTINUED. PILOT NOTICED DOOR SEAL LIGHT WAS ILLUMINATED. SHUT OFF DOOR SEAL SYSTEM AND SMELL WENT AWAY. INSPECTION REVEALED PUMP BADLY DISTORTED AND MELTED. DROPPING RESISTOR WIRING MESDR 98ZZZX2802Starter · failedINSPECTION FOUND STARTER FAILED IN 45 DAYS AND 80-HOUR TIME IN SERVICE. ELECTRO SYSTEMS O/H UNIT.SDR 98ZZZX2801Alternator · failedREMOVED ALTERNATOR AT ENGINE CHANGE. FOUND SHAFT BEARINGS FAILED (DRIVE END), .1250 INCH MOVEMENT SIDE TO SIDE. UP AND DOWN. TIME IN SERVICE 215 HOURS. REMOVED JUST PRIOR TO FAILURE AND ENGINE DAMAGE. (ELECTRO SYSTEMS O/H UNIT).SDR AU980759Bulkhead · cracked(AUS) BULKHEAD LOCATED AT FS 257.6 CRACKED. PART TOTAL CYCLES: 4,996.SDR AU980758Pipe · cracked(AUS) RIGHT ENGINE CSU TO UNFEATHERING SYSTEM PIPE BROKEN AT CSU FITTING.SDR AU980711Mount · worn(AUS) ELEVATOR CONTROL SYSTEM BOB WEIGHTS LOOSE DUE TO P/N AN 960-416 WASHERS LOCATED UNDER THE HEAD OF THE WEIGHT ATTACHING BOLTS EMBEDDING THEMSELVES INTO THE WORN MOUNT. PART TOTAL CYCLES: 1,870.SDR AU980709Bushing · loose(AUS) NOSE LANDING GEAR UPPER DRAG BRACE RIGHT BUSHING LOOSE. PART TOTAL CYCLES: 1,870.SDR AU981248Insert · disintegrated(AUS) FUEL TANK FOAM INSERT MATERIAL DETERIORATED AND BLOCKING FUEL FILTER AND FUEL DRAINS. INSERT IS POST-MODIFICATION SB 2109 (AD/BEECH55/68).SDR 98ZZZX2623Drag Brace · failedNOSE GEAR UPPER DRAG BRACE (ORIGINAL TUBING STYLE) BROKE AT THE WELD FOR THE ACTUATOR ATTACHMENT POINT. APPEARS TO HAVE CRACKED AND FAILED FROM AGE STRESS AND POSSIBLE INTERIOR CORROSION. SUBMITTER STATED BEECHCRAFT OFFERS A NEW STYLE CASTING DRAG BRACE ASSESDR AU980824Bolt · broken(AUS) ENGINE CONNECTING ROD BOLT FAILED. PART TOTAL CYCLES: 1,315.SDR 98ZZZX2186Cylinder · crackedSEVENTY HOURS AGO, THIS ENGINE HAD TWO CRACKED CYLINDER HEADS. THE CRACKS WERE IN THE AREA BETWEEN THE TOP SPARK PLUG HOLE AND THE FUEL INJECTOR BOSS. THIS INSPECTION SHOWED ANOTHER CRACK. THE OPPOSITE ENGINE HAD FOUR CRACKED HEADS AT THIS TIME AND ONE CRACSDR 98ZZZX2185Cylinder · crackedSEVENTY HOURS AGO, THIS ENGINE HAD TWO CRACKED CYLINDER HEADS. THE CRACKS WERE IN THE AREA BETWEEN THE TOP SPARK PLUG HOLE AND THE FUEL INJECTOR BOSS. THIS INSPECTION SHOWED ANOTHER CRACK. THE OPPOSITE ENGINE HAD FOUR CRACKED HEADS AT THIS TIME AND ONE CRACSDR AU980551Bulb · failed(AUS) NOSE LANDING GEAR DOWNLOCK INDICATOR BULB BLOWN.SDR 98ZZZX2046Filter · brokenWHILE RUNNING AIRCRAFT BEFORE AN ANNUAL INSPECTION, NOTED THE LT GYRO PRESSURE WAS LOW. THE OWNER MENTIONED THE PRESSURE REGULATOR NEEDED TO BE ADJUSTED. INSPECTION OF THE PRESSURE SYSTEM FILTERS FOUND THE IN-LINE GYRO PRESSURE FILTER HAD A PIECE OF THE BODYSDR 99ZZZX705Crankcase · crackedENGINE CASE HAD A CATASTROPHIC FAILURE AROUND NR 4 CYLINDER IN-FLIGHT. POSSIBLE CAUSE - CASE FATIGUE.SDR 98ZZZX1460Bearing · failedDURING RANDOM CHECK FOR AIRCRAFT CONDITION, FOUND AIR CONDITIONING TENSIONING PULLEY BEARING DISINTEGRATED. PULLEY WAS HELD IN PLACE BY BELT. ALL BEARING BALLS WERE GONE. ONLY INNER AND OUTER RACE REMAINED. THIS IS SECOND PULLEY TO FAIL ON THIS AIRCRAFT INSDR 98ZZZX1658Receiver · burnedAIRCRAFT DEPARTED RIC. EN ROUTE, CREW NOTED BURNED ODOR AND THE NAV UNIT EMITTED SMOKE (A WHISP). CREW PULLED THE CIRCUIT BREAKER OF THE AFFECTED UNIT AND RETURNED TO RIC.SDR 98ZZZX1914Receiver · failedNAVIGATION RECEIVER CONVERTER FAILED CAUSING UNIT TO EMIT A BURNED ODOR IN THE AIRCRAFT COCKPIT AND UNIT DID SMOKE AT FAILURE. CREW PULLED THE CIRCUIT BREAKER AND RETURNED. NO PASSENGERS ON BOARD.SDR 98ZZZX1078Drive Coupling · failedSUBMITTER STATED ALTERNATOR DRIVE HAS NO TBO AND ON FAILURE OF THIS UNIT THE INTERNAL GEAR AND ENGINE OIL SUPPLY ARE FOULED WITH METAL AND DEBRIS WHICH COULD CAUSE A CATASTROPHIC ENGINE FAILURE. PART SHOULD HAVE LIFE-LIMIT. MEL SHOULD NOT ALLOW OPERATION WITSDR AU980300Doubler · cracked(AUS) LT TAILPLANE INBOARD RIB/REAR SPAR JOINT DOUBLER CRACKED.SDR AU980299Spar · cracked(AUS) ELEVATOR SPAR CRACKED ACROSS SPAR WEB IN AREA OF OUTBOARD HINGE ATTACHMENT. CRACK ORIGINATED AT THE HINGE ATTACHMENT BOLT HOLE AND PROPAGATED IN BOTH DIRECTIONS. FACTORY FITTED DOUBLER ALSO CRACKED.SDR AU980417Control Arm · misrigged(AUS) AILERON CONTROL SYSTEM RIGGED INCORRECTLY. THE AILERON BELLCRANKS WERE NOT HITTING THE STOPS AND THE AILERONS WERE SHORT OF TRAVEL BY FIVE DEGREES. PERSONNEL/MAINTENANCE ERROR.SDR AU980416Tube · damaged(AUS) LEFT LANDING GEAR DRIVE TUBE CREASED AT INBOARD FITTING (GEARBOX END). THE CREASE WAS RUSTED AND APPEARS TO HAVE BEEN DAMAGED SOME TIME AGO AND WAS CLOSE TO FAILURE.SDR AU980414Pipe · bulged(AUS) ENGINE EXHAUST PIPES (BOTH ENGINES) HAVE SEVERE BULGING. THREE OF THE FOUR PIPES HAVE IMPROPER PREVIOUS REPAIRS.SDR AU980176Hose · deteriorated(AUS) ALL ENGINE HOSES TIME EXPIRED. HOSES WERE NOT CHANGED DURING RECENT ENGINE CHANGE.SDR AU980175Exhaust System · damaged(AUS) EXHAUST ASSEMBLIES (3OFF4) DAMAGED DUE TO SEVERE BULGING.SDR AU980174Aileron · misrigged(AUS) AILERON CONTROL SYSTEM INCORRECTLY RIGGED.SDR AU980169Tube · damaged(AUS) LH LANDING GEAR DRIVE TUBE CREASED AT INBOARD FITTING.SDR 98ZZZX761Air Filter · mismarkedORDERED PARTS FROM BEECH DISTRIBUTOR FOR INDUCTION AIR FILTER PN 96-38005-1. TWO BOXES MARKED WITH SAME PART NUMBER, BUT FILTER PART NUMBER INSIDE IS P/N 35-380035-7. THIS IS NOW THE 10TH TIME RECEIVED MISMARKED PARTS FROM THE BEECH FACTORY AND DISTRIBUTORS.SDR AU980061Cover · separated(AUS) LH SPAR COVER SEPARATED AND JAMMED BETWEEN LANDING GEAR MICROSWITCHES.SDR 98ZZZX551Control Cable · failedPROPELLER CONTROL CABLE BROKE AT ENGINE END AT THE POINT WHICH THREADED END IS CRIMPED ON TO CABLE END.SDR AU980044Arm · cracked(AUS) NOSE LANDING GEAR RETRACT/EXTEND ARM CRACKED IN AREA WHERE THE ARM JOINS THE INPUT DRIVE BOSS.SDR 98ZZZX148Cylinder · failedDURING A FLIGHT JUST AFTER TAKEOFF, PILOT REPORTED THE ENGINE PERIODICALLY LOST POWER AND VIBRATED. UPON LANDING, PILOT ALSO NOTICED A CONSIDERABLE AMOUNT OF OIL ON THE NACELLE. UPON INVESTIGATION, DISCOVERED THE NR 6 CYLINDER PUSH ROD WAS BENT AND PUSH ROD SDR 97ZZZX5165Wire · shortedENGINE WOULD NOT STAR, HIGH AMP DRAW WITH RELAY ENGAGED. FOUND STARTER WIRE SHORTED AGAINST ENGINE MOUNT. TTAF: 381.8 HOURS. STARTER WIRES NEED TO BE INSPECTED AND TIED BACK.SDR AU971521Hinge · fractured(AUS) MAIN CABIN DOOR UPPER FORWARD HINGE FRACTURED AT THE HINGE BOLT HOLE. SUSPECT INITIATED BY INTERGRANULAR CORROSION DUE TO DISSIMILAR METAL CONTACT.SDR 97ZZZX5168Engine · failedLEFT ENGINE FAILED ON TAKEOFF OUT OF NEW ORLEANS. REMOVED AND REPLACED ENGINE. CAUSE UNKNOWN AT THIS TIME.SDR AU971431Actuator · broken(AUS) NOSE LANDING GEAR RETRACTION ACTUATOR AFT ATTACHMENT LUG BROKEN OFF.SDR 97ZZZX5170Gear Motor · malfunctionedBUF - GEAR WOULD NOT EXTEND. DID A GO-AROUND. GEAR FINALLY CAME DOWN. REMOVED AND REPLACED LANDING GEAR MOTOR AND DYNAMIC BRAKE RELAY. OPS CHECKS GOOD.SDR AU971502Wire · broken(AUS) NOSE LANDING GEAR INDICATOR ARM ACTUATING WIRE BROKEN.SDR AU971548Skin · cracked(AUS) ELEVATOR SKIN OUTBOARD OF THE RH TRIM TAB FOUND WITH SMALL CRACK. WITH FIRM FORCE APPLIED TO THE TRAILING EDGE, THE CRACK OPENED UP TO 127MM (5IN) IN LENGTH. CLOSER INSPECTION REVEALED SEVERAL MORE CRACKS. CRACKING WAS INITIATED BY CORROSION. SUSPECT SKSDR 97ZZZX5173Control Cable · out of adjON TAKEOFF OUT OF CEDAR RAPIDS, GOT BAD VIBRATIONS IN ELEVATOR YOKE MOVING BACK AND FORTH .25 INCH. CHECKED AND ADJUSTED ELEVATOR CABLES TO MFG SPECS. OPS CHECKS GOOD.SDR 97ZZZX4665Gear · failedLANDING GEAR WOULD NOT COME DOWN ELECTRICALLY OR MANUALLY. BELLIED AIRCRAFT IN. CAUSE UNKNOWN AT THIS TIME AS TO WHY GEAR WOULD NOT EXTEND.SDR 97ZZZX4667Tube Assy · chafedLEFT ENGINE LOST OIL. ENGINE SHUT DOWN, LANDED IN JOHNSTOWN, PA. FOUND HOLE CHAFED THROUGH UNFEATHERING ACCUMULATOR TUBE ASSY AT FIRE WALL. REMOVED AND REPLACED LINE, SERVICED ENGINE WITH OIL. OPS CHECKED GOOD.SDR 97ZZZX4666Door · openedON TAKEOFF OUT OF CHARLOTTE, NC, CLT, CABIN DOOR CAME OPEN, RETURNED TO CLT. MAINTENANCE INSPECTED DOOR, COULD NOT FIND ANY PROBLEMS. INSTALLED DOOR HANDLE KIT 35-5050-1P FOR PRECAUTIONARY MEASURES.SDR 97ZZZX4820Cylinder · failedPILOT REPORTED RIGHT ENGINE RUNNING ROUGH. INVESTIGATION FOUND NR 4 CYL HEAD SEPARATED FROM BARREL. THE CYLINDER HAD BEEN INSTALLED 148 HOURS BEFORE. RECENTLY OVERHAULED. TOTAL TIME ON CYLINDERS ARE NOT RECORDED. SUBMITTER RECOMMENDS THAT CYLINDERS BE SCR
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