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 CA050429002Cylinder · separatedLOSS OF RIGHT ENGINE POWER IN-FLIGHT. UNSCHEDULED LANDING, NR 3 CYLINDER SEPARATED. THE 58 STUDS BROKE. ENGINE REPLACED BY LYCOMING TIO540A2B, S/N R11946-61, DUAL INSPECTION OF CONTROLS DONE.SDR CA050408011Magneto · burned(CAN) RT ENGINE PARTIAL FAILURE ON CLIMB-OUT. RPM, MP, FF, FP EXCESSIVE DROPS. TROUBLE SHOOTING FOUND THAT LT MAGNETO FAILED. NEW MAGNETO INSTALLED. A/C TEST FLOWN, SATISFACTORY TEST FLIGHT. U/S MAGNETO SENT OUT FOR O/H. TEAR DOWN FOUND POINTS BURNT. DISDR AU510002090Governor · failedRT ENGINE PROPELLER GOVERNOR COUPLING GEAR PNO A-3181 DRIVE TEETH (8OFF) SHEARED.SDR CA050223005Switch · defective(CAN) HEATER GROUND FAN NOT WORKING AFTER LANDING, HEATER SYSTEM CHECK AND FOUND DEFECTIVE WIRE (OPEN) FROM LT LANDING GROUND SWITCH. THE OTHER SYSTEM WASN'T AFFECTED.SDR CA050130001Bolt · failed(CAN) WHEN THE NOSE WAS LOWERED DURING LANDING, A SEVERE VIBRATION DEVELOPED WHEN THE NOSE TIRE TOUCHED THE RUNWAY. STEERING WAS NOT AVAILABLE BUT DIRECTIONAL CONTROL WAS MAINTAINED WITH RUDDER. AS THE AIRCRAFT SLOWED, THE VIBRATION EASED UP. TURNING TO EXITSDR CA050121008Alternator · shorted(CAN) AN INTERNAL SHORT IN THE ALTERNATOR CAUSED THE VOLTAGE REGULATER CIRCUIT BREAKER TO POP. DUE TO THE DESIGN OF THE SYSTEM, THE FAILURE WAS NOT ISOLATED TO THE FAILED SIDE. THE PILOT TURNED OFF ALL ELECTRIC DEVICES AND LANDED AT THE NEAREST AIRPORT. THESDR CA050106003Pump · cracked(CAN) TOOK OFF, ENROUTE, AIRCRAFT WAS ON A BASE RELOCATION FLIGHT. PILOT HAD GEAR IN-TRANSIT LIGHT FOR LONGER THAN NORMAL AFTER GEAR WAS SELECTED UP. RE-SELECTED GEAR DOWN AND LOCKED 3 GREEN. RE-SELECTED GEAR UP AND STILL HAD IN-TRANSIT LIGHT. CONTINUED WISDR CA050105004Engine · failed(CAN) AFTER TAKEOFF THE LT ENGINE ENCOUNTERED RPM FLUCTUATIONS, THE AIRCRAFT RETURNED TO THE AIRPORT. AFTER SOME DISCUSSION WITH THE MECHANICS, THE PILOTS DRAINED THE AIRCRAFT AGAIN AND CARRIED OUT A GROUND RUN. EVERYTHING RETURNED TO NORMAL. THE AIRCRAFT DEPASDR CA041222012Bolt · mismanufactured(CAN) WHEN REINSTALLING THE HORIZONTAL STAB, (AT THE AFT SPAR ATTACH POINT) USING NEW HARDWARE, IT WAS DISCOVERED THAT THE REQUIRED BOLTS WERE LONGER IN TOTAL LENGTH BY 0.1875 AND SHANK LENGTH BY 0.1875, THAN THE ORIGIONAL BOLTS REMOVED. THIS CAUSED THE NUTS SDR CA050110004Circuit Breaker · damaged(CAN) AC WAS RETURNING WHEN RT ALT WENT OFF-LINE, 5 MIN LATER LT ALT SYS WENT OFF-LINE. BATTERY, LT ALT, BOTH VOLT REG, LT OVER-VOLT RELAY, LT VOLT REG CB WERE REPLACED. NO TEST FOR OVER-VOLT RELAY SPECIFIED IN MM, IN ELEC SYS OF MM A 500 HOUR OVER-VOLT RELASDR CA041119009Magneto · cracked(CAN) MAGNETO WAS REMOVED AT ENGINE REMOVAL. MAG WAS SENT IN BECAUSE THE OIL SLINGER RING WAS NOT IN THE GROOVE. TEAR DOWN RESULTED IN THE FOLLOWING FINDINGS, WIRE ROUTING INCORRECT, LEAD WEARING ON COM SCREW, COIL LEAD NOT POSITIONED CORRECTLY, TUBING MISSINSDR 2005FA0000121Bearing · failedRT REAR MAIN BEARING BEGAN TO SHRED METAL INTO OIL FILTER AFTER LANDING. OIL CHANGE AND FILTER CUT OPEN. THIS WAS FOUND ON A PRE-BUY. LETTER TO FAA SENT SEPT 03, 2005, BUT NO REPLY. (K)SDR CA040830014Control Rod · cracked(CAN) ON INSPECTION, FOUND THE RT AILERON CONTROL ROD CRACKED ON THE OUTER THREADED PORTION OF THE ROD WHERE THE ROD END THREADS INTO THE ROD. THE CRACK WAS APPROXIMATLEY 1 INCH IN LENGTH LONGITUDINALY WITH THE ROD.SDR CA040831008Bolt · seized(CAN) WHEN THE PILOT SELECTED GEAR DOWN, THE RT GEAR LIGHT DID NOT ILLUMINATE.AFTER NUMEROUS RETRACTIONS AND EXTENSIONS NEAR THE AIRPORT, THE LIGHT NEVER CAME ON. AFTER LANDING THE RT DOWNLOCK HOOK WAS NOT COMPLETELY ENGAGED. WERE MOVED THE BOLT AND REPLACED WSDR 2004F00235Downlock · dirtyTHE RT MAIN LANDING GEAR COLLAPSED AFTER TOUCH DOWN, SUSPECT DIRTY GEARS WITH GRIT ON DOWNLOCK. ALSO AIRCRAFT HAD BEEN OUT OF SERVICE FOR 5 WEEKS AND RUST HAD ACCUMULATED ON DOWN LOCK. (EA05200405925)SDR G1I2004F00002Belt · displacedAIRCRAFT LOST ELECTRICAL POWER. FOUND RT ENGINE ALTERNATOR BELT NOT ON THE PULLEY SYSTEM. REINSTALLED AND CORRECTLY TENSIONED ALTERNATOR BELT, OPS CHECK OF ELECTRICAL SYSTEM GOOD. PROBABLE CAUSE IS IDLER PULLEY BECAME LOOSE ALLOWING THE ALTERNATOR BELT TO JSDR G1I2004F00001Wire · brokenAIRCRAFT LOST ELECTRICAL POWER. FOUND FIELD WIRE BROKEN AT RING TERMINAL WHERE WIRE ATTACHES TO LT ALTERNATOR. INSTALLED NEW RING TERMINAL ON WIRE AND REATTACHED TO ALTERNATOR. PROBABLE CAUSE OF FAILURE IS AGE AND VIBRATION. RECOMMENDED DETAILED INSPECTIONSDR CA040719005Magneto · wornOIL LEAK WAS DISCOVERED AT MAGNETO MOUNTING FLANGE GASKET. UPON REMOVAL OF UPPER AND LOWER MAGNETO MOUNT CLAMPS (P/N 66M19385), WEAR AND FRETTING OF THE MAGNETO MOUNTING FLANGE WAS DISCOVERED. WHEN CHECKED, THE MAGNETO WAS STILL CORRECTLY TIMED TO THE ENGINESDR CA040719004Magneto · wornOIL LEAK WAS DISCOVERED AT MAGNETO MOUNTING FLANGE GASKET. UPON REMOVAL OF UPPER AND LOWER MAGNETO MOUNT CLAMPS (P/N 66M19385), WEAR AND FRETTING OF THE MAGNETO MOUNTING FLANGE WAS DISCOVERED. WHEN CHECKED, THE MAGNETO WAS STILL CORRECTLY TIMED TO THE ENGINESDR CA040720006Screw · separatedTHESE TWO BOLTS HOLD THE FUEL PUMP IDLER GEAR SHAFT TO THE ACCESSORY HOUSING. FAILURE OF THE BOLTS ALLOWED THE IDLER GEAR AND SHAFT TO DROP TO THE BOTTOM OF THE ACCESSORY CASE. THE FUEL PUMP STOPPED TURNING AND THE ENGINE QUIT. ENGINE RESTARTED, USING ELECTSDR W1X2004F00000Hinge · brokenSTEEL HINGE (PW 4752932) FAILED PRIOR TO AD 2000-25-01 INTERVAL. (GL13200409283)SDR AUS20040462Pump · leaking(AUS) RT ENGINE DRIVEN FUEL PUMP LEAKING EXCESSIVELY FROM PUMP BODY. A LARGE AMOUNT OF FUEL WAS SPRAYING ONTO THE TURBOCHARGER WITH A HIGH RISK OF ENGINE FIRE. THE PUMP WAS A NEW ITEM WITH NO SIGN OF DAMAGE TO THE PUMP AND ALL THE MFGS TAMPER WIRES ARE IN PLACSDR CA040528007O-Ring · cutUPON LANDING, THE LEFT BRAKE DID NOT WORK. TWO O-RINGS IN THE BRAKE ASSEMBLY WERE DISCOVERED TWISTED AND CUT WHICH CAUSED A LARGE BRAKE FLUID LEAK. THE O-RINGS WERE REPLACED, THE SYSTEM WAS BLED AND TESTED.SDR CA040426004Pump · inoperative(CAN) PUMP WAS RECENTLY MODIFIED/OVERHAULED. IT WAS DISCOVERED THAT ENGINE DRIVEN FUEL PUMP OUTPUT PRESSURE DROPPED RIGHT OFF AT IDLE POWER BUT WAS FINE AT HIGH POWER SETTINGS. ENGINE DID NOT GIVE ANY INDICATION OF PUMP PRESSURE DIFFICULTIES, ROUGH RUNNING, QSDR CA040419003Brush Block · shortedAFTER DEPART, LOW VOLT IND & SELECTED AUX VOLTAGE REG WITH NO IMPROVEMENT. SEVERAL SELECTIONS WERE MADE BETWEEN MAIN & AUX REG WITH NO IMPROVEMENT. A/C RETURNED TO AIRPORT FOR A LANDING. INVEST REVEALED A SHORT-CIRCUITED BRUSHBLOCK IN RT ALTERNATOR R, WHICH DESDR 2004F00103Downlock Switch · inoperativeON A PART 91 FLIGHT THE GEAR DID NOT GET A LT DOWN LIGHT AND THE GEAR SELECTOR DID NOT COME BACK TO CENTER. AFTER A SAFE LANDING FOUND THE SWITCH NOT OPENING ALL THE WAY. CLEANED SWITCH AND BELIEVE THAT THE INTERNAL SPRING IS BROKEN AND ONLY ALLOWING HALF TRSDR CA040310009Powerpack · failed(CAN) WHEN THE PILOT SELECTED GEAR UP, ONE OF THE GEARS WAS NOT RETRACTING AND THE TRANSITION LIGHT REMAINED ILLUMINATED. AFTER SEVERAL ATTEMPTS THE GEAR RETRACTED AND EVERYTHING WAS NORMAL. THE POWER PACK WAS REPLACED.SDR CA040308010Trim System · lack of lube(CAN) PILOT REPORTED ELEVATOR TRIM JAMMED FULL FORWARD AND COULD NOT TRIM NOSE UP. ELEVATOR TRIM JACK FOUND NOT LUBRICATED. SHAFT LUBRICATED, SYSTEM FUNCTIONS NORMAL. FORWARD TRIM JACK SPOOL CHECKED OK. SPOOLING AROUND ELECTRIC ACTUATOR CKECKED OK. CABLE TESDR CA040219006Axle · broken(CAN) PILOT WAS TAXIING OUT FOR TAKEOFF WHEN THE AXLE BROKE. VIBRATION AND NOISE WAS HEARD. TAXIED BACK AND DISCOVERED THE MAIN WHEEL HAD TILTED OVER AND WAS RUBBING ON THE FORK ASSEMBLY.SDR CA040123008Bolt · corroded(CAN) THE AIRCRAFT WAS ON APPROACH WHEN THE CREW COULD NOT GET A DOWN AND LOCKED (GREEN) INDICATION ON THE RT MAIN GEAR. THE AIRCRAFT FLEW LOCALLY AND AFTER SEVERAL ATTEMPTS FLEW TO ANOTHER AIRPORT FOR A TOWER FLYBY AND LANDING. UPON TOUCHDOWN, THE RT MAIN GESDR CA040106005Downlock · inoperative(CAN) AIRCRAFT WAS PREPARING TO LAND, PILOT SELECTED GEAR DOWN, ONLY THE NOSE AND RT GEAR HAD A LOCK INDICATION, UNSAFE GEAR INDICATION.SDR AUS20031257Arm · broken(AUS) LT MAIN LANDING GEAR RETRACTION ARM BROKEN. ASSOCIATED FORK AND ROD END BENT. DAMAGE ALSO TO DOWNLOCK HOOK AND ROD END ASSEMBLY. SUSPECT DOWNLOCK HOOK FAILED TO DISENGAGE.SDR CA031205015Uplock · frozen(CAN) LANDING GEAR UPLOCK FROZEN. WOULD NOT RELEASE TO LOWER GEAR. A MANUAL GEAR EXTENSION WAS COMPLETED. AIRCRAFT GEAR INSPECTED AND RE-LUBRICATED. FLIGHTS SINCE THEN HAVE BEEN SATISFACTORY.SDR CA031205016Bulb · loose(CAN) NO RT LANDING GEAR DOWN AND LOCKED INDICATION. SOURCE CONFIRMED TO BE A LOOSE LIGHT BULB SOCKET. NO OTHER ACTION TAKEN.SDR AUS20031271Hose · leaking(AUS) FUEL PRESSURE GAUGE SENSOR HOSE LEAKING IN AREA BEHIND INSTRUMENT PANEL.SDR CA031215001Cooling Jet · separated(CAN) PISTON COOLING JET BACKED OUT OF HOLE. BOUNCED AROUND INSIDE OF ENGINE BEFORE THE CRANKSHAFT PUSHED IT THROUGH THE TOP OF THE CASESDR AUS20031062Seal · damaged(AUS) LT ENGINE HYDRAULIC PUMP DRIVESHAFT SEAL DAMAGED AND LEAKING. HYDRAULIC PUMP HAD BEEN CHANGED ON THE PREVIOUS DAY.SDR CA031021004Engine · failed(CAN) IN CRUISE THE LT ENGINE LOST POWER FOR APPROXIMATELY 5 MINUTES, THEN RESTARTED. THE ONLY INDICATION WAS A LOSS OF M.P. TO 20' AND A YAW TO THE LEFT. THE LT PROP WAS FEATHERED BUT CONTINUED TO ROTATE SO THE PILOT FELT THE ENGINE WAS STILL RUNNING AND UNFESDR CA031002006Switch · failed(CAN) WHEN ACCOMPLISHING A O/H ON THE HEATER WE FOUND THE DIFFERENTIAL PRESS SW STUCK IN THE CLOSED POSITION. THIS IS THE FOURTH SWITCH FOUND DEFECTIVE IN OUR O/H SHOP. THE SUPPOSEDLY NEW IMPROVED SWITCH MFG HAS PRODUCED IS NO BETTER THAN THE OLD SWITCH THAT ISDR CA030924005Stud · broken(CAN) LT ENGINE CYLINDER NR 5 CYLINDER BASE STUDS SHEARED OFF IN CASE. STUDS APPEAR TO HAVE BEEN CRACKED INSIDE CASE AREA. POSSIBLY FROM OVER TORQUEING.SDR CA030730001Fork · cracked(CAN) WHILE INSPECTING BRAKE PADS A CRACK WAS NOTICED ON THE RT MAIN LEG CASTING AT THE AXEL RADIUS. FURTHER INSPECTION NOTED A 1.5 INCH CRACK IN THE RT LEG AND A 0.5 CRACK IN THE LT LEG. BOTH MAIN LANDING GEAR LEGS REPLACED WITH SERVICEABLE UNITS.SDR CA030606003Cable · jammed(CAN) AUTO PILOT PITCH SERVO BRIDLE CABLE TO ELEVATOR MAIN CONTROL CABLE CLAMPS ERRONEOUSLY INSTALLED CAUSING PITCH CONTROL JAMMING AT FULL ELEVATOR UP EXTENSION.SDR CA030606002Clamp · jammed(CAN) AUTO PILOT BRIDLE CABLE CLAMP (PITCH) JAMS AGAINST EACH OTHER AT OR NEAR FULL UP (NOSE UP) CONTROL MOVEMENT. THIS IS A RECURRING PROBLEM. THIS HAS ALSO HAPPENED YEARS AGO WITH OLD EDO-AIR (ALTIMATIC III A/P). THESE CLAMPS ARE NEWER STYLE (MANDITORY BY ADSDR CA030606001Bolt · failed(CAN) DURING LAST THREE PROPELLER OVERHAULS THESE BOLTS ARE REPLACED WITH NEW AS REQUIRED. THE LAST TWO INSTALLS WERE NOT IN COMPLIANCE WITH SL 508. THESE WERE ONLY BY CHANCE NOTICED BY THE MAINTENANCE CO-ORDINATOR (NOT AME). THE PREVIOUS ONE WAS NOT NOTICED ASDR CA030606008Crankshaft · failed(CAN) COUNTERWEIGHT BLADE BUSHINGS AND BORE WORN (LOOSE) BEYOND REPAIRABLE LIMITS. PROP GOVERNOR GEAR P/N 70389 HAD FAILED.SDR AUS20031168Hose · deteriorated(AUS) FUEL HOSE LOCATED BETWEEN FUEL SELECTOR AND FUEL BOWL PERISHED.SDR CA030604006Blade · corroded(CAN) PROPELLER RECEIVED ON 22 MAY 2003, MODEL HC-E2YK-2B/FC847504 REMOVED FOR INSPECTION DUE TO EXCESSIVE ROTATIONAL BLADE MOVEMENT. A DECISION WAS MADE TO OVERHAUL THE PROPELLER. VISUAL INSPECTION ON ONE BLADE REVEALED EXCESSIVE CORROSION AT THE BLADE BEARINSDR AUS20030572Transistor · failed(AUS) INSTRUMENT LIGHTING SOLID STATE DIMMER TRANSISTORS BLOWN DUE TO WATER INGRESS THROUGH CRACKED WINDSCREEN. ELECTRICAL EQUIPMENTAND LOOMS CONTAMINATED WITH WATER.SDR CA030519001Tube · broken(CAN) TUBE ASSEMBLY FOUND BROKEN AT THE INTAKE OF THE FUEL INJECTOR WHICH CAUSED LOSS OF POWER DURING CLIMB.SDR CA030501009Drive Shaft · cracked(CAN) RT FLAP FLEX CABLE WAS FOUND TO HAVE A CRACK ON THE SLINED SHAFT FROM THE PIN HOLE TO THE END OF THE DRIVE. THIS WAS DISCOVERED WHEN AD 82-27-13 WAS CARRIED OUT. REPLACED SHAFT DRIVE
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