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 = 'B200' 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 = 'B200' 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 CA110905003Oil System · leaking(CAN) ON A REPOSITIONING FLIGHT, WHILE IN CRUISE, THE PILOT NOTICED HEAVY TORQUE FLUCTUATIONS FROM THE ENGINE FOLLOWED BY LARGE FLAMES FROM EXHAUST. THE ENGINE WAS SHUTDOWN AND THE FLIGHT CONTINUED TO DESTINATION WHERE THE ACFT LANDED UNEVENTFULLY. GROUND INSSDR CA110902006Shutoff Valve · intermittent(CAN) LT ENGINE NO START ON FIRST ATTEMPT. SHUTOFF VALVE CYCLED AND FOUND OPERATIVE. VALVE CHANGED AS PRECAUTION AND SENT FOR INSPECTION. O/H OF UNIT PERFORMED. INSPECT VALVES ON ACFT FLEET FOR ROUGH OR SLOW OPERATING VALVES. REPLACE NEXT HIGHEST TIME VALVSDR CA110831006Shutoff Valve · misinstalled(CAN) DURING SCHEDULED ACFT MX, A REPLACEMENT OXYGEN BOTTLE WAS INSTALLED. FLIGHT CREW LATER DISCOVERED THE OXYGEN SYS WAS NOT WORKING PROPERLY. THE OXYGEN SHUTOFF VALVE HAD BEEN RIGGED BACKWARDS TO THAT OF NORMAL OPERATIONS, MEANING WHEN THE COCKPIT HANDLESDR CA110825003Bolt · sheared(CAN) UPPER DOOR LATCH BOLT FOUND SHEARED DURING INSPECTION AT FIRST THREAD.SDR CA110826013Seal · leaking(CAN) WHILE IN CRUISE, APPROX 20 MINUTES FROM DESTINATION (INBOUND) THE PILOTS NOTICED THE RT ENGINE OIL PRESSURE FLUCTUATING FROM 70-130 PSI. THE FLIGHT WAS CONTINUED AND AN UNEVENTFUL LANDING WAS MADE. INVESTIGATION REVEALED THE EDFP (HIGH PRESSURE) ACCESSSDR CA110826012Seal · leaking(CAN) OIL SEAL ON AIR CONDITIONER DRIVE PAD ON THE ACCESSORY CASE OF THE ENGINE HAD POPPED OUT OF THE CARRIER AND ENGINE LEAKED A SUBSTANTIAL AMOUNT OF OIL. REPLACED SEAL AND SEAL CARRIER WITH NEW.SDR CA110804008Tach Generator · failedACFT WAS ON A ROUTINE FLIGHT. WHEN THE NP (PROP SPEED) INDICATION WENT TO ZERO. THE TACH GENERATOR WAS REPLACED WITH AN O/H UNIT WITH OUT FURTHER INCIDENT.SDR CA110727003Fitting · corrodedFITTING LT SIDE, CHAFING AND CORRODED AT ANCHOR NUT LOCATION.SDR CA110804006Tube · deterioratedON A ROUTINE FLIGHT, THE LT BLEED AIR FAIL LIGHT ILLUMINATED. THE CREW DID NOT NOTICE A ENGINE ITT, SO THEY SHUT OFF THE LT BLEED AIR VALVE AND CONTINUED. UPON INSP, IT WAS NOTED THE EVA TUBING WAS HARD AND BRITTLE IN SEVERAL PLACES AND HAD SEVERAL REPAIRS OSDR CA110804007Pressure Switch · failedAFTER CHANGING THE BLEED AIR FAIL PRESSURE SWITCH ON A TEST FLIGHT, THE LT BLEED AIR FAIL SWITCH ILUMINATED AGAIN. FURTHER INSP REVEALED THE NEW PRESSURE SWITCH HAD FAILED. ANOTHER NEW SWITCH WAS INSTALLED WITH OUT FURTHER INCIDIENT.SDR CA110726011Web · crackedWEB HAD EXTENSIVE CRACKS, SOME VISUAL AND MANY FOUND ON NDT CHECK. FREQ EDDY CURRENT WAS USED. TECH SUPPORT INDICATED THAT CONDITION HAD BEEN SEEN BEFORE ON HIGH TIME, HIGH CYCLE ACFT.SDR CA110726010Frame · crackedFRAME CRACKED, AT STRINGER 9, ALONG SKIN FLANGE BEND RADIUS. CRACKED APPROX 2.5 INCHES ALONG BEND.SDR CA110726009Frame · crackedFRAME CRACKED. CRACK IS TYPICAL THROUGH PEAR SHAPED LIGHTNING HOLE IN FRAME.SDR CA110726008Skin · crackedSKIN FOUND CRACKED DURING VISUAL INSPECTION.SDR CA110627019Valve · bentDURING POST-FLIGHT INSPECTION, ANTI-SIPHON VALVE IN RT OTBD WING FUEL FILLER WAS FOUND FORCED OUT AT FLAPPER SEAL AREA AND CRACKED UP TO ATTACH FLANGE. VALVE WAS REPLACED WITH NEW PART, SAME PN. DAMAGE WAS CAUSED BY FUELLER`S FORCING FUEL NOZZLE IN FILLER ANSDR CA110624004Powerpack · failedTHE HYD POWER PACK REPLACED WITH AN O/H POWER PACK. O/H POWER PACK WAS INSTALLED AND SERVICED IAW MM. DURING THE TESTING OF THE UNIT, MX NOTICED THAT THE GEAR WAS NOT EXTENDING SMOOTHLY, IT EXTENDED ABOUT 6 INCHES AND STARTED TO CHATTER. SYS WAS BLED SEVERSDR CA110618001Bearing · failedFLAP SYS ASSYMETRY OCCURRED DURING A HIGH ALTITUDE SIMULATED OVERSHOOT. PILOT REPORTED THAT THE ACFT DIDN`T WANT TO CLIMB VERY WELL AND IT WANTED TO NATURALLY TURN TO THE RT ONCE CLIMB ENGINE POWER WAS APPLIED AND FLAPS WERE RETRACTED. FURTHER INSPECTION OUTSDR CA110623011Circuit Breaker · trippedON APPROACH TO LANDING, CREW SELECTED THE GEAR DOWN BUT GEAR DID NOT EXTEND. CREW WHEN THRU THEIR PROCEDURES AND FOUND THAT BOTH THE 1 & 2, 50 AMP CIRCUIT BREAKERS FOR THE NR 2 DUAL FEED BUS HAD POPPED. THE CREW ADVISED TOWER AND PROCEEDED TO EXTEND THE GEAR SDR CA110719008Transducer · failedDURING FLIGHT, THE CREW NOTICED THE LT ENGINE OIL PRESSURE DECREASING. IAW THE SOP`S THE ENGINE WAS SHUTDOWN IN FLIGHT AND A SAFE LANDING WAS MADE. TROUBLESHOOTING WAS CARRIED OUT AND FOUND THAT THE OIL PRESSURE TRANSDUCER HAD FAILED GIVING THE LOW READING.SDR CA110606004Drain · blockedDURING CRUISE AT FL210, CREW NOTICED OIL PRESSURE AND TORQUE FLUCTUATIONS WITH SMOKE COMING FROM THE EXHAUST STACK. THE ENGINE WAS SHUTDOWN AND AN UNEVENTFUL SINGLE ENGINE LANDING WAS ACCOMPLISHED AT THE POINT OF DEPARTURE. POST-FLIGHT INSPECTION REVEALED A SDR CA110719007Circuit Breaker · meltedPILOTS SMELLED A FAINT ODOR OF SMOKE THAT SEEMED TO DISSIPATE AFTER THE ENVIRONMENTAL SWITCHES WERE TURNED ON AND CONTINUED FLIGHT. DURING GROUND CHECKS OF THE ACFT, BY MX, THE FIRE DETECTION SYS WAS FOUND U/S WHICH LEAD TO THE DISCOVERY OF THE CIRCUIT BREAKESDR CA110531007Seal · leakingENGINE LOST 3-4 QUARTS DURING PREVIOUS FLIGHT. DURING INVESTIGATION OIL WAS FOUND TO BE COMING FROM THE HIGH PRESSURE FUEL PUMP DRAIN BETWEEN THE ENGINE AND FCU. FCU AND FUEL PUMP WERE REMOVED AND THE SEAL AT THE ENGINE DRIVE WAS FOUND TO HAVE MIGRATED COMPLESDR CA110512006Pressure Switch · leakingTHE FLUID WAS LEAKING INTERNALY AND SHORTED THE SWITCH CAUSING THE SYS NOT TO WORK. A NEW PRESSURE SWICH WAS INSTALLED, BREAKER PUSHED IN AND AIR CONDITION SYS RECHARGE .SDR FCPR20110004Access Panel · corrodedDURING BONDED PANEL INSP, FOUND CORROSION BETWEEN LT AND RT INBD AUX FUEL TANK BOND PANELS AND WING STRUCTURE. PANELS PN 101-120076-605/-606.SDR CA110513004Relay · failedLANDING GEAR MOTOR RELAY CONTACTS WELDED SHUT ALLOWING HYD MOTOR TO RUN FOR AN EXTENDED PERIOD EVEN THOUGH THE 2 AMP LANDING GEAR MOTOR RELAY C/B POPPED. THE RELAY WAS REPLACED AND THE HYD POWER PAC REMOVED FOR INSP AND SERVICE AS REQUIRED BY THE MFG AS IT RANSDR CA110428009Bolt · missing(CAN) DURING POST FLIGHT INSPECTION ON ACFT CREW NOTICED THAT THE RT OTBD BRAKE CALIPER CASTING WAS BROKEN. MAINTENANCE WAS NOTIFIED AND UPON INVESTIGATION FOUND 1 OF THE GUIDE PINS WAS MISSING, PN 069-02000. THE BOLT THAT HOLDS PIN IN PLACE WAS STILL LOCK WSDR CA110426007Bearing · binding(CAN) WHILE IN CRUISE FLIGHT, PILOT NOTICED ENGINE FLUCTUATIONS OF APPROXIMATELY 150 LBS TORQUE AND 1.0 TO 1.5 PERCENT N1. RETURNED TO BASE WITH UNEVENTFUL LANDING. MAINTENANCE REMOVED THE FUEL CONTROL UNIT AND DISCOVERED THE DRIVE BEARING FELT ROUGH AND THESDR CA060410007Shutoff Valve · intermittent(CAN) DURING TAKEOFF ROLL, ACFT VEERED TO THE RT. CREWS PULLED POWER BACK AND RETURNED TO BLOCKS. FOUND THE LEFT ENGINE BLEED FIREWALL SHUTOFF VALVE WAS STUCK IN THE CLOSED POSITION AND THE CREW DID NOT NOTICE THE FAULT DURING START CHECKLIST. THE VALVE BEISDR 2011F00068Arm · looseA CASTING ARM ATTACHED TO THE RUDDER TORQUE TUBE WAS DISCOVERED TO HAVE ALL 6 ATTACHING RIVETS LOOSE AND WORKING.SDR CA110308004Uplock Switch · stuck(CAN) ON APPROACH, THE LANDING GEAR WAS SELECTED DOWN, NO LT MLG DOWN AND LOCKED GREEN LIGHT WAS OBTAINED. A MISSED APPROACH WAS CONDUCTED, THE GEAR SELECTED DOWN AGAIN AND ALL 3 GREEN DOWN AND LOCKED LIGHTS WERE OBTAINED. AFTER LANDING, A VIRTUAL INSPECTIONSDR CA110222010Engine · malfunctioned(CAN) DURING TAKEOFF THROUGH ABOUT 30 KTS, THE NR1 ENGINE POWER ROLLED BACK TO FLIGHT IDLE. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE INSPECTED ENGINE CONTROLS, OIL, FUEL AND AIR SYSTEMS WITHOUT FINDING ABNORMALITIES. SEVERAL ENGINE POWER RUNS CARRIED OSDR CA110207008Static Inverter · failed(CAN) ON A ROUTINE FLIGHT, THE NR 1 STATIC INVERTER FAILED, THE PILOT SELECTED NR 2 STATIC INVERTER AND THE FLIGHT CONTINUED WITH OUT INCODIENT. THE NR 1 STATIC INVERTER WAS REPLACED WITH OUT FURTHER INCOIDENT.SDR CA110204006Wire · misinstalled(CAN) DURING APPROACH, IT WAS NOTICED THAT ONCE THE LANDING GEAR WAS DEPLOYED THAT THE NOSE LANDING GEAR DOWN INDICATOR LIGHT WAS EXTINGUISHED. PILOT USED THE "PUSH TO TEST" FUNCTION AND CONFIRMED THAT LIGHT BULBS WERE NOT BURNED OUT. APPROACH ABORTED AND THESDR CA110207007Washer · failed(CAN) DURING A ROUTINE TAKE-OFF, THE PILOTS NOTED THE LANDING GEAR WOULD NOT RETRACT, THE PILOTS ELECTED TO RETURN TO DEPARTURE AIRFIELD AND LANDED WITH OUT INCIDENT. UPON FURTHER INSPECTION, IT WAS REVEALED THAT THE RH MAIN LANDING GEAR TORQUE KNEES HAD SEPSDR CA110201010Mount · loose(CAN) VISUAL MOVEMENT CHECK REVEALED LOOSENESS OF ENGINE MOUNT FITTINGS P/N 50-980089-1. THERE ARE 4 PER NACELLE. THE LOWER PAIR WHERE FOUND LOOSE.SDR 2011FA0000072Brake Assy · leakingDURING LANDING ROLL-OUT AND AFTER UTILIZING BETA OR DISCING TO SLOW THE ACFT DOWN TO TAXI SPEEDS, I SWITCHED TO WHEEL BRAKING AND THERE WAS NO PRESSURE ON THE LT SIDE. GROUND CONTROL WAS ABLE TO CLEAR ME TO THE SIGNATURE RAMP AREA WITHOUT REQUIRING A FULL-STOSDR CA110201008Skin · cracked(CAN) VISUAL INSPECTION REVEALED CRACKED OUTBOARD SKINS P/N 100-110068-15 AND 16. THESE ARE THE OUTER SKINS ON THE OUTER WINGS LH AND RH. CRACKS WERE LOCATED AT ABOUT 12 O`CLOCK POSITION OF THE OUTBOARD FUEL CAPS. CRACKS UNDOUBTEDLY RELATED TO ABNORMAL LOADS ASDR CA110201007Keel · cracked(CAN) VISUAL INSPECTION OF THE NOSE KEEL RIBS P/N 101-410052-9 AND 101-410079-1 REVEALED CRACKS AT UPPER FWD CORNERS OF THE FORWARD GEAR DOOR HINGE CUTOUTS.SDR CA110118001Stator · crackedDURING SCHEDULED HSI THE PT STATOR 1ST STAGE WAS FOUND TO BE CRACKED BEYOND LIMITS, THE INNER RING WAS CRACKED COMPLETELY THROUGH AND THE OUTER RING WAS CRACKED COMPLETELY THROUGH EXTENDING INTO A VANE. INSP OF THE OPPOSITE ENGINE REVEALED CRACKING OF THE SAMESDR CA110117011Brake Assy · frozen(CAN) LANDED AT 0015 AND DURING THE LANDING ROLL EXPERIENCED TIRE FAILURE ON NR 3 AND 4 MLG TIRES, LIKELY DUE TO A BRAKES FREEZING ON DEPARTURE. UPON POWERING UP, THE LT BRAKES GRABBED BEFORE BREAKING FREE. ON THE DEPARTURE ROLL THROUGH APPROXIMATELY 80 KTS SDR CA110125025Cover · cracked(CAN) DURING SCHEDULED PHASE INSPECTION, MAINTENANCE DISCOVERED THE HOT BUSS (CIRCUIT BREAKER) PLASTIC COVER AND SUPPORT ASSEMBLY CRACKING AT VARIOUS POINTS. A REVIEW OF OTHER B200`S IN THE FLEET SHOW THIS PART HAVING BEEN REPLACED IN THE PAST FOR THE SAME RSDR CA101229009Wire Harness · shorted(CAN) DURING A ROUTINE FLIGHT, THE CREW NOTED THE CIRCUIT BREAKER POPPED ON THE PROPELLER DEICE SYSTEM. THE CREW CONTINUED TO DESTINATION WITHOUT INCIDENT. MAINTENANCE DISCOVERED THAT THE WIRE HARNESS HAD SHORTED OUT IN THE SPINNER. THE HARNESS WAS REPLACED WSDR CA101229010O-Ring · failed(CAN) ON A ROUTINE TRAINING FLIGHT, IT WAS NOTED BY THE CREW THAT THE LANDING GEAR POWER PACK WAS CYCLING APPROXIMATELY EVERY 30 SECONDS. MAINTENANCE INSPECTION REVIELED THAT THE O-RING ON THE CHECK VALVE HAD FAILED P/N MS28775-016. O-RING WAS REMOVED AND RESDR CA101216005Bearing · failed(CAN) TODAY DECEMBER 16/2010 13:00 HRS ON A ROUTINE FLIGHT FROM GRAND PRAIRIE TO HIGH LEVEL WITH KING AIR C-FPQQ (MEDEVAC NOR-ALTA 912). CENTER CONTACTED THEM EN ROUTE AND ASKED THEM IF THEY HAD LOST A WHEEL FROM THE AIRCRAFT. THE CREW TOTALLY UNAWARE OF THIS SDR CA101213010Motor · odor(CAN) ON A FLIGHT, IT WAS DISCOVERED THAT WHEN CABIN AIR WAS SELECTED THE SMELL OF BURNING WIRES BECAME EVIDENT. THE CABIN AIR WAS TURNED OFF & THE FLIGHT CONTINUED WITHOUT INCIDENT. UPON ARRIVAL AT DESTINATION, THE MOTOR WAS REPLACED AND FUNCTION CHECKED SERVSDR CA101213006Skin · damaged(CAN) DURING UNSCHEDULED MAINTENANCE ON A UNRELATED ITEM ON THE AIRCRAFT, IT WAS NOTED THAT THE RH OUTBOARD SKIN BOTTOM SIDE IN LINE WITH THE PROP WASH HAD A SIZABLE CRACK GOING IN SEVERAL DIRECTIONS CAUSED FROM OIL CANNING. THE FLAP WAS REPAIRED IN ACCORDANCESDR CA101207006Fuel Control · malfunctioned(CAN) PILOT REPORTED SMALL TORQUE FLUCTUATIONS IN CRUISE FLIGHT. MAINTENANCE REMOVED THE FUEL CONTROL UNIT FOR INSPECTION AND REPAIR AS NECESSARY. (TC# 20101207006)SDR CA101130007Skin · crackedBOTH LOWER FWD ENGINE COWLS ON AIRCRAFT HAD CRACKED DUCT SKINS P/N 101-910020-3.SDR CA110105017Adc · inoperativeON THE TAXI, THE PILOTS EFIS SCREEN WENT BLANK, THE AIRCRAFT RETURN TO THE BLOCKS AND THE UNIT WAS EXCHANGED WITHOUT INCIDENT.SDR CA101026004Coax · failed(CAN) DURING APPROACH IN IMC GPS PORTION OF THE FMS FAILED AND GAVE ERROR MESSAGE "GPS 1 NOT NAV". IT WAS DETERMINED THE COAXIAL CABLE AT THE BASE OF THE GPS ANTENNA HAD A POOR CONNECTION. THE COAXIAL CABLE WAS EASILY PULLED FROM THE COAX CONNECTOR. CONNECT
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