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 jasc_code = '3252' 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 jasc_code = '3252' 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 99ZZZX2516Rod · corrodedSHIMMY DAMPENER ROD WAS FOUND TO HAVE CORROSION INSIDE AND OUT CAUSING FLUID TO LEAK BY THE O-RINGS. CORROSION SEEMS TO BE FROM NORMAL OPERATION. ROD WAS REPLACED.SDR 99ZZZX2359Dampener · damagedNOSE GEAR SHIMMY DAMPENER ALSO ALIGNS NOSE SEAL ON RETRACTION: UNIT SHAFT CIRCLIP FAILED ALLOWING SHAFT TO EXIT BODY AND JAMMED NOSE. GEAR AT ANGLE TO CENTERLINE OF AIRCRAFT. GROOVE FOR CIRCLIP DOES NOT APPEAR DEEP ENOUGH.SDR AU990430024Roll Pin · broken(AU) PILOT LANDED AND REPORTED NOSE SHIMMY. SUBSEQUENT TEARDOWN REVEALED A BROKEN ROLL PIN SHARD WHICH HELD THE INTERNAL METERING PISTON. RIGGING, STOP BLOCK INSPECTIONS, AND PRIOR LOG BOOK ENTRIES REVEALED NO FAULTS.SDR 99ZZZX1858Valve · crackedON PRELIMINARY FUNCTIONAL TEST, THE BODY WAS NOTED TO HAVE A PIN HOLE CRACK WITH 3,000 PSI APPLIED TO THE P1 PORT. THE CRACK IS ADJACENT TO THE C1 PORT.SDR 98ZZZX4508Shimmy Dampener · failedAIRCRAFT EXPERIENCED NOSE WHEEL SHIMMY. A NEW SHIMMY DAMPENER INSTALLED. THE USUAL PRECAUTIONS AND TROUBLESHOOTING PROCEDURES WERE UTILIZED TO DETERMINE SHIMMY DAMPENER. WITHIN A FEW HOURS, ACFT REPORTED WITH SAME PROBLEM. INSTALLED NEW SHIMMY DAMPENER MFSDR 99ZZZX721Shimmy Dampener · wornFOUND SHIMMY DAMPENER ROD END BROKE OFF AND MOUNT BOLT BADLY WORN (ALMOST IN TWO) AND BOLT BENT ALMOST 90 DEGREES. THIS WAS DISCOVERED DURING ROUTINE MAINTENANCE DUE TO STRANGE ANGLE OF SHIMMY DAMPENER. WHEN PART WAS CHANGED, DISCOVERED IT HAD BEEN BROKEN FOSDR 98ZZZX1999Dampener · crackedSHIMMY DAMPENER WELDED AFTER DAMAGE. AFTER 6 MONTHS USE, CRACK DEVELOPED WHILE IN SERVICE. RESULTING LEAK OF FLUID CAUSED SEVERE SHIMMY ON ATTEMPTED TAKEOFFS. UNIT REPLACED WITH NEW ITEM FROM CESSNA.SDR 98ZZZX1653Dampener · wornSHIMMY DAMPENER HAD NO FLUID AND SHAFT WOULD NOT COME OUT FOR OVERHAUL. INSTALLED NEW PART.SDR 98ZZZX1102Steering Unit · malfunctionedDURING TAXI AFTER LANDING, AIRCRAFT STARTED TO TURN LEFT WITHOUT INPUT TO TILLER OR RUDDER PEDALS. AIRCRAFT EXAMINED AND NO APPARENT CAUSE WAS IDENTIFIED. CONTACTED CESSNA AND REQUESTED A REPLACEMENT STEERING UNIT. TECHNICIANS FOR ICT AND LGB CAME TO PHX ANSDR 98ZZZX1088Dampener · seizedOPERATOR REPORTED NOSE WHEEL STEERING PULLED TO THE LEFT WHEN INDICATING STRAIGHT (RUDDER PEDALS IN NEUTRAL). FOUND NOSE TIRE SEVERELY SCUFFED ON CENTERLINE OF TREAD. ATTEMPTS TO MANUALLY TURN NOSE WHEEL FOUND SHIMMY DAMPENER FROZEN IN PLACE. REPLACED NOSE SDR AU980101Damper · corroded(AUS) NOSE LANDING GEAR SHIMMY DAMPER PISTON CORRODED AND CHROME PLATING RUSTED OFF. SHIMMY DAMPER ALSO LOW ON OIL.SDR 97ZZZX5129Barrel · failedAIRCRAFT WAS BROUGHT TO MAINTENANCE AFTER A TRAINING FLIGHT WITH REPORT OF A SEVERE NOSE WHEEL VIBRATION. AN INSPECTION REVEALED THAT THE END OF THE SHIMMY DAMPENER BARREL CLOSEST TO THE SERVICE HOLE WAS BROKEN OFF. THE OUTER RETAINING LINE AND BEARING HEAD SDR 97ZZZX4771Manifold · chafedINSPECTION FOUND MANIFOLD ASSY OF DAMPER ASSY CHAFED DUE TO HOSE RUBBING ON OUTSIDE DIAMETER OF COMPENSATOR LOCATION. REPEAT DEFECT.SDR 97ZZZX4012Shimmy Damper · brokenNOSE WHEEL BEGAN TO SHIMMY ON LANDING ROLL-OUT AT APPROXIMATELY 50 KNOTS. NO ABNORMAL CREW ACTION REQUIRED. SHIMMY DAMPER WAS REMOVED AND FOUND TO HAVE FAILED INTERNALLY. ROLL PIN SECURING SHAFT TO PISTON SHEARED. THIS PREVENTED ANY DAMPENING ACTION. NOSESDR 97ZZZX3379Cylinder · failedSHIMMY DAMPENER HOUSING FAILED DURING FLIGHT. UNIT FAILED AT THE OUTER PORTION OF OUTER RETAINING RING FLANGE. FAILURE WAS ON DOWN-WIND LEG AFTER A NORMAL TOUCH AND GO. SUBMITTER STATES OWNER MENTIONED SEVERAL YEARS AGO, TWO SEPARATE SEVERE SHIMMY INSTANCESSDR SWAA970495Damper · looseON LANDING AT APPROX 80 KNOTS, AIRCRAFT MADE AN ABRUPT RIGHT TURN, DIFFICULT TO HOLD AIRCRAFT CENTERED, WITHOUT USING FULL LEFT RUDDER. CREW USED TILLER TO CORRECT. ENGINES, REVERSERS AND BRAKES APPEARED NORMAL. RETORQUED LT GEAR SHIMMY DAMPER PER BOEING M/SDR 96ZZZX5892Dampener · failedAIRCRAFT LANDED, RAN OFF RUNWAY PUSHING NOSE GEAR UNDER FUSELAGE. OWNER SAID PLANE DEVELOPED SHIMMY AND HE COULDN'T KEEP ON RUNWAY. CHECKED SHIMMY DAMPENER AND FOUND ONE-HALF AIR IN IT. SUBMITTER STATED SHOULD MAYBE CHECK SHIMMY DAMPENER MORE OFTEN FOR FLUISDR CA961007018Arm · broken(CAN) AFTER LANDING SHIMMY DEVELOPED EITHER CAUSING ARM TO BREAK OR ARM WAS ALREADY BROKEN. STEERING FOUND OK AND FLUID LEVEL IN SHIMMY DAMPENER AND OLEO WAS CORRECT.SDR CALA9601275Shimmy Damper · failedTHE AIRCRAFT BEGAN TO BOUNCE UP AND DOWN SOON AFTER LANDING. THE BOUNCING STOPPED AFTER THE AIRCRAFT SLOWED TO 100 KNOTS, BUT THEN PULLED TO THE LEFT. THE AIRCRAFT WAS STOPPED AND TAXIED OFF THE RUNWAY. MAINTENANCE FOUND THE RT MLG SHIMMY DAMPER HAD FAILED SDR 96ZZZX4335Shimmy Damper · leakagePRIOR TO TAKEOFF, PILOT EXPERIENCED NOSE WHEEL SHIMMY. TAKEOFF WAS ABORTED, AIRCRAFT RETURNED TO RAMP. MAINTENANCE FOUND FLUID LEAKAGE COMING FROM NOSE WHEEL SHIMMY DAMPER. REPLACED WITH SERVICEABLE UNIT. TAXI TEST NOTED, NO DISCREPANCIES. AIRCRAFT RETURNESDR 96ZZZX3320Attach Clamp · failedTHE SHIMMY DAMPENER CLAMP ASSY, PN 2243015-1, ALIGNMENT PIN FAILED AND CAUSED THE SHIMMY DAMPENER TO ROTATE ON THE STRUT HOUSING AND IMPROPERLY ALIGN THE DAMPENER CAUSING THE DAMPENER TO JAM THE LANDING GEAR IN THE UP POSITION. NOTE: THE DAMPENER CLAMP LOOKSSDR CA960611008O-Ring · cut(CAN) PILOT REPORTED NOSE WHEEL SHIMMY. MINOR LEAK ON SHIMMY DAMPER. PISTON HEAD "O" RING CUT.SDR 96ZZZX2855Eye Bolt · failedSHIMMY DAMPENER EYE BOLT FAILED ON ROLL-OUT ON NORMAL LANDING. NO ACCIDENT RESULTED.SDR 96FDEA00730Cylinder · failedLOST SYS 3 HYD AFTER LANDING, MADE TURN ON TO TAXIWAY LOST ALL FLUID CONFIRMED EXTERNAL LEAK FROM A/C ON GROUND. REMOVED AND REPLACED NOSEWHEEL STEERING CYLINDER PER MM 32-52-01. RESERVICED NR 3 HYDRO SYS TO FULL, ALL SYSTEMS CHECK GOOD.SDR CA951222005Shimmy Bracket · pivoted 90 deg(CAN)THE PILOT NOTICED THAT THE PEDALS FELT LIKE SOMETHING HOOKED THEM DURING RETRACTION OF THE GEAR. ON EXAMINATION AFTER LANDING, IT WAS DISCOVERED THAT THE STEERING CABLE HAD BEEN BENT AT THE TURNBUCKLE .THE SHIMMY DAMPER HAD ROTATED 90 DEGREES FROM IT'S POSDR 95ZZZX6171Dampener · misrepairedPILOT COMPLAINED OF EXCESSIVE NOSEWHEEL SHIMMY. EXAMINATION FOUND SHIMMY DAMPENER WAS EMPTY, HAD PREVIOUSLY BEEN FILLED WITH MOTOR OIL INSTEAD OF 5606 AND FILL PORT HAD BEEN TAPPED OVERSIZE, THREADS TAPPED CROOKED (ON AN ANGLE), AND AN OVERSIZED BOLT INSTALLESDR 95ZZZX4270Clamp · loosePILOT REPORTED LANDING GEAR WOULD NOT LOCK UP, INTRANSIT LIGHT ON WHILE THE GEAR WAS RETRACTED. INVESTIGATION REVEALED THE SHIMMY DAMPENER CLAMP ON THE STRUT WAS LOOSE AND THE SHIMMY DAMPENER SHAFT CAUGHT THE SKIN ON THE TUNNEL COVER AND TORE A HOLE IN IT. TSDR 95ZZZX3953Stop-Bolt · shearedA DIRT PILE ON 45 DEGREE ANGLE ON RUNWAY CAUSED NOSE WHEEL TO DEFLECT AND START SHIMMY. SEVERE SHIMMY CAUSED SHEARING OF AN-3 STOP-BOLT RESULTING IN WHEEL TURNING SIDEWAYS AND STRUT COLLAPSING. THE NEW NOSE STRUT HAS A HEAVIER, AN-4 STOP-BOLT.SDR 95ZZZX2178Rod End · wrong partDURING RAMP CHECK, FOUND SHIMMY DAMPER SHAFT ROD END BENT. FOUND CAUSE TO BE INCORRECT SHAFT INSTALLED. SHAFT LENGTH SHOULD BE APPROXIMATELY 6.450 INCHES WITHOUT ROD END. SHAFT INSTALLED WAS APPROXIMATELY 6.950 INCHES (LONGER SHAFTS ARE FOR PA-28-161 SHIMMY
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