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 = 'A185F' 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 = 'A185F' 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 CA060516004Reinforcement · crackedEXCESSIVE MOVEMENT FOUND AT AFT LT HINGE ASSY, INSIDE REINFORCEMENT P/N 0732106-1, ALSO FOUND CRACKED.SDR CA060518003Strut · shearedDURING TOUCH DOWN, INSTRUCTOR HEARD THE VOICE ADVISORY SYSTEM WITH THE MESSAGE "CHECK GEAR" AND LOST THE LIGHT ON THE BLOCK INDICATOR P/N 2A11179-001 ON THE RIGHT AND SIDE. DECIDED TO LAND ON LAKE WITH SMALLER WAVE WITH NO PROBLEM. THE INSTRUCTOR FOUND THE SDR 2006FA0000485Jackscrew · strippedMAINTENANCE PERSONNEL WERE ADVISED BY THE PILOT THE HORIZONTAL STABILIZER TRIM QUIT WORKING. INSPECTION FOUND THE BARREL SIDE OF THE TRIM SCREW JACK HAD STRIPPED OUT. THE SYSTEM INCLUDES 2 TRIM SCREW JACKS THE OTHER TRIM SCREW JACK TOOK ALL OF THE LOAD AND JSDR CA060509001Flap Track · cracked(CAN) LT IB FLAP TRACK, FWD ANGLES, AGAINST SPAR FOUND CRACKED AT BEND RADIUS, LOWER END. (TC NR 20060509001)SDR CA060515005Spar · cracked(CAN) 1) SPAR (P/N 0732602-2 2) REINFORCEMENT (P/N 0732603-1 3) BRACKETS (P/N 0732101-4 ALL 3 OF ABOVE ITEMS WERE FOUND CRACKED AND REPLACED. (TC NR 20060515005).SDR CA060425002Rib · crackedRIGHT WING RIB AT STN 40.125 AFT UPPER FLANGE CRACKED ALONG BEND RADIUS.SDR CA060116007Bracket · brokenUPON APPROACH TO LAND ON LAKE, FLAPS 10 SELECTED. A/C IMMEDIATELY BEGAN TO ROLL TO LT, RETURNED FLAPS TO ZERO, A/C RETURNED TO LVL FLT. TRIED TO DEPLOY FLAPS AGAIN (SLOWLY) AND OBSERVED RT FLAP DEPLOYED NORMALLY, LT FLAP DID NOT MOVE, A/C THEN RETURNED TO WSDR CA051221001Hinge · misrepairedUPON INSPECTION, MAINTENANCE PERSONNEL DISCOVERED SEVERAL PLACES WHERE NAILS AND LOCK PINS WERE USED IN PLACE OF THE PROPER NAS561 PINS. SAFETYING METHOD WAS "BENT OVER" INSTEAD OF LOCK WIRE. LOCATIONS WERE TRIM WHEEL, SEAT BACK HINGE POINTS AND SEAT LOCK MESDR 2006FA0000091Landing Gear · lack of lubeRT MAIN GEAR, NO GREEN GEARDOWN LIGHT. GEAR CYCLED SEVERAL TIMES, RT MAIN GEAR COLLAPSED AFTER LANDING. REMOVED GEAR ASSY FOUND LACK OF LUBE THE PROBLEM. REPLACED PARTS, BENT WHEN GEAR COLLAPSED. LUBED, REINSTALLED. OPS OK. LUBE GEAR MORE OFTEN. (K)SDR 2005FA0001498Encoder · failedFOLLOWING INSTALLATION OF A NEW GNS480, DURING INITIAL POWER CHECKS, FOUND THE FOLLOWING FAILURE FLAGS DISPLAYED: COM COMUNICATION FAILURE, NAV COMMUNICATION FAILURE, ALTITUDE ENCODER COMMUNICATION FAILURE. INSTALLATION OF ANOTHER UNIT RESOLVED THE PROBLEMS. SDR CA051108008Injector · contaminated(CAN) FULL POWER NOT AVAILABLE FOR TAKEOFF. STATIC RPM 150 RPM LOW. ENGINE SLIGHTLY ROUGH. REMOVED INJECTORS AND FOUND UNIDENTIFIED PARTICLE IN NR5 INJECTOR. REMOVED PARTICLE AND ENGINE RAN NORMALLY.SDR 2005FA0001079Magneto · damagedPERFORMED MAGNETO CHECK AND FOUND LT MAGNETO DROPPED 500 RPM. REMOVED MAG AND FOUND IMPULSE COUPLING RIVETS SHEARED, DRIVE GEAR BUMPER RETAINER BROKEN AND BUMPERS DAMAGED. REMOVED OIL FILTER AND FOUND METAL SHAVINGS.SDR CA050815002Line · corroded(CAN) DURING TROUBLESHOOTING, FOUND FUEL CROSS-FEED LINE ROUTED THROUGH RT DOOR POST WEEPING FUEL. PORTION OF LINE REMOVED AND UPON FURTHER EXAMINATION A PIN-HOLE CAUSED BY CORROSION WAS FOUND UNDER PLASTIC ANTI-CHAFE MATERIAL. SUSPECT CONDENSATION OVER MANY YSDR CA050526005Lock · broken(CAN) ADULT MALE WAS ADJUSTING HIMSELF IN THE FRONT RT SEAT WHEN THE SEAT COLLAPSED REARWARD. PASSENGER WAS QUITE LARGE, 250 LBS PLUS. PART FAILED AT THE FORWARD ATTACH CRIMP. WHERE IT CRIMPS ON TO THE SPLINE.SDR CA050614009Crankshaft · fractured(CAN) CRANKSHAFT FRACTURED AT NR 2 MAIN BEARING JOURNAL FILLET NEXT TO NR 3 CHEEK. FAILURE IS IN LINE WITH NR 2 CONNECTING ROD JOURNAL IN AREA WHERE CRANKSHAFT IS INSPECTED FOR SUB-SURFACE CRACKS BY UT. MAIN BEARINGS WERE POUNDED TO VERY THIN METAL PIECES. NSDR CA050530008Alternator · failed(CAN) ALTERNATOR FAILED IN FLIGHT. REPLACED UNIT.SDR 2005FA0000652Pawl · wornAPPEARS THAT THE STEERING LOCK PAWL DID NOT ENGAGE SUFFICIENTLY TO LOCK THE TAIL WHEEL. UPON LANDING THE TAIL WHEEL CASTORED. SWINGING THE AC TO THE RT AND OFF OF THE RUNWAY. AC SUSTAINED DAMAGE TO ITS LT WING. INVESTIGATION DISCLOSED THAT THE TAIL WHEEL SSDR 2005FA0000937Bracket · brokenPILOT REPORTED THAT THE FLAPS FELT FUNNY AND THAT THEY MADE A GRINDING NOISE. INSPECTION OF FLAP SYSTEM FOUND PULLEY BRACKET FOR LT FLAP EXTEND CABLE HAD BROKEN AT 2 OF THE 4 MOUNTING SCREW TABS.SDR 2005FA0000814Piston · crackedREMOVED CYLINDERS ON A FRESHLY OVERHAULED ENGINE PRIOR TO RUNNING AND FOUND A 3 INCH CRACK AROUND THE OIL RING LANDING. (K)SDR CA050316005Hub · cracked(CAN) MCCAULEY PROPELLER D2A34C58, WORK ORDER NR T 65243 C-XX PROPELLER RECEIVED FOR 10 YEAR OVERHAUL. LAST OVERHAUL MAR 1989. 5 YEAR CORROSION INSPECTION JUNE 1994, 259.9 HOURS SINCE OVERHAUL. NOW 889.2 HOUR SINCE OVERHAUL. FOUND HUB CRACKED IN ONE BLADE SSDR CA050329012Battery · shorted(CAN) AFTER TAKEOFF FROM AIRPORT THE PILOT SMELLED THE BATTERY OVERCHARGING, HE NOTICED THE ALTERNATOR AMPMETER CHARGING AT APPROXIMATELY 60 AMPS. THE PILOT TURNED OFF THE ALTERNATOR AND MASTER SWITCHES AND PROCEEDED INTO THE AIRPORT USING HIS CELL PHONE AS CSDR CA050218001Gearbox · cracked(CAN) ON LANDING I HEARD A FAINT CRACKING SOUND, AS I TAXIIED OF THE RUNWAY. THE LT WING THEN DROPPED ABOUT 18 INCHES BEFORE COMING TO A STOP. THE WING ENGINE DID NOT TOUCH THE GROUND. THIS WAS OUR SECOND SKI TRIP OF THE DAY. UPON CHECKING WE DISCOVERED THE SDR L1K2005F00000Master Cylinder · contaminatedAC LANDING AT BELOW FREEZING TEMP, HAD BRAKES LOCKING UP (FROZE UP) ON LANDING. INSP AFTER INCIDENT FOUND DIRT AND DEBRIS ALONG WITH CONTAMINATED FLUID (WATER) IN BOTTOM OF BOTH RT AND LT BRAKE MASTER CYL PN 0541139-22 WHEN REMOVED. CYL BODIES SHOWED NO SIGNSDR 2005FA0000297Alternator · corrodedLOW VOLTAGE LIGHT COMES ON OCCASIONALLY-RESET SWITCH AND OPERATES NORMAL. FOUND BRUSHES WORN OUT IN ALTERNATOR. REMOVING ALTERNATOR WAS EXTREMELY DIFFICULT. MOUNTING BOLT WAS FROZEN IN ALTERNATOR. USING PENETRANT HELPED TO FREE THE BOLT. DISCOVERED THAT FACILSDR CA050203003Housing · cracked(CAN) DURING ROUTINE 500 HOURS INSPECTION, BOTH MAGNETO HOUSINGS WERE FOUND CRACKED IAW FIGURE 716 OF MFG MASTER SERVICE MANUAL X40000.<AGMETPS (2) - P/N SGRN-1225S/N 653290R S/N 653291SDR CA041222010Nut · cracked(CAN) RETENTION NUT THREAD CRACKED, 3 INCHES IN LENGTH, . DISCOVERED DURING OVERHAUL L.P.I. INSPECTION.SDR CA041120001Engine · making metal(CAN) DURING 200 HR. INSP. THE OIL FILTER WAS CUT OPEN TO LOOK FOR METAL. FILTER ELEMENT WAS WASHED IN VAROSOL AND DRAINED THROUGH A FILTER TO REVEAL METAL PARTICLES. THE ENGINE SHOP WAS CALLED TO IDENTIFY THE METAL. WE PULLED NR 2 & 4 CYLINDERS TO OBSERVE TSDR CA041026008Cylinder Head · separated(CAN) NR 3 ALUMUNUM HEAD SEPERATED AT 3RD FIN ABOVE BARRIER. ALL 6 CYLINDERS REPLACED. CYLINDERS THAT WERE REMOVED SENT BACK TO MFG FOR MATERIAL EXAMINATION.SDR CA041017001Crankcase · cracked(CAN) THE CESSNA 185 WAS RETURNING TO HOME BASE FROM THE HUNTING CAMP, WHEN IN CRUISE,WITH ALL ENGINE PARAMETERS INDICATING NORMAL,THE ENGINE STOPPED IN FLIGHT AND T HE SEASONED PILOT WAS ABLE TO LAND WITHOUT INCIDENT. THE ENGINE SUFFERD TWO CRACKS TO THE CRANSDR CA041001011Magneto · arced(CAN) PILOT REPORTED A 200 RPM DROP ON RT MAGNETO. TROUBLESHOOTING REVEALED THAT TOP IGNITION WIRE ON NR 5 CYLINDER WAS UNSERVICEABLE. WHEN HARNESS WAS REMOVED FROM MAGNETO, EVIDENCE OF HEAVY ARCING WAS NOTED IN THE NR 5 LEAD OUTLET AREA OF THE DISTRIBUTOR BLSDR CA040921005Cylinder · cracked(CAN) CYLINDER ASSEMBLY FOUND CRACKED FROM SPARK PLUG HOLE.SDR CA040728003B-Nut · separated(CAN) PILOT WAS UNABLE TO HAVE GEAR DOWN INDICATION WITH BOTH ELECTRIC AND MANUAL EXTENSION. WHEEL RETRACTED BACK INSIDE WHEEL WELL ON LANDING. INSPECTION FOUND HYDRAULIC LINE INSIDE THE AIRFRAME BELLY TO RT FLOAT HAD BROKEN OFF FROM THE B-NUT. IT APPEARED SDR CA040922003Pulley Bracket · failed(CAN) AFTER TAKE-OFF, WHEN RAISING FLAPS FROM 100 TO 00, PILOT FELT A RELEASE OF TENSION AND A/C BANKED LT, UNTIL FLAP HANDLE LOCKED IN AT 00 POSITION. PILOT CHECKED FLT CONTROLS & ALL APPEARED NORMAL, PILOT SUSPECTED SOMETHING WRONG WITH FLAPS. A/C FLOWN TO BSDR 2004FA0000840Distributor Blk · burnedON 5/20/2004 THIS MAGNETO WAS REMOVED, PILOT REPORTED ROUGH ENGINE OPERATION AT ALTITUDES OF 8,000 FT OR HIGHER. PILOT ISOLATED MISFIRING MAGNETO. MAGNETO APPEARED TO BE FUNCTIONING NORMALLY ON GROUND AT SEA LEVEL AND INFLIGHT AT LOWER ALTITUDES. MAGNETO DISDR CA040709002Cylinder Head · cracked(CAN) CRACKED COMPLETELY THROUGH FROM ONE SPARK PLUG HOLE TO THE EXHAUST VALVE SEAT TOTHE OTHER SPARK PLUG HOLE. CYLINDER WAS REPAIRED 25.6 HOURS PREVIOUS. (DUE TO EXHAUST VALVE PROBLEMS) NOTE: LOGBOOK INCORRECTLY STATED CYLINDER WAS OVERHAULED. CYLINDER WAS ASDR CA040525005Shoulder Belt · inadequateIT WAS NOTED DURING INSPECTION, THAT THE REAR SEAT SHOULDER HARNESSES WERE NOT INCOMPLIANCE WITH AIRWORTHINESS DIRECTIVE 86-26-04. THIS DIRECTIVE IS SERIAL NUMBER SPECIFIC AND SHOULD NOT APPLY TO THIS AIRCRAFT. IT APPEARS THAT THESE HARNESSES WERE RECYCLED BSDR CA040519008Battery · leaking(CAN) DURING ANNUAL PERFORMANCE TEST IT WAS NOTICED THAT DURACELL MN1300 BATTERIES DATED MAR 2010 WERE LEAKING WHAT APPEARED TO BE BATTERY ACID. WHEN THE VOLTAGE OF THE BATTERIES WAS CHECKED IT WAS FOUND THAT THE AFFECTED BATTERIES WERE BELOW TWO VOLTS. ELT BASDR CA040512003Control Cable · frayed(CAN) FRAYED AT WING ROOT PULLEY.SDR CA040512002Control Cable · frayed(CAN) FRAYED AT PULLEY WING ROOT, PULLEY NOT SEIZED.SDR CA040421004Pan · corroded(CAN) DURING RIGHT COWL FLAP HINGE REPLACEMENT, FOUND COWL FLAP PAN ASSEMBLY HAS SEVERE CORROSION UNDER HINGE HALF. THIS AREA IS ONLY VISIBLE AFTER REMOVING THE HINGE.SDR CA040825002Bracket · cracked(CAN) REPAIRED HORIZONTAL STABILIZER. AFT ATTACHMENT POINT REINFORCEMENT BRACKETS 0732101-4 AND 0732106 REPLACED WITH NEW PARTS. ADJACENT RIVETS REPLACED. TAIL REASSEMBLED.SDR CA040408008Gear · damaged(CAN) DURING A RUN-UP FOR A 50 HOUR INSPECTION THE AME NOTED THAT THE LT MAG WAS TOTALLY DEAD. UPON INSPECTION IT SHOWED THAT 2 TEETH ON THE DRIVE GEAR FOR THE DISTRIBUTOR WERE TOTALLY MISSING. THESE TEETH BEING MISSING WOULD NOT ALLOW THE DISTRIBUTOR ON THESDR 2004FA0000348Cylinder · leakingLEAKING CYLINDER CAUSED GEAR NOT TO LOCK, GEAR COLLAPSED DURING TAXI.SDR 2004FA0000074Line · cracked12/19/03 AIRCRAFT ENCOUNTERED UNEXPECTED TURBULENT AIR, POSSIBLE WINDSHEAR. THE FORCES ACTING ON THE AIRFRAME CAUSED THIS 3.88 INCH HYDRAULIC LINE TO FRACTURE. THE LINE CONNECTS TO A BULKHEAD ON ONE END AND TO A TEE ON THE OTHER. FROM THE TEE, IT CONNECTS TO ASDR CA040506001Spar · crackedREMOVED HORIZONTAL STABILIZER. REAR SPAR REINFORCEMENT PART NUMBER 0732603-1 CHANGED. AFT ATTACHEMNT POINT REINFORCEMENT BRACKET RT PART NUMBER 0732101-4 REPLACED WITH NEW. ADJACENT RIVETS REPLACED. SERVICE KIT SK185-27 INSTALLED TO FACILITATE SCREW JACK RSDR CA031001005Cylinder Head · separated(CAN) IN FLIGHT SEPARATION OF CYLINDER HEAD (POSITION NR 2), VIBRATION AND LOST OF POWER. CYLINDER PREVIOUSLY INSTALLED MAY 23/03, AIRCRAFT TIME 3792.1 HOURS AND ACCUMULATED 119.4 HOURS OF FLIGHT AT TIME OF SEPARATION. CYLINDER REPLACED WITH SA ME MODEL AND SDR CA030928002Pulley Bracket · detached(CAN) ON FINAL APPROACH TO LAND THE AIRCRAFT WAS BUFFETED BY A GUST OF WIND AT WHICH TIME THE LT FLAP PARTIALLY RETRACTED. THE AIRCRAFT MADE AN UNEVENTFULL LANDING AND DURING INVESTIGATION BY MAINTENANCE THE LT FLAP PULLEY BRACKET WAS FOUND DETACHED FROM THE ASDR CA030805002Line · plugged(CAN) AIRCRAFT IS EQUIPPED WITH AN AFTERMARKET 6 CYLINDER EXHAUST GAS TEMPERATURE ENGINE MONITOR. DURING BREAK-IN PERIOD FOR FACTORY REMANUFACTURED ENGINE, NR 4 CYLINDER EGT RAN 200 DEGREES F HIGHER THAN THE OTHER FIVE CYLINDERS. TROUBLESHOOTING EVENTUALLY FOUSDR CA030731004Pushrod Tube · stuck(CAN) ELEVATOR CONTROL JAMMED ON PREFLT FUNCTION TEST. COMPLETE SYSTEM INSPECTED FOR FAULT. FINDINGS: LOOSE NUT (FOD) NR NAS 697A6 FOUND STUCK ON TOP OF ELEVATOR PUSH ROD NR 0510111-10 AT BELLCRANK ASSEMBLY NR 0761202-50 ATTACHMENT. RESTRAINING ELEVATOR MOVEMESDR CA030521006Bracket · wrong part(CAN) FLAP CABLE IN LT WING AT FLAP PULLEY BRACKET FALL OF THE PULLEY BECAUSE OF THE WRONG SIZE OF PULLEY, PULLEY AND BOLT SHOULD BE USE ON A/C S/N 185-0238 AND ON.
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