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 CA160125006Fuel Control · failed(CAN) REJECTED TAKEOFF BY FLIGHT CREW WHO REPORTED NO POWER ON LT ENGINE. AS FLIGHT CREW TAXIED BACK POWER RETURNED AND ENGINE STABLE BUT SLOW RESPONSE TO POWER INPUT.SDR YADA2015122201Connector · corrodedHAD TO PUMP GEAR DOWN TO GET THREE GREEN, NOSE GEAR HAD NOT INDICATED GREEN. NO IN-TRANSIT LIGHT. FERRY GEAR DOWN. MX COULD NOT DUPLICATE. GEAR RETRACT & EXTEND, OPERATIONS CHECKED GOOD MULTIPLE TIMES. REPLACED NOSE GEAR DRAG BRACE DOWN LOCK SWITCH FOR COSDR YADA20151215001Gyro · faultyCOPILOT ATTITUDE INDICATOR SHOWING 5 - 10°, BANK TO RIGHT DURING LEVEL FLIGHT. RETURN TO AIRPORT OF DEPARTURE. REPLACED INOPERATIVE ATTITUDE GYRO, CHECKED GOOD.SDR YADA20151212001Dimmer · shortedROLLING FOR TAKEOFF, ENG INSTRUMENTS INOPERATIVE FOLLOWED BY ELEC BURNING SMELL & POPPED CB. LOCATED & REPLACED LIGHTING DIMMER CONTROL & POWER SUPPLY FOR INSTRUMENT LIGHTS. CONFIRMED INTERNAL FAILURE OF UNIT.SDR CA151204005Line · cracked(CAN) DURING INSTALLATION OF THE FUEL MOTIVE LINE IN THE RT WING ROOT IT WAS NOTICED THAT THE B-NUT TUBE SLEEVE WAS CRACKED.SDR TIMA2016F00020Bleed Air Sys · smokeENROUTE, THE LT BLEED FAIL WARNING ILLUMINATED. WHILE FINISHING THE CHECKLIST FOR THE FAILURE SMOKE ENTERED THE CABIN OF THE AIRCRAFT. ELECTED TO CONDUCT A LANDING. UPON LANDING, THE SMOKE DISSIPATED FROM THE CABIN OF THE AIRCRAFT.SDR CA151203004Governor · malfunctioned(CAN) THE PROPELLER WOULD FLUCTUATE +/- 400 FT/LBS IN TORQUE DURING CLIMB AND DESCENT. ORIGINALLY THE BETA CABLE CLEVIS AND JAM NUT WERE ADJUSTED AND BETA ARM AND BLOCK REPLACED. WHEN THE EVENT REOCCURRED THE PROP GOVERNOR WAS REPLACED WITH NO RECURRENCE SINCSDR YADA20151130001Uplock Switch · shortedLANDING GEAR UNSAFE INDICATION, AFTER RETRACTION, RED LIGHT IN HANDLE. ACFT LANDED UNEVENTFULLY AT AIRPORT OF ORIGIN. IDENTIFIED & REPLACED A FAULTY NOSE GEAR UPLOCK INDICATION SWITCH, SWITCH WAS FOUND TO HAVE CONTAMINATION & CORROSION ON TERMINAL CONTACTS USDR TIMA20151127009Computer · faultySTALL WARNING HORN SOUNDED CONTINUOUSLY FROM THE TIME THE ACFT TOOK OFF. PILOT ELECTED TO RETURN TO TAKEOFF AIRFIELD FOR AN UNEVENTFUL LANDING. SUBSEQUENT INSPECTION REVEALED THE LIFT DETECTOR COMPUTER WAS FAULTY.SDR YADA20151124001Oil System · out of adjustOIL PRESS ON RT ENG 141 PSI. CREW ELECTED TO RETURN TO AIRPORT OF DEPARTURE & UNEVENTFUL LANDING MADE. ADJUSTED OIL PRESS DOWN TO LIMIT.SDR YADA20151123001Heating Element · overheatedLEFT PILOT SIDE, PROP DE-ICE GLOWING ORANGE WHEN IN USE. ACFT RETURNED TO AIRPORT OF DEPARTURE, DUE ICING CONDITIONS. UNEVENTFUL LANDING MADE. OBSERVED DAMAGED HEATING ELEMENT IN ON PROP BLADE DE-ICE BOOT. PROPELLER WAS REPLACED.SDR TIMA20151120008Terminal · corrodedAFTER TAKEOFF, WHEN GEAR SELECTED UP, THEY FAILED TO RETRACT. PILOT RETURNED TO TAKEOFF AIRFIELD FOR UNEVENTFUL LANDING. SUBSEQUENT INSPECTION FOUND THE LG POWER CB POPPED & CORROSION ON THE CB TERMINALS.SDR YADA20151105001Hydraulic Line · leakingAFTER TAKEOFF & LG RETRACTION, PILOT NOTICED HYD POWER PACK RUNNING EXCESSIVELY, THEN LOW HYD WARNING LIGHT CAME ON. MANUALLY EXTENDED THE LG & RETURNED TO ORIGINAL AIRPORT FOR AN UNEVENTFUL LANDING. AFTER LANDING, HYD FLUID WAS OBSERVED LEAKING FROM THE HYDSDR JIKA2015110201Motor · malfunctionedAFTER TAKEOFF THE PILOT NOTICED A SMOKE SMELL IN COCKPIT. THE PILOT NOTIFIED THE TOWER & DECLARED AN EMER. THE PILOT RETURNED & LANDED WITHOUT INCIDENT. TROUBLESHOOTING REVEALED A FAULTY ELEC FLAP MOTOR & GEAR BOX ASSEMBLY. REPLACED ELEC FLAP MOTOR & GEAR SDR JIKA2015103001Tube · collapsedEN-ROUTE THE PILOT NOTICED THE RT ENG OIL PRESS WARNING LIGHT ILLUMINATED & THE OIL PRESS INDICATION WAS AT 60 PSI & IN THE YELLOW ARC. THE PILOT REDUCED THE POWER ON THE RT ENG. DECLARED AN EMER, DIVERTED & LANDED WITHOUT INCIDENT. INSPECTED THE RT ENG, OISDR YADA20151009001Clevis Pin · missingPILOT REPORTED COPILOT RT RUDDER PEDAL DISCONNECTED FROM MASTER CYLINDER. REPLACED A MISSING CLEVIS PIN & RELATED COTTER PIN.SDR EPUA201510070003Uplock Switch · shortedLANDING GEAR, NOSE, DID NOT COMPLETE UP CYCLE AFTER RETRACTION. WHEN GEAR WAS EXTENDED AN ALTERNATE EXTENSION PROCEDURE WAS REQUIRED TO GET THE NLG TO INDICATE DOWN & LOCKED.SDR TIMA20151004005Fastener · missingDURING TAKEOFF ROLL, THE RT POWER LEVER DID NOT PROVIDE FULL TRAVEL. TAKEOFF TORQUE COULD NOT BE ACHIEVED ON THE RT ENG & THE TAKEOFF WAS ABORTED. SUBSEQUENT INSPECTION REVEALED A MISSING FASTENER IN THE POWER LEVER CLAMP BRACKET UNDER THE PEDESTAL.SDR YADA20150930001Fan · failedPIREP SMELL OF ELEC BURNING IN FLIGHT. CREW ELECTED TO RETURN TO DEPARTURE AIRPORT & LANDED WITHOUT INCIDENT. MX VERIFIED THE RECIRCULATION FAN HAD INTERMITTENT GRINDING SOUND & SEIZING, DEFERRED. ACFT RETURNED TO BASE WITHOUT INCIDENT. FAN TO BE REPLACED.SDR TIMA20150915004Seat Track · corrodedDURING MX, THE RT SIDE SEAT RAIL WAS FOUND TO BE CORRODED.SDR TIMA20150715003Seat Track · corrodedDURING MX INSPECTION, THE LT SIDE SEAT RAIL WAS FOUND TO BE CORRODED.SDR YADA20150904001Wire · shortedPILOT REPORTED ELEC SMELL IN COCKPIT AFTER DEPARTURE. RETURNED TO ORIGINAL AIRPORT FOR UNEVENTFUL LANDING. LOCATED A PINCHED & SHORTED WIRE ON THE AFT RECIRCULATING FAN AT THE RESISTOR STACK. FAN UNIT REPLACED.SDR YADA20150819001Turbine Blades · damagedWHILE INVESTIGATING RISING ENG ITT TREND, FOUND SIGNIFICANT DAMAGE TO COMPRESSOR SHROUD SEGMENTS & CT BLADES. CAUSE OF DAMAGE APPEARS TO BE FROM EXCESSIVE CARBON BUILD UP ON THE COMBUSTION LINER COMING LOOSE & ABRADING SEGMENTS & CT BLADES TO THE POINT THE SESDR EPUA2015080415002Bracket · bentDURING APPROACH THE GEAR WAS SELECTED DOWN & THE GEAR DOWN ANNUNCIATOR DID NOT ILLUMINATE. DECLARED AN EMER & LANDED WITHOUT INCIDENT. INSPECTED ACFT & DETERMINED THAT DRAG BRACE BRACKET PN 114-820077-3 WAS DEFORMED & NOT ALLOWING THE NLG SWITCH TO ACTUATE PSDR CA150817022Wire · damaged(CAN) YAW DAMPENER CONTROL BREAKER POPS AFTER THE COMPASS FLAG PULLS ON THE HSI. FOUND SEVERAL WIRES BARE AND SHORTING IN CAPTAINS CONTROL COLUMN CURLY CORD. CORD WIRES RE-TERMINATED AND YAW DAMPER TESTED SERVICEABLE.SDR YADA20150725001Warning Light · inoperativeLANDING UNSAFE LIGHT & LANDING POSITION LIGHT INOPERATIVE DURING LANDING. PERFORMED FLYBY & EMERGENCY GEAR EXTENSION IAW QRH. AN UNEVENTFUL LANDING WAS PERFORMED & NO EMERGENCY WAS DECLARED. ALL GEAR DOWN & LOCKED GREEN LIGHTS ILLUMINATED ON ROLLOUT AFTER LSDR CA150723006Collar · worn(CAN) AFTER TAKE OFF, ON INITIAL CLIMB BELOW 1000 FEET, THE LEFT PROPELLER RPM DROPPED RAPIDLY TO APPROX. 6 TO 700 RPM. TORQUE INCREASED TO 4300 FT/LBS BEFORE THE INCREASE WAS ARRESTED. THE PLANE WAS HANDLING POORLY AND THERE WERE CONCERNS THAT THE PROPELLER WSDR TIMA20150620002Downlock Switch · out of adjustON APPROACH FOR LANDING, NOSE GEAR DOWN LIGHT FAILED TO ILLUMINATE. ACFT LANDED UNEVENTFULLY. UPON TOUCHDOWN THE NLG DOWN LIGHT ILLUMINATED. INSPECTION REVEALED THE NLG DOWNLOCK SWITCH WAS OUT OF ADJUSTMENT.SDR YADA20150522001O-Ring · damagedPILOT REPORTED APPEARANCE OF SMOKE IN COCKPIT AT TOUCHDOWN. REPORTED AS POSSIBLY COMING FROM BLEED AIR, OILY SMELL. CORRECTED AN OIL LEAK AT THE LT OIL COOLER INBD FITTING & REPLACED O RING AT FITTING, CLEANED DUCTING AS REQUIRED. OIL LINE AT LEAKING FITTINSDR YADA20150502001Windshield · crackedAFTER DEPARTURE, LT FWD WINDSHIELD OUTER PANE CRACKED. CREW ELECTED TO RETURN TO ORIGINAL AIRPORT & MADE AN UNEVENTFUL LANDING. REPLACED THE WINDSHIELD.SDR CA150501005Drive Shaft · broken(CAN) THE END OF ITS LIFE DRIVE SHAFT HEAD BROKE OFF AT THE ACTUATOR.SDR EPUA20150428003Fuel Line · chafedDURING A FLEET CAMPAIGN DIRECTIVE INSPECTION, DUE TO A PREVIOUS FAILURE IN WHICH THE ENG LOST POWER & LEAKED FUEL, THE LT ENG WAS FOUND TO HAVE A CHAFED ENG FUEL TUBE, PN 3040637. DUE TO THE LEVEL OF CHAFING THE FUEL TUBE NEEDED TO BE REPLACED. THE FUEL TUBESDR EPUA2015042815002Fuel Line · chafedDURING A FLEET CAMPAIGN DIRECTIVE, DUE TO A PREVIOUS FAILURE IN WHICH THE AN ENG LOST POWER & LEAKED FUEL, THE LT ENG WAS FOUND TO HAVE A CHAFED ENG FUEL TUBE, PN 3040637. DUE TO THE LEVEL OF CHAFING THE FUEL NEEDED TO BE REPLACED. THE FUEL LINE WAS FOUND TOSDR EPUA20150429001Fuel Line · chafedNUMBER 1 ENG FUEL LINE, PN 3040637, WAS INSPECTED & FOUND TO HAVE CHAFING THAT EXCEEDED THE LIMITS FOR CONTINUED SERVICE. WE HAVE ELECTED TO INSPECT ALL OF OUR ACFT FOR THIS DEFECT & HAVE DISCOVERED OTHERS REQUIRING PART REPLACEMENT. SB 13250R1, OPTIONAL, ADSDR EPUA20150428001Tube · leakingPILOT ABORTED TAKE OFF DUE TO LOW AND FALLING TORQUE ON LEFT ENGINE. MAINTENANCE INSPECTED LEFT ENGINE AND DETERMINED THAT THE FUEL PRESSURE DELIVERY TUBE (PN: 3040637) HAD DEVELOPED A LEAK. CHAFFING HAD OCCURRED BETWEEN THE FUEL DELIVERY TUBE AND THE STARTESDR CA150427015Door · out of alignment(CAN) PILOT NOTICED THAT THE CABIN DOOR HANDLE IN THE CLOSED & LOCKED POSITION DID NOT LINE UP WITH THE DOOR PLACARD & THAT IT HUNG DOWN FROM ITS NORMAL CLOSED POSITION, STREAMLINE OR PARALLEL WITH THE WL. INSPECTION OF THE DOOR & ITS LOCKING MECHANISM WAS CASDR YADA20150410001Terminal · faultyAFTER TAKEOFF, CREW REPORTED SEEING & SMELLING ELEC SMOKE FROM BEHIND THE FUEL QTY PANEL. THE CREW DEPLOYED OXYGEN MASKS & MADE AN UNEVENTFUL EMER LANDING AT THE AIRPORT OF ORIGIN. THE CREW REPORTED THE SMOKE & ODOR HAD DISSIPATED UPON LANDING. NO SYS FAULTSDR YADA2015040800104Windshield · crackedFLIGHT CREW REPORTED THAT THE RT WINDSHIELD OUTER PANE CRACKED ON CLIMB OUT. THE CREW ELECTED TO RETURN. LANDING UNEVENTFUL. WINDSHIELD REPLACED.SDR JIKA2015031701Exhaust Stack · leakingDURING CRUISE FLIGHT, PILOT NOTICED THE RT FIRE PULL, HANDLE ILLUMINATED, THE PILOT FOLLOWED THE CHECKLIST PROCEDURES IN THE FLIGHT MANUAL & PERFORMED AN INFLIGHT SHUT DOWN OF THE RT ENG. THE PILOT DECLARED AN EMER, RETURNED & LANDED WITHOUT INCIDENT. INSPECSDR JIKA2015031301Wire · chafedDURING CRUISE ON TRAINING FLIGHT, THE PILOT SIMULATED AN ENG FIRE BY TESTING AMP SIDE OF THE LT FIRE SYS TO ILLUMINATE THE FIRE WARNING T HANDLE. THE RED LIGHTS ILLUMINATED FOR APPROX ONE SECOND & THEN EXTINGUISHED, DESPITE THE SWITCH STILL BEING DEPRESSED. SDR CA150413006Bearing · failed(CAN) ACFT LOST OIL PRESSURE ON THE RT ENGINE IN FLIGHT. THERE WAS A LOUD "BANG" HEARD AND A FLAME WAS THOUGHT TO HAVE BEEN NOTED COMING FROM THE EXHAUST. THE FIRE BOTTLE WAS BLOWN. IT WAS FOUND THAT THERE WAS NO ENGINE FIRE, NO FUEL LEAKS WERE NOTED AND NSDR CA150325015Oil System · low pressure(CAN) DURING CRUISE, PILOTS NOTED NR 2 ENGINE OIL PRESSURE DROPPING, THIS WAS QUICKLY FOLLOWED BY A LOW OIL PRESSURE WARNING LIGHT. CREW REPORTED A LOUD NOISE AND THE ENGINE SPOOLED DOWN. THE CREW SECURED ENGINE AND ACTIONED THE ENGINE FIRE BOTTLE. DECLARED SDR YADA2015021915001Yoke · seizedON DAILY INSPECTION MX FOUND THE NLG ACTUATOR YOKE TO DRAG BRACE BOLE SHEERED ON ONE SIDE OF THE BRACE. THE BOLT WAS FOUND TO BE SEIZED IN THE YOKE. DRAG BRACES & ACTUATOR YOKE WERE REPLACED. EXTRA CARE MUST BE USED TO VERIFY THAT LUBRICANT IS ACTUALLY FLOWSDR CA150218002Conduit · unsecure(CAN) THE CREW REPORTED THAT THEIR ELEVATOR TRIM WAS LOCKED IN 2 DEGREES UP WITH NO RESPONSE IN MANUAL MODE. THE ACFT WAS UNDER CONTROL AT ALL TIMES & LANDED SAFELY.
INSPECTED THE SYS FOR ISSUES & FOUND THAT THE TWO GUIDE TUBES, CONDUITS, THAT STOP THE CABSDR YADA20150123001Mount Bracket · crackedNOSE WHEEL STEERING VERY DIFFICULT TO USE. HARD TO MANIPULATE RUDDER PEDALS WHILE ON GND. FOUND LT RUDDER BELLCRANK MOUNT BRACKET LOOSE WITH ONE CRACKED MOUNT EAR, ALLOWING BELLCRANK TO RUB. REPLACED BRACKET & COMPLIED WITH RECOMMENDED SERVICE BULLETIN SB27SDR EPUA20150116001Unknown · malfunctionedPILOT REPORTS THAT THERE IS A LOSS IN CABIN PRESS DURING FLIGHT. NO EMER ACTIONS WERE REQUIRED. ACFT LANDED SAFELY AT ITS SCHEDULED LOCATION & THE PRESSURIZATION SYS WAS DEFERRED.SDR YADA20141223001Cable · brokenATTEMPTING TO DEPLANE, AIR STAIR DOOR WOULD NOT OPEN. FOUND ONE DOOR CAM OPERATING CABLE HAD BROKEN.SDR YADA20141222001Handle · brokenPILOT REPORTED AIR STAIR DOOR OPERATION VERY STIFF, INSIDE DOOR HANDLE BROKE WHILE TRYING TO OPEN. REPLACED DOOR HANDLE & LUBED DOOR SYS.SDR YADA20141218001Hydraulic Line · rupturedON APPROACH FLIGHT CREW SELECTED LANDING GEAR DOWN. THE NOSE GEAR FAILED TO COMPLETELY EXTEND & LOCK, LANDING GEAR PUMP CONTINUED TO RUN. THE PILOT PULLED THE LG CB & THEN THE HYD LOW LEVEL ANNUNCIATOR ILLUMINATED. THE PILOT COMPLETED THE GEAR EXTENSION WITSDR CA141218018Starter Gen · failed(CAN) THE RIGHT STARTER GENERATOR FAILED ON DECEMBER 17TH 2014 WITH ONLY 399.6 HOURS SINCE OVERHAUL. THE OVERHAUL INTERVAL FOR THESE STARTER GENS, OPERATOR ESTABLISHED OH TIME, IS 1000 HRS. THE LAST OVERHAUL WAS COMPLETED 06/18/2013.
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