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 = '1900C' 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 = '1900C' 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 FFSA2011F00001Spar Cap · corrodedHORIZONTAL STABILIZER REAR SPAR, RT LOWER CAP, FOUND CORRODED INBD AND OTBD OF THE HSS 66.0 CENTER ELEVATOR HINGE LOCATION.SDR FFSA2011F00000Door Frame · crackedDURING THE 3RD, 200 HR INTERVAL, DETAILED INSP, A CRACK WAS DISCOVERED IN THE UPPER FWD CORNER OF THE AFT CARGO DOOR FRAME. THE CRACK WAS LOCATED IN THE UPPER LEG OF THE DOOR FRAME STARTING AT FS 458.3 AND EXTENDED AFT HORIZONTALLY ABOUT 4". THE CRACK WAS JUSDR TIMA20110004Skin · corrodedDISCOVERED CORROSION DAMAGE ON THE FUSELAGE BELLY SKINS DURING VISUAL INSPECTION. REPAIRED SKINS USING COVER PATCH METHOD IAW BEECH SRM 51-70-6.SDR TIMA20110003Skin · corrodedDISCOVERED CORROSION DAMAGE ON THE FUSELAGE BELLY SKINS DURING VISUAL INSPECTION. REPAIRED SKINS USING COVER PATCH METHOD IAW BEECH SRM 51-70-6.SDR 2011FA0000478Motor · failedREPORTED THAT AT APPROX 0130 IN THE MORNING PILOT HAD TO MANUALLY EXTEND THE LANDING GEAR PRIOR TO LANDING. THE PILOT SELECTED GEAR DOWN AND IT DID NOTHING. HE FOUND THE LANDING GEAR RELAY CIRCUIT BREAKER HAD POPPED. HE THEN MANUALLY PUMPED THE GEAR DOWN ANSDR TIMA20110002Retaining Nut · backed outON APPROACH A SPLIT FLAP CONDITION OCCURRED. WHEN FLAPS WERE SELECTED DOWN, THE LT INBOARD FLAP REMAINED IN THE FULL UP POSITION. ALL OTHER FLAPS EXTENDED NORMALLY. CAUSE WAS DETERMINED TO BE A DRIVE GEAR RETAINING NUT THAT HAD BACKED OUT UNDER AIR LOAD IN SDR HSYA2011062411Wire · loosePILOT REPORTED - OVERHEAD PANEL OVERHEATING WITH A STRONG ELECTRICAL BURNING ODOR IN-FLIGHT. WINDSHIELD WIPERS CYCLED ONCE UNCOMMANDED. MAINTENANCE TROUBLESHOOTING - MAINTENANCE LOWERED OVERHEAD CONTROL PANEL TO TROUBLESHOOT, FOUND BALLAST RESISTOR HAD A LOSDR TIMA20110001Connector · burnedSTRONG BURNING SMELL IN THE COCKPIT - AIR RETURN TO BIL. TROUBLESHOT TO SHORTED BURNT 37 PIN CONNECTOR AT DB-207 AURAL ANNUNCIATOR AMPLIFIER.SDR JIKA11060301Governor · failedDURING A TRAINING FLIGHT OUT OF KCRP, A SIMULATED SINGLE ENGINE OUT PROCEDURE WAS CONDUCTED WITH THE LEFT ENGINE. DURING ENGINE RE-START, THE PROPELLER WOULD NOT COME OUT OF FEATHER. THE CREW RETURNED TO KCRP, AND ALTHOUGH NO EMERGENCY WAS DECLARED, FIRE EQUSDR YADA060311001Altimeter · inoperativePILOT REPORTED HIS ENCODING ALTIMETER WAS INOPERATIVE ON TAKEOFF. THIS SITUATION ALSO RENDERED THE ALTITUDE ALERTER AND TRANSPONDER MODE C INOPERATIVE. EXCESS FUEL WAS BURNED OFF AND THE ACFT RETURNED TO BASE. MX REPLACED THE PILOT'S ENCODING ALTIMETER, PERSDR JIKA11052501Altimeter · inoperativeUPON DEPARTURE THE PILOT REPORTED A GPS ALTITUDE FAILURE FOLLOWED BY ATC REQUESTING A CHECK OF THE TRANSPONDER. THE PILOT SELECTED THE NR 2 TRANSPONDER, ATC REPORTED THAT THEY WERE STILL NOT RECEIVING ALTITUDE REPORTING INFORMATION. THE PILOT NOTICED A 10-20SDR KGBR507Y201105250Skin Panel · crackedCRACK IN SKIN PANEL .5 INCH FWD OF THE TRAILING EDGE, 4.5 INCHES TO 10.5 INCHES FROM THE INBOARD EDGE OF THE FLAP. ALSO ARE 2 CRACKS IN THE AREA OF THE INBOARD ATTACH BRACKET AREA AT THE OUTBOARD ACCESS HOLE, 13 INCHES OUTBOARD OF THE INBOARD EDGE, EACH AT APSDR CA110601007Bearing · failedELECTRIC LANDING GEAR MOTOR FOR THE GEAR HYDRAULIC POWERPACK ASSY WAS FOUND WITH INTERNAL BEARING DAMAGE AND ELECTRICAL BURNING SMELL. PART REPLACED. NO FURTHER ISSUES.SDR CA110506002Cable · failed(CAN) AIRCRAFT WAS PARKED OUTSIDE OVERNIGHT IN THE RAIN. THE FOLLOWING DAY WHILE FLYING AT FL240, THE CREW REPORTED ELEVATOR FROZEN. MAINTENANCE GAINED ACCESS TO TAIL SECTION AND FOUND ELEVATOR AUTO PILOT SERVO CABLE DRUM FROZEN FROM RAIN INGRESS INSIDE TAIL CSDR HSYA2011042211Skin · corrodedFUSELAGE STATION 438 HAS AREA OF EXFLOLIATION CORROSION ON LOWER FUSELAGE SKIN. CUT OUT EXFLOLIATED AREA AND FABRICATED FILLER (1.8750" X 2.6250") USING MATERIAL SPEC. 2024T3 .025. FABRICATED DOUBLER (5.1875" X 6.0625") USING MATERIAL SPEC. 2024T3 .032. CLEANSDR YADA042111Relay · stuckENROUTE, THE PILOT NOTICED THE LANDING GEAR RELAY CIRCUT BREAKER WAS POPPED. THE FLIGHT CREW ALSO THOUGHT THEY COULD HEAR THE LANDING GEAR PUMP RUNNING BUT WERE UNSURE. AT ONE POINT IN THE FLIGHT THE HYD RESERVOIR LOW LEVEL LIGHT CAME ON BUT LATER EXTINGUISHSDR YADA041511Landing Gear · malfunctionedPILOT REPORTED THAT IN CRUISE, NOTICED THE LANDING GEAR RELAY CIRCUT BREAKER WAS POPPED. SEVERAL ATTEMPTS TO RESET THE CIRCUT BREAKER WERE UNSUCCESSFUL. ON ARRIVAL THE CREW HAD TO MANUALLY EXTEND THE LANDING GEAR. MECHANIC WAS CONTACTED AND INSPECTED THE ACSDR CA110414004Bolt · failed(CAN) COMING OUT OF AIRPORT THIS MORNING THE CREW SELECTED GEAR UP AND THE RT STAYED GREEN WITH A RED HANDLE. THE CREW CONFIRMED VISUALLY THAT THE GEAR HADN`T MOVED WHILE THE OTHER 2 WERE UP. THEY CYCLED THE GEAR AGAIN AND IT CAME UP NORMALLY. WE DECIDED TSDR CA110627004Engine · power loss(CAN) POWER LOSS/IFSD DURING CRUISE, THE ENGINE SURGED FOLLOWED BY A POWER LOSS. THE PILOT NOTICED THE ENGINE TEMPERATURE REACHED 1100 C. THE ENGINE WAS SHUTDOWN IMMEDIATELY AND SINGLE ENGINE LANDING CARRIED OUT WITH NO INCIDENT. THE ENGINE WAS SENT TO VECTOSDR CA110324003Stud · burned(CAN) WHILE TROUBLESHOOTING A PROPELLER DE-ICE SNAG, THE MAINTENANCE CREW FOUND THE RT DC POWER PANEL START CABLE STUD TO BE BURNED. POWER PANEL WERE REPLACED.SDR CA110322001Engine · failed(CAN) MARCH 16TH, 2011, 11:20 PM, DIVERTED DUE TO RISE IN ITT, FOLLOWED WITH AN ENG SURGE. THE CREW SHUT THE ENG DOWN & LANDED SAFELY AT THE AIRPORT. AS OF NOW ALL WE KNOW IS THAT THERE WAS AN INTERNAL ENG FAILURE. THE ENG WAS REMOVED & SENT FOR A TEAR DOWNSDR CA110214020Relay · failedLANDING GEAR WOULD NOT EXTEND WHEN THE GEAR SELECTOR WAS MOVED TO THE DOWN POSITION. GEAR WAS EXTENDED USING MANUAL HAND PUMP WITH NO OTHER PROBLEMS. UPON INSP IT WAS DISCOVERED THERE WAS MOISTURE IN THE MLG RELAY CAUSING IT TO FREEZE IN FLIGHT. THIS WAS PROSDR CA110131008Hose · leaking(CAN) DURING RETRACTION TESTS, A LOUD CRACK WAS HEARD ON EXTENSION. FLUID WAS FOUND UNDERNEATH LH GEAR WHEEL WELL. VISUAL INSPECTION OF AREA CARRIED OUT. FLUID WAS OBSERVED POURING OUT OF HOSE FITTING CRIMP AREA.SDR CA110126006Amplifier · failed(CAN) ON CLIMB-OUT A BURNING ODOR WAS NOTICED IN THE CABIN, THE PILOTS HEADSET THEN CUT-OUT. AN UNEVENTFUL EMERGENCY LANDING WAS CARRIED OUT. UPON INSPECTION THE AUDIO CONTROL AMPLIFIER WAS FOUND TO HAVE FAILED INTERNALLY CAUSING THE SMOKE ODOR.SDR EPUA12152010404GVActuator · failedNLG FAILED TO EXTEND DUE TO FAILURE OF HYD ACTUATOR CAUSING LOSS OF HYD FLUID. UPON INSP, HYD ACTUATOR END CAP FOUND TO BE UNSERVICABLE.SDR 2010F00251Downlock Switch · intermittentON APPROACH TO THE AIRPORT, THE GEAR WAS SELECTED DOWN BUT THERE WAS NO INDICATION THE NOSE GEAR WAS DOWN AND LOCKED. THE GEAR WAS CYCLED SEVERAL TIMES AND CYCLED MANUALLY ONCE BUT THERE WAS STILL NO NOSE GEAR DOWN INDICATION. THE ACFT RETURNED TO BASE. ON SDR EPU2011F00001Fire Warning · false activationLT ENGINE FIRE WARNING ILLUMINATED MOMENTAIRLY. NO FIRE OCCURRED. FIRE WARNING SYS WAS INSPECTED IAW MM, ALL CONNECTIONS WERE CLEANED DURING THE INSPECTION AND ALL RESULTS OF CHECKS WERE WITHIN LIMITS.SDR CA110107010Bracket · bentAIRSTAIR DOOR AJAR SWITCH WAS HIT BY A BOARDING PASSENGER FOOT. THE IMPACT BENT THE SWITCH HOLDING BRACKET JUST ENOUGH THAT IT DID NOT CAUSE THE WARNING LIGHT TO LIGHT UP (ILLUMINATE). DURING CLIMB (8000FT), THE PRESSURIZATION IN THE CABIN THEN PUSHED ENOUGHSDR CA101209003Relay · unserviceable(CAN) THIS AIRCRAFT HAS BEEN OFF-LINE AND UNDERGOING MAINTENANCE FOR SEVERAL WEEKS DUE TO A SNAG WITH THE MAIN LANDING GEAR EXTENSION SYSTEM. THE AIRCRAFT HAS BEEN EXPERIENCING PROBLEMS EXTENDING THE MAIN LANDING GEAR, ESPECIALLY AFTER EXTENDED FLIGHT AT ALTITSDR CA101129007Shaft · shearedCOCKPIT INDICATION ALERTED CREW TO FAULT WITH FUEL PRESSURE SYSTEM. DEFECT DEFERRED AS PER MEL. UPON INSPECTION BY MAINTENANCE, THE DRIVE SHAFT FOR THE LOW PRESSURE ENGINE DRIVEN FUEL PUMP DRIVE SHAFT WAS FOUND SHEARED.SDR HSYA2010110310Landing Gear · malfunctionedAFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT -COME UP-AFTER CYCLING THE GEAR STILL WOULD NOT COME UP AND WAS STILL INDICATING 3 GREEN IN THE DOWN POSITION. CREW ADVISED THE TOWER AND DECLARED AN EMERGENCY TO LAND. ACFT LANDED WITH NO FURTHER INCIDENT. MX SDR HSYA2010110210Skin · corrodedDURING ACFT INSP THE FOLLOWING DISCREPANCIES WERE DISCOVERED. FUSELAGE STA 318 LT LOWER BELLY HAS EXFOLIATION CORROSION ON LOWER BELLY SKIN. REMOVED CORROSION, CLEANED, TREATED AND PRIMED AREA. CUT OUT 2" X 1.5" CORROSION AREA AND FABRICATED FILLER AND REPAIRSDR CA101020001Wire · chafedWHILE COMPLETEING PHASE 3 INSP IN THE CABIN WHICH INVOLVES REMOVING THE FLOOR PANELS, THERE WERE WIRES FOUND CHAFING ON THE EDGE OF THE WIRING TRAY AT FS 177.35. ALSO DISCOVERED WIRES CHAFED THROUGH THE INSULATION AND WAS ARCING ON THE METAL TRAY THAT THE WISDR YADA1018201000002Elevator · damaged2 MINUTES OUT OF LANDING,THE PILOT REPORTED (ON LANDING) THAT HE HAD TAKEN A LIGHTNING STRIKE TO THE NOSE OF THE ACFT. INSP OF THE ACFT REVEALED THAT THE TIP OF THE RT ELEVATOR HAD "BLOWN UP". A MECHANIC HAS BEEN DISPATCHED TO THE SCENE WITH AN ELEVATOR AND SDR YAD2010F00000Master Cylinder · unserviceableON LANDING, LT BRAKES LOCKED UP. PILOT STATED THAT AFTER LANDING THE LT BRAKES ACTIVATED WITHOUT INPUT FROM EITHER CREW MEMBER. THE DEGREE OF BRAKING ACTION WAS SLIGHT INITIALLY BUT BUILT AS TAXI PROGRESSED TO THE POINT THAT THE ACFT COULD NOT BE TAXIED AFTESDR 2010F00210Fire Loop · no testLT FIRE PULL HANDLE FLASHED INTERMITTENT (2 SEC) ON DESCENT. ALL INDICATIONS OTHERWISE WERE NORMAL DID TEST LT LOOP AND AMP NEITHER WOULD TEST.SDR CA100917001Spring · crackedPROPELLER WAS TIME EXPIRED. UPON DISASSEMBLY OF THE SPRING ASSY, THE FEATHERING SPRING WAS FOUND TO BE CRACKED. NO OTHER DAMAGE WAS FOUND.SDR HSYA2010082910Skin · corrodedSTATION 453 HAS EXFOLIATION CORROSION FUSELAGE BELLY SKIN. CUT OUT SKIN CORROSION (2.5" X 3.25") AND FABRICATED FILLER FROM .040 2024T3-FABRICATED DOUBLER (5.75" X 6.75") FROM .050 2024T3. CLEANED, TREATED, PRIMED AND SEALED- INSTALLED IAW SRM 51-70-00, 53-30-SDR CA100916002Spring · brokenPROPELLER WAS TIME EXPIRED. UPON DISASSEMBLY OF THE SPRING ASSY, THE FEATHERING SPRING WAS FOUND TO BE BROKEN. NO OTHER DAMAGE WAS FOUND.SDR CA100729006Liner · misrepairedWHILE REMOVING THE LED PORTION OF CC OUTER LINER IAW PWC 724002-SRR-05 INCOMPLETE RESISTANCE WELD HOLDING LED PORTION IN PLACE WAS FOUND. CIRCUMFERENTIAL RESISTANCE WELD HAD SEVEN EQUALLY SPACED WELDING POINTS WHICH HELD IN PLACE THE LED PORTION INSTEAD OF COSDR ERAA201000004Light · inoperativeWHEN EXTENDING GEAR IN KSM, NONE OF THE GREEN INDICATORS FOR THE GEAR DOWN & LOCKED INDICATION ILLUMINATED. RAN THROUGH QRH. RETURNED TO ANC, FLEW BY TO VISUALLY CONFIRM GEAR DOWN. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED LIGHT BULBS IN GEAR DOWN POSISDR CA100723004Line · crackedON TAKEOFF, ENGINE WAS UNABLE TO ACHIEVE FULL POWER AND ACFT RETURNED TO BASE. A NORMAL LANDING WAS CARRIED OUT. UPON INSP, THE P3 LINE FROM THE COMPRESSOR CASE TO THE FCU WAS FOUND CRACKED, PREVENTING FULL P3 AIR FROM REACHING THE FCU. LINE WAS REPLACED, NOSDR CA100715004Wire · burnedWHEN REMOVING THE RT CIRCUIT BREAKER PANEL TO CHECK THE EDGELIGHT PANEL, THERE WAS ONE BRASS SCREW WITH THE TIP BURNED. MX IMMEDIATELY INVESTIGATED THE SOURCE. THERE WAS A NR 10 WIRE FROM THE AVIONICS BUSS BAR TO THE ARTIFICIAL HORIZON THAT WAS ALMOST BURNEDSDR ERAA201000003Handle · inoperativeCABIN DOOR WON'T OPEN FROM INSIDE. REMOVED AND REPLACED INTERIOR DOOR HANDLE ASSY REF 1900C MM 52-10-00.SDR CA100916001Spring · brokenPROPELLER WAS TIME EXPIRED. UPON DISASSEMBLY OF THE SPRING ASSY, THE FEATHERING SPRING WAS FOUND TO BE BROKEN. NO OTHER DAMAGE WAS FOUND.SDR FFSA201000001Channel · crackedDURING NR 3 PHASE INSP THE LOWER DOOR FRAME CHANNEL WAS FOUND TO BE CRACKED. THE CHANNEL, PN 114-420041-41, RUNS FROM FUSELAGE STA 150.60 TO STA 177.35 ACROSS THE BOTTOM OF THE DOOR OPENING. THE CRACK WAS LOCATED IN THE BEND RADIUS OF THE OTBD SUPPORT FLANGE SDR CA100622013Compressor · failedON SHORT FINAL, LT ENGINE STARTED TO SURGE, TORQUE FLUCTUATING BETWEEN 200-1200 LBS, ITT RISING RAPIDLY TO 900 DEGREE`S. THE POWER WAS REDUCED TO IDLE AND LANDED NORMALLY. TAXIED IN ON IDLE POWER AND SHUTDOWN ENGINE. MX FOUND 1 STAGE COMPRESSOR RUBBING ON HOSDR HSYA2010060210Cable · looseAFTER ROTATION, CAPTAIN REPORTED AN UNCOMMANDED RT ENGINE AUTO FEATHER. THE ACFT RETURNED TO THE AIRPORT WITHOUT FURTHER INCIDENT ARRIVING BACK IN THE BLOCKS FOR MX TROUBLESHOOTING AND EVALUATION AT 1355Z. MX TROUBLESHOT ACFT AND FOUND BETA VALVE OUT OF ADJUSTSDR CA100525018Resistor · overheatedAFT VENT BLOWER LOW SPEED RESISTOR OVERHEATED AND CAUSED SMOKE ODOR IN CABIN. NO FIRE OR SMOKE WAS CREATED.SDR HSYA2010050810Vent · contaminatedPILOT REPORTED TO MX AFTER LANDING, THAT A BURNING PLASTIC/RUBBER SMELL IN CABIN WITH BLEEDS ON, CABIN TEMP SET TO COLD. MX TROUBLESHOT ACFT AND FOUND RUBBISH UNDER PILOT SEAT AIR VENT. REMOVED RUBBISH AND CLEANED AIR VENT IAW MM 12-20-00. MX OPS CHECKS PERFOR
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