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 = 'PA31' 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 = 'PA31' 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 CA000410034Wire · corroded(CAN) SMOKE AT NOSE OF AIRCRAFT AT START. MAINTENANCE GROUND BLOWER FAILED TO START. FURTHER INVESTIGATION FOUND A BROKEN WIRE INSIDE A BUTT SPLICE (AMP320559) IN A SPLICED SECTION OF THE WIRE HA8E CONNECTING LANDING GEAR SAFETY SWITCH TO WIRE H7CF IN WING SDR CA000330006Solenoid · stuck(CAN) PILOT REPORTED SLUGGISH GYRO OPERATION, FOUND LOW GYRO PRESSURE (3 PSI) ON BOTH ENGINES SELECTED OR SINGLE ENGINE OPERATION. UNABLE TO INCREASE PRESSURE. REMOVED VALVES (P/N 2H22-11) AND BENCH TESTED RESPECTIVE SOLENOIDS. SOLENOIDS FOUND TO BE PARTIASDR CA000322008Rod · damaged(CAN) PITCH CHANGE ROD INSTALLED UPSIDE DOWN AT SOME TIME PREVIOUS.SDR CA000329043Crankshaft · broken(CAN) CRANKSHAFT FOUND BROKEN AT COUNTERWEIGHT.SDR CA000301046Igniter · defective(CAN) IGNITORS WERE FOUND TO BE MISSING THE CERAMIC COATING WHICH IS REQUIRED TO PREVENT THE INGNITION LEAD SPRING FROM ARCING INSIDE THE LEAD BARREL. (FLASH OVER). AVIALL, AIRCRAFT HEATERS, API AND ELECTRO SYSTEMS ARE AWARE OF THE QA PROBLEM.SDR AU000209Structure · damaged(AUS) RIGHT FORWARD WING ATTACHMENT FITTING TO FUSELAGE UNDER TENSION. THE FUSELAGE IN THIS AREA BULGING AND CRACKING. INTERNAL STRESS DAMAGE AND CRACKING. CAUSE OF DAMAGE UNKNOWN.SDR CA000301049Line · frayed(CAN) DURING INSPECTION, WORN ALUMINIUM MANIFOLD AND OIL PRESSURE LINES WERE FOUND (PN''S 41918-00/4191-0). THE DEFECT WAS LOCATED BEHIND THE LEFT ENGINE FIREWALL AT THE LOWER BEND AS THEY GO INTO THE WING LEADING EDGE TO THE FUSELAGE. BOTH LINES WERE WORN SDR CA000215021Plug · cracked(CAN) IT WAS NOTICED THAT THE NOSE TIRE SEEMED TO BE LOW IN PRESSURE. UPON REINSTALLING NOSE WHEEL WITH NEW TUBE IT WAS NOTICED THAT THE LANDING GEAR AXLE PLUG WAS CRACKED - MOST LIKELY DUE TO OVER-TORQUE OF AXLE BOLT.BOTH AXLE PLUGS REPLACED.SDR CA000218003Gear · sheared(CAN) DURING FLIGHT, ENGINE STOPPED. IT WAS FOUND THAT THE CRANKSHAFT GEAR HAD FAILED. THE GEAR WAS STILL SECURELY FASTENED TO THE CRANK. AD 91-14-22.SDR CA000128054Brake · overheated(CAN) AIRCRAFT ARRIVED WITH BOTH BRAKES LEAKING AND DISCS WARPED. ASSEMBLY WAS INSTALLED JUNE 1/98.DISCOVERED WHEEL ASSY HAD P/N 40-102A SCRATCHED ON IT.THIS ASSEMBLY SHOULD HAVE HAD BRAKE P/N 30-68A (NOW SUPECEDED BY 30-68B) INSTALLED ALONG WITH DISC P/N 164SDR AU000128054Brake Disc · overheated(AU) AIRCRAFT ARRIVED WITH BOTH BRAKES LEAKING AND DISCS WARPED. ASSEMBLY WAS INSTALLED JUNE 1/98. DISCOVERED WHEEL ASSY HAD P/N 40-102A SCRATCHED ON IT. THIS ASSEMBLY SHOULD HAVE HAD BRAKE P/N 30-68A (NOW SUPECEDED BY 30-68B) INSTALLED ALONG WITH DISC P/N SDR CA000120015Engine · fire(CAN) FOLLOWING AN INSP & SERVICING, A/C WAS GROUND RUN.AFTER 3-4 MINS RT ENGINE WAS BROUGHT OUT OF IDLE & A LOUD BANG WAS HEARD.THE RT ENGINE & NACELLE WAS OBSERVED TO BE ON FIRE: BOTH ENGINES WERE SHUTDOWN & FUEL CUT-OFF CLOSED. ENGINE, TOGETHER WITH A HANGASDR CA000110097Rib · cracked(CAN) RUDDER TIP RIB AND FORWARD BRACING CHANNEL WERE FOUND TO BE CRACKED DURING A 1000 HR INSPECTION. CRACKS WERE FOUND AROUND THE NUTPLATES HOLDING THE BALANCE WEIGHT ON TOP OF THE RUDDER. HARDWARE SECURING THE WEIGHT BECAME LOOSE AND WAS UNDETECTED UNTIL SDR CA991231007Latch · binding(CAN) DURING FLIGHT, ABOUT 22:45 HRS. THE FRONT LEFT DOOR OPENED BY ABOUT 1.THE PILOTS CHECKED THE DOOR AFTER RETURNING TO SEPT-ILES. NO DEFECT FOUND, BUT NOTED THAT THE DOOR HANDLE HAD TO BE PUSHED ALL THE WAY TO REALLY LOCK THE DOOR. THERE IS NO SYSTEM TOSDR CA991231014Bracket · broken(CAN) WHEN THE PILOT TRIED TO LOWER THE WHEELS FOR LANDING, THE WHEELS DID NOT EXTEND. AFTER MANY ATTEMPTS AND TRYING WITH THE EMERGENCY PUMP, THE PILOT MOVED THE LEVER FROM BELOW THE INSTRUMENT PANEL.THE SUPPORT BRACKET OF THE SHAFT WAS FOUND UNSCREWED AND LSDR CA991231011Motor · intermittent(CAN) PILOT REPORTED LT COWL FLAP REFUSED TO OPEN IN FLIGHT. MAINTENANCE DISCOVERED ACTUATOR MOTOR OPERATING INTERMITTANTLY. MOTOR (DUKESP/N:5142-00-1; PIPER P/N475-194) REPLACED.SUBMITTER NOTED THAT ASSEMBLY DATE FOR UNSERVICEABLE PART WAS MARCH 10,1999.SDR CA991210093Crankshaft · failed(CAN) A SECTION OF THE CRANKSHAFT COUNTER WEIGHT LUG FAILED.SDR CA991112025Switch · failed(CAN) WHILE ON GROUND AND ENGINES RUNNING, HEATER WAS SELECTED ON. SMOKE AND SMELL EMANATED FROM UNDER THE INSTRUMENT PANEL. MASTER SWITCH TURNED OFF-NO SMOKE. RE-ATTEMPT MASTER ON - HEATER FAN STARTED BY ITSELF WITH HEATER SWITCH TURNED OFF PILOT FELT SWSDR CA991208072Line · loose(CAN) OIL PRESSURE LINE LOOSE AFTER TAKEOFF AS NOTED BY OIL ON LEFT COWLING. AIRCRAFT RETURNED FOR LANDING (APPROXIMATELY 3 MINUTE FLIGHT). ENGINE SHUT DOWN AFTER LANDING.SDR CA991104014Switch · failed(CAN) AFTER TAKEOFF, THE LANDING GEAR WAS SELECTED UP, THE GEAR HANDLE RETURNED TO NEUTRAL, BUT THE RED UNSAFE LIGHT REMAINED ILLUMINATED. THE LEFT DOOR MICROSWITCH WAS FOUND DEFECTIVE.SDR CA991027073Spring · broken(CAN) AD 98-08-18 ELEVATOR DOWN SPRING REPLACEMENT JULY 03/98 AT 14,302 TAFT. INSPECTION OF SPRING DURING NORMAL INSPECTION REVEALED ODD WEAR/DAMAGE TO SPRING END. CAUSE UNKNOWN.SDR CA991008005Selector · broke(CAN) WHEN ON APPROACH, PILOT SELECTED WING FLAPS, SELECTOR HANDLE BROKE OFF CLOSE TO PIVOT POINT. INSPECTION SHOWS 40 PERCENT DIAMETER OF STEM SHOWS INTERNAL CORROSION; THUS, WEAKENING THE STEM. KNOB P/N: 23943-00. PIPER SWITCH ASSY P/N: 487-839 REPLACESDR CA991004054Pump · failed(CAN) FUEL PRESSURE BELOW SPECIFICATIONS.SDR AU990946Nut · worn(AUS) PITCH CONTROL ROD END LOCKNUT VIBRATED LOOSE CAUSING DISCONNECTION OF THE PITCH CONTROL CABLE. INVESTIGATION FOUND THE LOCKING FUNCTION ON THE NUT WAS NON-EXISTENT.SDR CA991004019Stud · broken(CAN) CYLINDER STUDS FAILED.SDR CA991004056Bracket · cracked(CAN) BRACKET IMPROPERLY INSTALLED.SDR CA990927019Spring · cracked(CAN) INSPECTION CARRIED OUT IN ACCORDANCE WITH ALERT AL 99-04. FOUND SPRING CRACKED AT ATTACH LOOP.SDR AU990957Crankcase · cracked(AUS) CRANKCASE CRACKED ON FRONT RIGHT SIDE BELOW THE CYLINDER. CRACK LENGTH 50.8 MM (2 IN)CHES).SDR CA990907018Mount · broken(CAN) TURBO MOUNT BROKEN.SDR CA990907017Cylinder · cracked(CAN) CRACKED CYLINDER BETWEEN SPARK PLUG AND EXHAUST PORT.SDR CA990907041Spring · cracked(CAN) DURING A ROUTINE INSPECTION OBSERVED SOME SMALL MINUTE CRACKING AROUND THE RADIUS OF EACH HOOK END. SPRING AND LINK CHANGED OUT WITH NEW, OLD SPRING TAGGED AND PLACED IN QUARANTINE.SDR CA990817044Radio · failed(CAN) NR 2 COM SET KX175B (A LOANER UNIT) WENT DEAD. AIRCRAFT IS USUALLY OPERATING WITH A MAC 1700 (KX175B + DIGITAL). AVIONICS SHOP ADVISED THAT TROUBLE ORIGIN APPEARS TO BE A FAILING INTERCOM SYSTEM AND AUDIO PANEL DUE TO UNPROFESSIONAL WIRING SHOWING BEHISDR CA990812011Bracket · cracked(CAN) LEFT MAIN LANDING GEAR INBOARD GEAR DOOR NOT SITTING FLUSH - HANGING DOWN ABOUT .50 INCH. FURTHER INVESTIGATION REVEALED THAT THE UPPER ATTACHMENT BRACKETS FOR INBOARD GEAR DOOR ACTUATOR WERE CRACKED THROUGH. NEW BRACKETS INSTALLED . P/N'S 46357-000 ASDR CA990804009Controller · stuck open(CAN) MANIFOLD PRESSURE LOST, PILOT RETARDED THROTTLE TO IDLE THEN RESET THROTTLE POWER. THE PROBLEM WENT AWAY. DIFFERENTIAL CONTROLLER CHANGED, SUSPECTED DEBRIS IN VALVE PORT IN CONTROLLER.SDR CA990719038Heat Shield · damaged(CAN) REFERENCE: IPC FIG 82 ITEMS 23, 29, AND 57. DURING 50 HR INSPECTION FOUND SHIELD P/N 41604-01 WITH 6 CHERRY MAX RIVETS PULLED OUT WHICH SECURES HEAT SHIELD TO SKIN P/N 41667-08 AND ANGLE P/N 40667-1 ON RT NACELLE. HEAT SHIELD SHOWS TO HAVE BEEN EITHESDR AU990765Handle · broken(AUS) LANDING GEAR EMERGENCY HAND PUMP LEVER BROKEN. CAUSED BY OVER EXTENSION OF LEVER DURING OPERATION OF THE PUMP.SDR AU990764Downlock · contaminated(AUS) LEFT MAIN LANDING GEAR DOWNLOCK HOOK CONTAMINATED WITH MUD AND DIRT PREVENTING ACTUATION OF MICROSWITCH.SDR CA990715048Wire · broken(CAN) RIGHT ALTERNATOR WENT OFF-LINE AND THE AIRCRAFT STARTED TO LOSE NAVIGATIONAL AIDS. CREW DISCOVERED NO CHARGE FROM ALTERNATOR. THE AMP TERMINAL END WAS REPLACED AT THE FIELD TERMINAL FOR THE RIGHT ALTERNATOR AND BOTH ALTERNATOR BELTS TIGHTENED.SDR AU990458Hub · cracked(AUS) PROPELLER HUB CRACKED IN THREADS OF GREASE NIPPLE HOLE.SDR AU990402Bracket · misinstalled(AUS) RIGHT ENGINE IDLER PULLEY TOP MOUNT BRACKET CRACKED UNDER THE LOCKWIRE. THE IDLER PULLEY WAS ALSO MOUNTED ON THE INCORRECT SHAFT (PN 19760) INSTEAD OF THE CORRECT PN LW-19237 CAUSING APPROXIMATELY 2.54 MM (0.1 INCH) MISALIGNMENT OF THE ALTERNATOR BOLT.SDR CA990401003Gear · worn(CAN) ON INSPECTION, ALUMINUM FLAKES WERE FOUND IN THE OIL FILTER ON THE NR 2 ENGINE. INVESTIGATION FOUND THE LEFT HAND MAGNETO LOOSE DUE TO BEARING SHAFT WEAR. THIS ALLOWED THE DRIVE GEAR TO TILT AND CONTACT THE ENGINE CASE CAUSING ALUMINUM TO WEAR AWAY ANDSDR CA990330081Uplock · dirty & rusty(CAN) LEFT HAND LANDING GEAR HOOK FAILED TO MOVE INTO POSITION ON RETRACTION AFTER TAKEOFF. INVESTIGATION FOUND ACCUMULATED DIRT AND RUST ON THE UPLOCK ROD, TELESCOPIC END, UNDER THE DUST BOOT, CAUSING SLUGGISH OPERATION OF UPLOCK HOOK. IT IS TO BE NOTED THASDR CA990401011Turbocharger · leaking(CAN) ON LANDING OIL SEAL LEAK FROM TURBOCHARGER IGNITED. WHEN THE ENGINE WAS RETARDED TO IDLE, THERE WAS NO DAMAGE TO THE AIRCRAFT OR ENGINE COMPONENTS.SDR CA990330079Propeller Assy · misoverhauled(CAN) THE SUBMITTER SCRAPPED THIS PROPELLER AND A NEW PROPELLER WAS TAKEN INTO SERVICE. THE SUBMITTER REPORTS THAT THE PREVIOUS OVERHAUL WAS LOW COST AND QUESTIONABLE PARTS WERE REINSTALLED. SINCE THAT OVERHAUL, ROTATIONAL PLAY IN THE BLADES WAS REPORTED AND SDR CA990318025Bulkhead · cracked(CAN) LIP OF BACK PLATE CRACKED.SDR CA990318024Detector · failed(CAN) WHEN FLYING THROUGH MOISTURE, THE STALL WARNING WOULD CHIRP POSSIBLY SHORTING OUT.SDR CA990318023Gauge · malfunctioned(CAN) WHEN FULL, THE FUEL GAUGE WOULD READ 3/4.SDR CA990310036Turbocharger · seized(CAN) DURING CLIMB-OUT, THE NR 2 ENGINE BEGAN TO LOSE POWER AND WENT NORMALLY ASPIRATED. THE AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT. POST-FLIGHT INSPECTION REVEALED THE TURBOCHARGER HAD FAILED. THE TURBOCHARGER WAS REPLACED AND THE AIRCRAFT RETURNED TOSDR CA990318029Caliper · corroded(CAN) WALLS INSIDE CALIPERS CORRODED BEYOND LIMITS.SDR CA990224016Bolt · failed(CAN) THREE LANDING GEAR BOLTS FOUND BROKEN AND 2 OTHERS FOUND LOOSE ON THE DIRECTION ARM.
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