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 = '150J' 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 = '150J' 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 2016FA0000094Hinge · wornDURING ANNUAL INSPECTION, 2 MISSING PULL-TYPE RIVETS WERE FOUND MISSING ON THE LT OTBD ELEVATOR HINGE ASSY PN-0432165-1 ALONG WITH A WORN BUSHING, PN-0432003-1 AT SAME LOCATION. ALSO NOTED, WERE THE 2 MISSING HOLES REQUIRED TO BE DRILLED DURING MFG TO RECEIVESDR 2015FA0000658Valve · burnedREMOVED CYLINDERS NRS 1 AND 3 DUE TO NEAR ZERO COMPRESSIONS AND AUDIBLE LEAKING INTO EXHAUST SYS. BEGAN INVESTIGATION DUE TO LOW RPM AND VIBRATION ON TAKEOFF. EXAMINATION REVEALED INTAKE VALVES, PN 655970, INSTALLED IN BOTH THE INTAKE AND EXHAUST POSITIONS OFSDR 2015FA0000474Cylinder · crackedACFT DECLARED EMERGENCY DUE TO OIL LEAK AND EXCESSIVE VIBRATION. LANDED ON AIRFIELD WITHOUT FURTHER INCIDENT. INSPECTION REVEALED NR 3 CYLINDER BASE WAS CRACKED 75 PERCENT OF THE WAY AROUND AND NEARLY SEPARATED FROM ENGINE. SUSPECT 2 POSSIBLE CAUSES: FWD UPSDR CA150223008Fitting · cracked(CAN) DURING ANNUAL INSPECTION, FOUND CORROSION ON THE FITTING HOLDING VERTICAL STAB TO HORIZONTAL STAB. WHEN CORROSION WAS REMOVED, FAINT LINES WERE NOTICED. UNDER 10X MAGNIFICATION A CRACK WAS DETECT ON FORWARD VERTICAL SECTION OF FITTING APPROX 1/2" LONG. FSDR 2009FA0000908Leg Assy · corrodedDURING ANNUAL INSP, NOTED RUST STAINS ADJACENT TO THE STEPS LOCATED ON BOTH THE RT AND LT MLG LEGS. REMOVED THE STEPS AND FUND DEEP RUST PITS AND DAMAGE ON BOTH GEAR LEGS. BOTH GEAR LEGS WERE REMOVED AND REPLACED WITH USED SERVICEABLE GEAR LEGS. STEPS WERE SDR CA050826002Coil · weak(CAN) RAN ROUGH SLIGHTLY MORE PROP THAN NORMAL. MAG DROP, WEAK SPARK, ABOUT .3333 OF NORMAL STRENGTH. OVERHAULED MAG WAS INSTALLED, 900 HOUR PREVIOUSLY.SDR CA040914008Flange · corroded(CAN) PROPELLER REMOVED FOR CORROSION INSPECTION UNDER CAR 625, APPENDIX C, PARA 5. MOUNTING FLANGE CORRODED BEYOND REPAIR.SDR 2004FA0000413Valve · inoperativePILOT REPORTED HIGH OIL TEMPERATURE 220-225 DEGREES, REMOVED VALVE AND TESTED SIDE BY SIDE WITH NEW VALVE, OLD VALVE DID NOT CLOSE AT THE SAME RATE AS NEW VALVE, INSTALLED NEW VALVE AND OIL TEMP DECREASED TOO.SDR KZ52004F00000Valve · inoperativePILOT REPORTED HIGH OIL TEMP 210 DEGREES-220 DEGREES F., REMOVED VALVE AND TESTED SIDE BY SIDE WITH NEW VALVE, OLD VALVE DID NOT CLOSE AT THE SAME REATE AS NEW VALVE AND OIL TEMP DECREASED TO.SDR CA020731014Stop · missing(CAN) UPON COMPLETING INSPECTION OF RUDDER STOPS PER AD CF-2000-20, IT WAS FOUND THAT THE RUDDER STOPS WERE BOTH MISSING. THERE WERE NO HOLES IN THE TAILCONE SKIN WHERE THE STOPS SHOULD HAVE BEEN, BUT THE ANCHOR NUTS WERE RIVETS TO THE BULKHEAD. THIS SKIN WAS SDR 223527605Battery · leakingON DOING A PRE FLIGHT INSPECTION I FOUND THAT ACID WAS LEAKING FROM THE ELT BATTERY. FURTHER INSPECTION SHOWS THAT ACID LEAKING FROM THE PACK HAD DESTROYED THE ELT ELECTRONICS MODULE, THE MOUNTING BASE WAS EATEN THROUGH AS WAS THE CARPET AND THE ACID WAS ATTACSDR CA011121002Control Cable · broken(CAN) PILOT APPLIED CARB HEAT ON DOWNWIND AND KNOB SHAFT ASSEMBLY CAME OUT IN HER HAND. PUSH / PULL WIRE HAD BROKEN ABOUT 3 INCHES PAST THE END OF THE SHAFT. EXAMINATION OF THE BREAK INDICATED A LONG STANDING CRACK ABOUT 2/3 OF THE WAY THROUGH THE WIRE. THERESDR CA010912017Stiffener · cracked(CAN) COMMON PROBLEM ON OLDER CESSNA 150 SERIES, MANUFACTURER HAS BEEN REPLACED THIS PART WITH A NEW IMPROVE PART P/N 0432169-1 ALSO INCLUDING NEW IMPROVE BULKHEAD ASSY P/N 0412177-2.SDR CA010820010Transmitter · stuck(CAN) TRANSMITTER LEVER PIVOT HAS BECOME SOMEWHAT STIFF, RESULTING IN INACCURATE FUEL LEVEL INDICATIONS. PART WAS REPLACED. THIS PART IS PART OF CESSNA SERVICE KIT SK-150-65. THE KIT WAS MADE NECESSARY BY THE UNAVAILABILITY OF THE ORIGINAL STEWART- WARNER SYSTSDR 20000720SH037Stabilizer · crackedBOTH STABILIZER SPARS FOUND CRACKED IN THE UPPER BEND RADIUS FOR THE FLANGE AT THE INBOARD PAD ABOUT 2 INCHES FROM THE PADS. THIS AREA IS CONCEALED UNDER STIFFENER 0432001-15 (ALSO CRACKED). THIS WAS DISCOVERED DURING INSPECTION FOR AD 80-11-04, ALSO SPAR RESDR CA000614016Frame · cracked(CAN) DURING 100 HOUR INSPECTION, IT WAS DISCOVERED THAT THERE WERE 2 SMALL CRACKS ON THE FRAME REAR LUG THAT HOUSES THE ADJUSTING CAM FOR THE SEAT BACK. ONE CRACK WAS FOUND ATTHE LUG WELD WHILE THE OTHER WAS FROM THE HOLE FOR THE SHAFT ASSY (0411105-1).IT WASSDR CA000301030Regulator · failed(CAN) THE REGULATOR FAILED AND CAUSED THE BATTERY TO BE OVERCHARGED WHICH DESTROYED THE BATTERY.SDR CA990729007Gear · spalled(CAN) MAGNETO GEARS WHICH ARE SUSPECTED TO BE UNAPPROVED PARTS. ONT. SAIB NR CE-98-21R1 WAS RELEASED TO CORRECTLY IDENTIFY THE GEARS IN THE FIELD.SDR 99ZZZX139Leg · crackedA STRESS CORROSION FRACTURE OCCURRED IN THE RADIUS AREA WHERE THE HIGH CARBON SPRING STEEL MAIN LANDING GEAR LEG AND THE LANDING GEAR EXTENSION CONTACT. SUBMITTER SUGGESTED IMMEDIATE INSPECTION AND REPETITIVE INSPECTIONS AFTER 50 LANDINGS OR 50 HOURS WHICHEVESDR 98ZZZX1920Valve · failedAIRCRAFT WAS ON A TRAINING FLIGHT WHEN POWER WAS LOST, WITH 1500 RPM BEING MAXIMUM AVAILABLE. A SAFE LANDING WAS MADE ON A COUNTY STONE ROAD. INVESTIGATION REVEALED THE INTAKE VALVE STEM HAD BROKEN AT THE BOTTOM OF VALVE KEEPER RECESS. KEEPER AND TOP OF STESDR CA980318020Carburetor · defective(CAN) ENGINE HAD JUST OVERHAULED AND FOUND TO BE RUNNING ROUGH IN THE LOW RPM RANGE. DIFFICULTY FOUND IN ADJUSTING IDLE MIXTURE. AFTER REVIEWING FAA AD 98-01-06 DECISION TO REPLACE CARBURETOR WAS MADE. CARBURETOR REMOVED HAD THE ONE PIECE VENTURI.SDR 98ZZZX557Fitting · crackedINSPECTION FOUND VERTICAL STABILIZER ATTACH FITTING CRACKED.SDR 97ZZZX3492Control · brokeMIXTURE CONTROL BROKE AT CARBURETOR APPROXIMATELY .1250 INCH FROM END OF CABLE.SDR 97ZZZX2799Line · chafedOIL PRESSURE INDICATOR LINE (COPPER) BETWEEN FIREWALL AND INDICATOR WORE THROUGH AND LEAKED DUE TO IMPROPER SECURING OF LINE BY PLASTIC TY-RAP BANDS. PLASIC TY-RAP IS HARDER THAN COPPER .1250 INCH LINE. LINES SHOULD BE SECURED BY PROPER SIZE ADEL CLAMPS.SDR 97ZZZX1102Cylinder · failedENGINE RAN ROUGH ON START. REMOVED COWLING. RESTARTED ENGINE. SHAKING VIOLENTLY. REMOVED ROCKER COVER. ENTIRE ROCKER ARMS, PINS, AND BOSSES FELL IN COVER. SUSPECT VALVE STUCK.SDR 97ZZZX831Venturi · wornOWNER REPORTED ENGINE BEING ROUGH AT LOW RPM AND POOR ACCELERATION AND HESITATION WHILE ADDING POWER, AND NOT RUNNING BELOW 1,000 RPM. INSPECTION REVEALED A TWO-PIECE VENTURI STILL INSTALLED AND WORN TO A POINT OF NEAR SEPARATION. AD 93-18-03 FOR INSTALLING SDR 96ZZZX73Switch · defectiveSWITCH INSTALLED NEW AT 4,000.4 HOURS ON MARCH 12, 1991. REMOVED AT 5,773.28 HOURS, NOVEMBER 30, 1995. TOTAL OPERATING TIME 1,772.9. INTERNAL WEAR BETWEEN TUMBLER AND HOUSING CAUSED CONTACTS TO WANDER AS ACTUATED, AND NO CONTACT. TO GROUND, ERRATIC, AND SWSDR 95ZZZX3275Magneto · coil crackedUPON INSPECTION OF INTERNAL COMPONENTS OF MAGNETO AT ANNUAL INSPECTION, HIGH TENSION COIL WAS FOUND CRACKED.SDR 95ZZZX2681Crankcase · stud pulledWHILE RETORQUING CYLINDER HOLD-DOWN NUT, THE STUD PULLED OUT OF ITS THREADS IN THE OPPOSITE CASE HALF; THUS, THE CASE HAS TO BE SPLIT TO REPAIR THE THREADS. THIS IS A COMMON PROBLEM AND COULD BE PREVENTED BY THE INSTALLATION OF HELICOILS EACH TIME THE ENGINE SDR 95ZZZX1903Nozzle · not compatibleONE-PIECE VENTURI, NOT COMPATIBLE WITH ORIGINAL DISCHARGE NOZZLE. SHOULD BE MANDATORY TO CHANGE DISCHARGE NOZZLE AT THE TIME OF ONE-PIECE VENTURI IS INSTALLED. OLD NOZZLE NOT COMPATIBLE WITH NEW VENTURI.SDR 95ZZZX651Control Cable · defectiveAT ANNUAL INSPECTION, THROTTLE WAS FOUND TO HAVE .50 INCH OF TRAVEL AFTER CARBURETOR WAS AGAINST THE IDLE SPEED SCREW. MOVEMENT WAS STILL FREE AND SMOOTH. SUSPECT THE INNER CORE OF THE FLEXIBLE CABLE WAS BROKEN AND THE OUTER SPINAL WIRES WERE STILL CONNECTED.
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