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 = '99' 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 = '99' 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 AXSA189WA12/30/10Wire · brokenMHT - DURING THE APPROACH TO LANDING THE NOSE WHEEL GEAR LIGHT FAILED TO ILLUMINATE. PILOT DID A GO AROUND, CIRCLED AIRPORT AT 2000 FT AND RECYCLED GEAR TO MAKE SURE THE LIGHT WAS NOT MALFUNCTIONING. THE TEST LIGHT SHOWED THE THREE GREEN LIGHTS WERE WORKING.SDR 2011FA0000014Sensor · crackedACFT EXPERIENCED "CROSS CHECK ATTITUDE" INDICATION ON AVIONICS PRIMARY FLIGHT DISPLAY (EFIS) AND HEADING INDICATIONS OF UP TO 90 DEGREES OFF LT AND RT WHILE IN CRUISE FLIGHT.SDR CA101207004Resistor · burned(CAN) AFTER LANDING AND DURING TAXI TO THE RAMP, THE CREW NOTICED SMOKE IN THE COCKPIT. MAINTENANCE DETERMINED THE DROPPING RESISTOR FOR THE WINDSHIELD WIPER MOTER HAD OVERHEATED (TC# 20101207004)SDR JDWA147SF1Switch · out of adjustON TAKEOFF ROLL, CABIN DOOR LIGHT CAME ON BEFORE LIFTOFF. PILOT ABORTED TAKEOFF AND WENT BACK TO RUN UP PAD. CHECKED DOOR AND TRIED ANOTHER TAKEOFF, DOOR LIGHT CAME ON BEFORE ACFT LT THE GROUND. RETURNED TO RAMP, MECHANIC RESET DOOR LIGHT SWITCH. SYS FUNCTIOSDR AXSA193WA09/10/10Safety Switch · faultyAFTER TAKEOFF, PILOT TRIED TO RETRACT LANDING GEAR. LANDING GEAR HANDLE WOULD NOT RETRACT GEAR. PILOT SELECTED DOWN AND HAD THREE GREEN LIGHTS AND RETURNED TO MHT WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT PROBLEM TO A FAULTY SAFETY SWITCH ON THE RIGSDR JDWA147F1Landing Gear · malfunctionedAFTER TAKEOFF, THE GEAR IN-TRANSIT LIGHT CAME ON. PILOT RETURNED WITHOUT FURTHER INCIDENT.SDR AXSA195WA08/31/10Switch · out of adjustACFT DEPARTED AT 1112Z, AFTER TAKEOFF, LANDING GEAR WAS RETRACTED AND THE RED GEAR UNSAFE LIGHT WOULD NOT GO OUT. PILOT CYCLED GEAR WITH NO CHANGE. PUT GEAR BACK DOWN AND LANDED WITHOUT INCIDENT. MX DETERMINED THAT THE CAUSE WAS THE UPLOCK INDICATION SWITCHSDR CA100806007Actuator · leakingDURING FLIGHT, THE CREW NOTICED THE HYD PUMP CYCLING. THE CREW PERFORMED AN EMERGENCY EXTENSION AND AN UNEVENTFUL LANDING WAS COMPLETED. MX FOUND THE RT MAIN GEAR ACTUATOR LEAKING FLUID OUT THE RAM. THE ACTUATOR WAS REPLACED.SDR TIMA201000002Cowling · openCOWL OPENED AFTER TAKEOFF. PILOT STATED THAT HE LATCHED THE COWL, BUT THERE IS NO WAY TO VISUALLY CONFIRM THAT THE LATCHES WERE CONNECTED. COWL WAS SUBSTANTIALLY DAMAGED BY BUFFETING.SDR JDWA118SF2Wire · brokenON APPROACH, NO NOSE GEAR DOWN LOCK LIGHT. PILOT CHECKED THE DOWN POSITION BY OPERATING HANDPUMP. LANDED WITHOUT INCIDENT. MECHANIC CALLED OUT, WIRE FROM THE DOWNLOCK SWITCH (PN 1CH25) WAS FOUND TO BE BROKEN. WIRE WAS REPAIRED, SYS OPS CHECK WAS OKAY. PLANESDR AXSA189WA11909Fuel Control · defectiveFLIGHT 1130 PBG-BUF - WHILE ON APPROACH THE PILOT REDUCED POWER AND THE LT ENGINE DID NOT RESPOND. THE PILOT RECEIVED VECTORS OFF THE APPROACH AND DISCOVERED THE ENGINE COULD INCREASE POWER BUT COULD NOT REDUCE POWER. THE PILOT ELECTED TO SHUTDOWN THE LT ENGSDR AXSA189WA11709Linkage · frozenFLIGHT 1130 BUF-PBG - WHILE ON DESCENT TO PBG THE PILOT REDUCED POWER TO THE LEFT ENGINE BUT THE ENGINE DID NOT RESPOND. THE PILOT INDICATED THAT POWER COULD BE INCREASED BUT WOULD NOT REDUCE BELOW 1200LBS/TQ AND 92 PERCENT NG. THE PILOT ELECTED TO SHUTDOWN SDR AXSA192WA102609Diode · shortedDURING A CHECK RIDE POWER TO THE LT BUS FAILED, THE NR 1 INVERTER FAILED AND THE LANDING GEAR WOULD NOT EXTEND. THE PILOTS LOWERED THE LANDING GEAR MANUALLY USING THE EMERGENCY CHECKLIST AND LANDED IN MHT WITHOUT INCIDENT. MAINTENANCE EVALUATION DISCOVERED ASDR HXX2009F00000Nut · brokenTHE NUT ASSY SEEMS TO HAVE SHEARED WHEN GEAR WAS RETRACTED. POSSIBLE OVERTRAVEL IN UP DIRECTION IS SUSPECTED. POSSIBLE FAILURE OF MOTOR CONTROLLER. WHEN GEAR WAS SELECTED DOWN NOTHING HAPPENED. MAIN GEAR ONLY WAS EXTENDED MANUALLY AFTER MUCH EFFORT BECAUSESDR AXSA195WA7/22/09Clevis Bolt · wornFLIGHT 1057 DEPARTED MHT FOR MPV AND AFTER GEAR RETRACTION THE GEAR IN TRANSIT LIGHT REMAINED ILLUMINATED. THE PILOT ATTEMPTED TO RETURN THE GEAR TO THE DOWN POSITION BUT WAS NOT ABLE TO GET PROPER GEAR INDICATIONS THAT THE GEAR WAS DOWN AND LOCKED. THE PILOSDR AXSA189WA6/17/09Fairing · departedAPPROX 20 MILES SOUTH, DURING DESCENT THE PILOT NOTED A LOUD NOISE AND THE ACFT SHUTTERED. ALL INSTUMENTS AND FLIGHT CONTROLS REMAINED NORMAL. THE PILOT SLOWED TO 160KTS AS A PRECAUTION AND LANDED WITHOUT INCIDENT. VISUAL INSP REVEALED THAT THE AFT AERODYNAMICSDR JDWA7994RFire Detector · malfunctionedUPON TAKEOFF ROLL, THE RT FIRE LIGHT CAME ON. PILOT IMMEDIATELY REDUCED POWER AND ABORTED TAKEOFF RUN. LIGHT WENT OUT ENROUTE BACK TO MX FACILITY. NO FIRE OR SMOKE WAS FOUND.SDR AXSA191WA2/6/2009Engine · leakingFLIGHT 1090 MHT-RKD 25 NM FROM DESTINATION RIGHT OIL PRESSURE ANNUNCIATOR ILLUMINATED AND PILOT NOTED OIL PRESSURE AT 20PSI, TORQUE WAS 600 FT-LBS WITH BOTH INDICATIONS WERE FLUCTUATING. NO YAW NOTED. AT 4000FT PILOT REDUCED POWER FOR DESCENT AND RIGHT ENGINSDR CA090205008Thrust Bearing · improper partBECAUSE OF AN ISSUE WITH ANOTHER ACTUATOR OF THE SAME PN THE COMPANY REMOVED THIS ACTUATOR FOR INSP. IT WAS FOUND THAT THRUST BRG ON THIS ACTUATOR WAS OF AN INCORRECT TYPE OR PN. (REF SDR 20090205006) THE TWO ACTUATORS WERE RECEIVED FROM THE SAME COMPANY AT TSDR JDWA118SF1Propeller · power lossON CLIMB OUT, LEFT PROPELLER RPM DROPPED FROM 2200 TO 1900 RPM. PILOT TOOK NOTE AND CALLED IN FOR RETURN. MAINTENANCE HAS NOT DETERMINED THE CAUSE AT THIS POINT, TROUBLE SHOOTING IS CURRENTLY IN PROGRESS, SUSPECTING EITHER PROP GOV OR OVERSPEED GOV.SDR 2009F00001Flap System · malfunctionedDURING FINAL APPROACH, BEFORE REACHING ANEYE INTERSECTION TO RWY 11 PILOT LOWERED FLAPS AND AS THE ACFT REACHED 140KTS LOWERED THE GEAR. WHEN THE GEAR WAS DOWN AND LOCKED THE PILOT NOTED AN ELECTRICAL BURNING SMELL AND, A FEW SECONDS LATER, NOTICED A LITTLE SMSDR CA081209004Mount · worn(CAN) WHILE COMPLETING A 100 HOUR INSPECTION THE UPPER LORD MOUNT WAS FOUND TO BE U/S. BOTH RUBBER HALVES HAD DETERIORATED TO THE POINT THAT RUBBER PIECES WERE CRUMBLING AND FALLING OFF. THERE WERE SMALL PILES OF CRUMBLED RUBBER ON THE TOP OF THE ENGINE. THSDR TIMA20080006Engine · seizedPILOT FELT A POWER SURGE AND SAW FLAMES OUT THE LEFT ENGINE EXHAUST FOR A MOMENT. LEFT PROPELLER STOPPED TURNING. PILOT SECURED ENGINE, CONTINUED ON AND LANDED WITHOUT INCIDENT. INVESTIGATION REVEALED THAT THE PT BLADES WERE MOSTLY GONE. CT BLADES ARE OK. SDR CA080909001Cooling Fan · broken(CAN) WHILE PERFORMING AN INSPECTION, THE ENGINEER PULLED THE STARTER-GENERATOR AND NOTICED THE COOLING FAN BROKEN. UPON FURTHER INVESTIGATION, THE ENGINEER NOTICED THAT 1 OF THE BROKEN FAN BLADES WAS PROVIDING A GROUND PATH INTERNALLY BETWEEN THE GENERATOR ANSDR CA080826002Fcu · failed(CAN) WHEN POWER WAS APPLIED TO ENGINE AFTER A TOUCHDOWN, A CONSIDERABLE YAW TO THE LT WAS FELT BY THE PILOTS. ACFT WAS MOVED OFF THE RUNWAY AND A MAINT RUN-UP OF ENGINES INDICATED A POWER LOSS IN THE LT ENGINE. AFTER TROUBLESHOOTING THE ENGINE A REPLACEMENT SDR 191WA021908Fitting · looseFLIGHT 1064 MHT-BTV DURING APPROACH SELECTED GEAR DOWN. THE GEAR INTRANSIT LIGHT REMAINED ILLUM AND THE LANDING GEAR C/B POPPED. THE GEAR DID NOT EXTEND. RESET THE C/B AND REATTEMPTED GEAR EXTENSION. THE LOW HYDRAULIC LIGHT ILLUM AND THE C/B POPPED AGAIN. SDR JDWA2008SAF01Resistor · blownON MONDAY THE 18TH OF FEBRUARY 2008, BEECH 99, N118SF, S/N U-32, SUBURBAN AIR FREIGHT POSITIONING FLIGHT, ROUTE NUMBER SUBAIR 13 OPERATING UNDER PART 91, DEPARTED OMAHA, NE EN ROUTE TO MOLINE, IL. AT APPROXIMATELY 20:30 HOURS JUST NORTH OF MUSCATINE, IA CENTESDR 191WA21408Heater · faultyFLIGHT 1043 (PWM-MHT) JUST AFTER DEPARTURE THE PILOT NOTED A BURNING SMELL AND SMOKE IN THE COCKPIT COMING FROM UNDER THE INSTRUMENT PANEL FOLLOWED SHORTLY BY THE SOUND OF A POPPING CIRCUIT BREAKER. THE PILOT IDENTIFIED THE CIRCUIT BREAKER AS THE COMBUSTION HSDR 195WA020508Window · leakingAIRCRAFT 195WA DEPART MPV-MHT FLIGHT 1057. 15NM FROM MPV THE PILOT NOTED SPARKS AND SMOKE COMING FROM THE CB PANEL WITH INSTRUMENT PANEL LIGHTS FLICKERING AND ATTITUDE INDICATOR CB POPPED. THE PILOT ADVISED ATC OF THE SITUATION AND RETURNED TO MPV AND LANDEDSDR CA080201001Chain · bent(CAN) DURING CLIMB, A LOUD NOISE WAS HEARD AND THE GEAR FAILED TO RETRACT (3) GREEN INDICATION DURING INSP THE AFT NOSE GEAR CHAIN WAS BROKEN AND THE REMOTE CIRCUIT BREAKER WAS FOUND POPPED NOSE CHAIN AND MASTER LINK REPLACED AND SYS INSPECTED 5 GEAR CYCLES C/SDR CA080117007Engine · failed(CAN) WHILE DOING PILOT TRAINING, THE LT OIL PRESSURE WARNING LIGHT CAME ON. PILOTS LOOKED DOWN AT OIL PRESSURE GAUGE, THE PRESSURE WAS DROPPING SO THEY SHUTDOWN THE ENGINE AND FEATHERED THE PROP. THEY RETURN TO BASE. ENGINE REMOVED FOR FURTHER INSPECTION. (TCSDR CA080117008Sprocket · worn(CAN) DURING INSP OF THE NLG RETRACT MECHANISM CHAIN FOR TENSION AND LUBRICATION, MAINT NOTED THE DUAL LINK CHAIN WAS ONLY RUNNING ON ONE LENGTH OF CHAIN RATHER THAN (2). AC WAS INSPECTED MORE CLOSLEY AND THE BRAZE/SPROCKET ASSY WHICH IS INTERMEDIATE BETWEEN SDR 194WA10232007Powerpack · seizedFLIGHT 1060 MHT-PWM DURING APPROACH FOR RWY 29 PILOT SELECTED GEAR DOWN (3 GREEN LIGHTS INDICATED) AND NOTED THE SMELL OF SMOKE. THE COCKPIT BEGAN TO FILL WITH SMOKE AND THE PILOT NOTED THE LANDING GEAR CIRCUIT BREAKER POPPED. THE PILOT MADE A NORMAL APPROACSDR 195WA101007Indicator · malfunctionedFLIGHT 1058 (MHT-MPV) EN ROUTE PILOT NOTICED SMOKE AND SMELL OF BURNING WIRES IN COCKPIT BETWEEN LEB VOR AND MPV VOR. THE PILOT ELECTED TO CONTINUE TO MPV AND LANDED WITHOUT INCIDENT. MAINTENANCE EVALUATION REVEALED SMOKE COMING FOR WEATHER RADAR INDICATOR. SDR TIMR20070009Actuator · crackedAFTER SELECTING GEAR DOWN ON APPROACH, THE PILOT NOTICED THAT HE DID NOT HAVE A GREEN (SAFE) INDICATION FOR THE NOSE GEAR. HE FOLLOWED THE EMERGENCY PROCEDURE TO PUMP THE GEAR DOWN BUT WAS UNABLE TO BUILD UP PRESSURE OR GET A GREEN LIGHT. PILOT THEN LANDED ANSDR UE5R04Blades · crackedDURING STRETCH CHECK OF TURBINE BLADES P/N T102401-100, FLUORESCENT PENETRANT INSPECTION WAS PERFORMED. THIS INSPECT REVEALED SEVERAL BLADES WITH CRACKS ALONG TRAILING EDGE. THESE CRACKS IN THE DIRECTION OF THE CHORD OF THE BLADE.SDR CA070911008Actuator · stripped(CAN) AFTER TAKEOFF GEAR SELECTED UP RT GEAR DID NOT COME UP. GEAR SELECTED DOWN, (3) GREEN INDICATIONS OBSERVED AC LANDED. AC BROUGHT INTO HANGER AND PUT ON JACKS RT MLG ACTUATOR REMOVED. FOUND THAT NUT, ACTUATOR P/N 115-810029-24 HAD NO TREADS IN IT. PASDR CA070815003Engine · damaged(CAN) DURING TAKEOFF ROLL, (JUST PRIOR TO VR) A LOUD POP WAS HEARD. THE AC CONTINUED WITH THE TAKEOFF AND ONCE AIRBORNE THE CREW DIVERTED BACK TO DEPARTURE AIRPORT FOR LANDING. AS THEY WERE COMING AROUND, THE PROP RPM, TORQUE, AND FUEL FLOW ON THE RT ENGINE BESDR CA070424008Hydraulic Line · ruptured(CAN) DURING APPROACH TO LAND THE CREW EXTENDED THE LANDING GEAR AND NOTICED THE NOSE GEAR WAS NOT DOWN AND LOCKED. THE EMERGENCY GEAR EXTENSION WAS ACTIVATED AND THE NOSE GEAR WAS LOCKED IN THE DOWN POSITION. THE AC LANDED WITHOUT INCEDENT. UPON INSP BY MAINTSDR CA070423007Probe · intermittent(CAN) BATTERY TEMP MONITOR WAS INDICATING HIGHER THAN NORMAL ON APPROACH. AIRCRAFT LANDED WITHOUT INCIDENT. BATTERY WAS LUKEWARM TO THE TOUCH. MONITOR WAS UNRESPONSIVE. BATTERY AND PROBE WERE REPLACED ALONG WITH WIRING INSPECTED AND AIRCRAFT RETURNED TO SERSDR CA070416002Probe · cracked(CAN) 7 OUT OF 8 T5 INDICATION PROBES WERE FOUND WITH LOOSE OR BROKEN TERMINALS AND MISSING CERAMIC INSULATION. THE PROBES APPEAR TO QUITE FRAGILE IN COMPARISON TO THE OEM PART. THE PARTS IN QUESTION ARE PMA PARTS, THEIR PN 26584. PROBES REPLACED AND AIRCRASDR AXS2007F00001Fire Detector · shortedDURING CLIMB OUT, THE LT ENGINE FIRE WARNING LIGHT CAME ON. THE PILOT DECLARED AND EMERGENCY, RETURNED TO BASE, LANDED WITHOUT INCIDENT. THE PILOT DID NOT SEE FLAMES OR SMOKE COMING FROM THE ENGINE AND DID NOT HAVE ANY OTHER INDICATIONS OF AN ENGINE FIRE, TSDR CA070220002Engine · making metal(CAN) CREW CALLED IN ON LANDING TO INFORM MAINTENANCE THAT THE RT CHIP LIGHT HAD ILLUMINATED. MAINTENANCE FOUND ENGINE HAD METAL IN OIL. ENGINE WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. THIS ENGINE WILL REQUIRE FURTHER INVESTIGATION AS TO THE CAUSE OF SDR CA060731002Planetary Gear · making metal(CAN) METAL CONTAMINATION WAS FOUND ON THE CHIP DETECTOR. METAL ORIGINATED FROM RGB AND WAS THE RESULT OF SIGNIFICANT MATERIAL LOSS BETWEEN THE 1ST STAGE SUN GEAR AND THE 1ST STAGE PLANETARY GEARS. THIS IS OUR 2ND SUCH CASE WITH TIME CONTINUED GEARS. (TC NR 2SDR CA060622002Drain · broken(CAN) AFTER FUELING THE AIRCRAFT THE FIRST OFFICER HEARD A SPLASH AND FOUND FUEL LEAKING FROM UNDER THE LEFT WING. THE T PORTION OF THE FUEL DRAIN HAD FALLEN OUT AND THERE WAS NO WAY TO SHUT THE QUICK DRAIN VALVE OFF. THE TOP PART OF THE VALVE AND ORING WERESDR AXS2006F00002Actuator · failedPILOT SELECTED GEAR DOWN BUT DID NOT RECEIVE ANY GREEN LIGHTS INDICATING GEAR DOWN AND LOCKED. PILOT EXECUTED MANUAL GEAR EXTENSION CHECKLIST AND RECEIVED 3 GREEN LIGHT AND THEN EXECUTED A FLY-BY WHERE TOWER OBSERVED GEAR TO BE EXTENDED. PILOT LANDED AND AS SDR CA060704002Gearbox · spalled(CAN) THE ENGINE CHIP DETECTOR WARNING ANNUNCIATED IN FLIGHT. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT DIVERTED TO AN ALTERNATE AIRPORT. SUBSEQUENT INSPECTION REVEALED SPALLING OF THE FIRST STAGE REDUCTION GEARBOX GEARING. (TC# 20060704002)SDR CA060531012Engine · making metal(CAN) IN CRUISE, THE CHIP LIGHT ACTIVATED ON THE LT ENGINE. THE ENGINE WAS SHUTDOWN AS A PRECAUTION AND THE AIRCRAFT DIVERTED TO NEAREST FIELD FOR NORMAL LANDING. CFR WAS REQUESTED TO BE ON STANBY. THERE WAS NO OTHER INDICATIONS OF ENGINE PROBLEMS. THE CHIPSDR CA060516003Actuator · crackedROUTINE VISUAL INSPECTION OF THE FLAP ACTUATORS INDICATED THAT THE OUTBOARD ATTACHMENT FLANGE OF THE RT OUTBOARD FLAP ACTUATOR WAS CRACKED. THERE WAS NO EVIDENCE OF THE ACTUATOR BEING DROPPED OR OTHERWISE ABUSED. THE FLANGE WAS BENT SLIGHTLY INBOARD AND THERSDR CA060512002Boot · departed(CAN) DURING MAINT WALK AROUND, COMPLETE PROP BLADE DE-ICE BOOT HAD DEPARTED AC. AIRFRAME, ENG WAS INSPECTED FOR FOD DAMAGE FROM DE-ICE BOOT. DETERMINED THAT BOOT HAD SEPERATED FROM AC DAY BEFORE DURING TAKE-OFF. PILOT FELT VIBRATION FROM LT ENG DURING RUN-U
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