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 = '369D' 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 = '369D' 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 95ZZZX6622Turbine · nozzle crackedWHILE CHANGING NR 1 NOZZLE, IT WAS DISCOVERED THE NR 2 NOZZLE WAS CRACKED. UNIT WAS SENT IN FOR REPAIR.SDR CA960126011Bearing · leaking(CAN)BEARING LEAKING GREASE AND FEELS ROUGH. FCU REPLACED.SDR CA960126010Governor · leaking(CAN)BEARING LEAKING BLUE GREASE AND FEELS ROUGH.SDR CA960126009Belt · worn(CAN)BELT WORN BEYOND LIMITS. 1000 HOUR NORMAL RETIREMENT LIFE.SDR CA951215201Bracket · cracked(CAN)TAIL ROTOR PEDAL BRACKET BROKE AWAY FROM AIRFRAME. PILOT PERFORMING PRE-FLIGHT CONTROL CHECK.SDR 95ZZZX6936Strut · crackedINSPECTION FOUND STRUT CRACKED AT HOLE FOR THE BRACE ATTACH POINT.SDR 95ZZZX6472Combustion Liner · crackedCOMBUSTION LINER INSPECTION FOUND CRACK ON INSIDE OF DOUBLE LIP AT 8:00 POSITION ABOUT 2.5 INCHES LONG. LINER RETURNED FOR REPAIR ON ALLISON 250. REPORT NR R159723.SDR 95ZZZX6323Case Half · crackedINSPECTED CASE HALVES AT ANNUAL, FOUND PLASTIC CRACKED BEYOND LIMITS WITH SOME MATERIAL MISSING.SDR 95ZZZX6208Unilock · defectivePILOT COMPLAINED THE CYCLIC WOULD DRIFT AFT EVEN WITH TRIM SET. REPLACED UNILOCK, CURED THE PROBLEM. UNIT SENT IN FOR OVERHAUL.SDR 95ZZZX6197Nozzle · defectivePILOT COMPLAINED OF POWER/N2 FLUCTUATING WITH COLLECTIVE INPUT. SUBSEQUENT INSPECTION REVEALED THE FUEL NOZZLE WAS AT FAULT. REMOVED AND REPLACED NOZZLE AND PROBLEM WAS CURED. NOZZLE SENT IN FOR REWORK.SDR 95ZZZX6240Bleed Valve · sticksPILOT COMPLAINED THE POWER CHECK WAS INCONSISTENT. SUBSEQUENT INSPECTION REVEALED THE BLEED VALVE WAS STICKY. UNIT SENT IN FOR REPAIR ON ALLISON 250 REPORT NR A159719.SDR 95ZZZX6196Cooler · leakingOIL COOLER WAS FOUND LEAKING IN CORE AREA. REMOVED AND REPLACED OIL COOLER. PART SENT IN FOR OVERHAUL.SDR CA951108009Blade · debonding(CAN)M/R BLADE LEADING EDGE ABRASION STRIP DEBONDED.SDR CA951108008Tail Rotor Assy · delaminated(CAN)SEVERE VIBRATION ON FINAL APPROACH. INSPECTION REVEALED THAT ELASTOMERIC CONICAL BEARINGS WERE DELAMINATED WHICH CAUSED VIBRATION.SDR 95ZZZX5920Blade · bearing looseDURING 25-HOUR INSPECTION, DISCOVERED THE M/R BLADE DAMPER ATTACH BEARING (369A7951-15) WAS QUITE LOOSE. BLADE WAS REMOVED, REPAIRED, AND REINSTALLED.SDR 95ZZZX6088Blade · delaminatedON PRE-FLIGHT, THE ABRASION STRIP WAS FOUND DELAMINATING. FOUND A BUBBLE, .75 INCH WIDE RUNNING AT AN ANGLE FROM THE LEADING EDGE AT STA 135.0 TO THE TRAILING EDGE OF THE ABRASION STRIP AT STA 145.0. PART REMOVED AND SENT IN FOR REPAIR (THIS IS ON THE BOTTOMSDR 95ZZZX5717Transmission · making metalPILOT REPORTED A CHIP LIGHT AND UPON INSPECTION OF THE CHIP DETECTOR, A LARGE SHINING FLAKE AND NUMEROUS SMALLER FLAKES WERE FOUND. UNIT WAS SENT IN FOR OVERHAUL. (UNIT HAS 429.6 HOURS REMAINING TO OVERHAUL).SDR 95ZZZX5541Fuel Control · faultyWHILE IN CRUISE FLIGHT, THE PILOT NOTICED A DECREASE IN MAIN ROTOR RPM AND THE NOSE OF THE HELICOPTER NOTICEABLY YAWED. THE PILOT DECREASED COLLECTIVE PITCH, BUT THE ENGINE POWER AND ROTOR RPM CONTINUED TO DECREASE. THE ENGINE DID NOT FAIL COMPLETELY. DURINSDR 95ZZZX5540Governor · failedWHILE IN CRUISE FLIGHT, THE PILOT NOTICED A DECREASE IN MAIN ROTOR RPM AND THE NOSE OF THE HELICOPTER NOTICEABLY YAWED. THE PILOT DECREASED COLLECTIVE PITCH, BUT THE ENGINE POWER AND ROTOR RPM CONTINUED TO DECREASE. THE ENGINE DID NOT FAIL COMPLETELY. DURINSDR 95ZZZX5045Mount · looseLOWER ENGINE MOUNT FOUND LOOSE ON LEFT SIDE AND BOLT HOLE ELONGATED. PART REPLACED. MANUFACTURER'S TORQUE IS 40 INCH/POUNDS AT THIS POINT. THE BOLT IS STAINLESS CLOSE TOLERANCE. THE STRUCTURE IS STAINLESS AND THE MOUNT IS STEEL. THIS SEEMS LIKE A LIGHT TOSDR 95ZZZX4273Blade · paint peelBLADE HAD RETURNED FROM REWORK RECENTLY AND SINCE INSTALLATION 90.9 HOURS AGO, 3 SECTIONS ON THE BOTTOM OF THE BLADE HAVE BEEN STRIPPED OF PAINT IN SHEETS ABOUT 75 SQUARE INCHES OF AREA EXPOSED AFFECTING THE LATERAL BALANCE OF THE ROTOR SYSTEM.SDR 95ZZZX4278Control Bracket · cap brokenDURING 100-HOUR INSPECTION, THE BEARING CAP WAS FOUND CRACKED AT THE FORWARD BOLT EAR.SDR 95ZZZX4279Governor · erraticGOVERNOR IS ERRATIC WITH ANY POWER CHANGE. UNIT REMOVED AND SENT IN FOR REPAIR ON ALLISON 250 REPORT NR A151615.SDR 95ZZZX4277Cover Assy · insert looseDURING 100 HOUR INSPECTION, THE LOWER CHIP PLUG WAS LOOSENED FOR REMOVAL WHEN IT WAS DISCOVERED THE INSERT BOSS WAS LOOSE IN THE COVER ASSEMBLY. PART REPLACED AND SENT FOR REPAIR.SDR 95ZZZX4037Turbine · locked-upN2 LOCKED UP. UNIT SENT IN FOR SAME PROBLEM 356.7 HOURS AGO. REMOVED SN CAT 33968 AND SENT TO BE REPAIRED ON ALLISON REPORT NR A160209.SDR 95ZZZX4038Pin · brokenON POST-FLIGHT, FOUND M/R BLADE PIN BROKEN AT THE END WHERE THE THREADS STOP. THIS IS THE SAME SERIAL NUMBERED PREFIX OF 2 OTHER BROKEN BLADE PINS IN THE LAST 12 MONTHS.SDR 95ZZZX3922Vent Tube · detachedENGINE DIFFUSER VENT ORIFICE TUBE WOULD NOT STAY IN PLACE. INSPECTION FOUND END OF THE TUBE THAT SLIPS INTO THE VENT BOSS WAS DEFORMED. INSTALLED NEW TUBE.SDR 95ZZZX3921Governor · misriggedDURING RIGGING CHECK, THE GOVERNOR CONTACTED THE UPPER LIMIT STOP BEFORE THE COLLECTIVE REACHED ITS STOP.SDR 95ZZZX4072Bearing Assy · bindingSWASHPLATE UNIBALL BINDING. PILOT FELT STIFFENING OF CONTROL ON LANDING. AFTER ALL CONTROLS WERE CHECKED, SWASHPLATE WAS REMOVED. UNIBALL COULD NOT BE MOVED BY HAND. SWASHPLATE BEARING ASSY WAS REPLACED. AIRCRAFT TEST FLOWN AND RELEASED.SDR 95ZZZX3739Gauge · inoperativeTOT GAUGE - ON NEXT START OF THE AIRCRAFT THERE WAS NO INDICATION OF TOT. GAUGED CHECKED AND WAS FOUND INOPERATIVE. REPLACED GAUGE.SDR 95ZZZX3747Nozzle · defectiveAIRCRAFT WOULD DROOP RPM WHEN THE COLLECTIVE WAS LIFTED. REPLACEMENT OF THE FUEL NOZZLE CORRECTED THE PROBLEM. FCU WAS CHANGED AS PRECAUTION.SDR 95ZZZX3740Fuel Control · malfunctionedPART WAS RETURNED FROM REPAIR AND INSTALLED ON THE AIRCRAFT ONLY TO HAVE THE SAME SYMPTOMS 1.5 HOURS LATER. COMPONENT HAS A FUEL SCHEDULING PROBLEM AND HAS BEEN SENT IN AGAIN ON ALLISON 250 REPORT NR A160211.SDR 95ZZZX3870Gauge · defectiveTORQUE GAUGE FLUCTUATED DURING OPERATION 4-5 PSI. BLEEDING THE SYSTEM FAILED TO CORRECT THE PROBLEM. REPLACING THE UNIT DID CORRECT IT.SDR 95ZZZX3748Blade Pin · fracturedAT 100-HOUR INSPECTION, THE PIN WAS DISCOVERED BROKEN WHERE THE CLIP LOCKS ON THE SHAFT. SEE MDHC SOR NR 300155.SDR 95ZZZX3868Link · defectiveREMOVED LINK DUE TO STICKY OPERATION. DISCOVERED THE PIVOT BUSHING HAD NOT BEEN PROPERLY SEATED. IT IS IN SOLID, BUT A GAP EXISTS BETWEEN THE LINK AND BUSHING.SDR 95ZZZX3297Housing · wornPILOT REPORTED THE IDLE WAS TOO LOW AT LIGHT OFF AND TOO HIGH AFTER ROLL-DOWN FROM FLIGHT IDLE. AFTER A LENGTHY PROCESS OF POKING, RIGGING, AND PRODDING, DISCOVERED THE SWITCH HOUSING AT THE END OF THE COLLECTIVE WAS WORN AT ITS INTERNAL STOPS. REPLACED UNITSDR 95ZZZX3334Fuel Control · malfunctionAIRCRAFT HUNG-START AT 30 PERCENT - ALL SUBSEQUENT ADJUSTMENT HAD LITTLE OR NEGATIVE EFFECT ON THE FUEL SCHEDULING. REMOVED AND REPLACED UNIT AND AIRCRAFT STARTS NOW. UNIT SENT IN FOR OVERHAUL.SDR 95ZZZX3052Starter · defectiveAMMETER FLUCTUATED 150 AMPS FOR FIRST 5 MINUTES OF OPERATION - CHANGED AMMETER.SDR 95ZZZX3051Gauge · sticksTOT GAUGE STICKS AT 450 DEGREES CELSIUS DURING START CYCLE (RAPID TOT INCREASE). PART SENT IN FOR REPAIR.SDR 95ZZZX3033Exhaust Pipe · crackedEXHAUST STACK WAS FOUND CRACKED ALONG THE CUSHION FLANGE. UNIT REMOVED AND SENT IN FOR REPAIR.SDR 95ZZZX2932Gyro · defectivePILOT COULD NOT ADJUST THE GYRO WITH THE CAGING KNOB. REMOVED AND REPLACED UNIT AND SENT IN FOR REPAIR.SDR 95ZZZX2931Bracket · chafedPILOT COMPLAINED ABOUT A T/R VIBRATION. FOUND T/R WHIP DAMPER BRACKET CHAFED BADLY FROM DAMPER ACTION. REPLACED PART.SDR 95ZZZX2470Bearing · defectiveDURING REPAIR OF M/R TRANSMISSION AFTER THE RING GEAR HAD FAILED, THE TRANSMISSION OUTPUT SHAFT DUPLEX BEARING ASSEMBLY WAS FOUND WITH A 'CLICK' IN IT AS IT ROTATED. BEARING WAS REMOVED AND SENT IN FOR OVERHAUL.SDR 95ZZZX2401Transmission · pump defectiveDURING PRE-FLIGHT, PILOT FELT A ROUGH CLUNK IN THE ROTOR SYSTEM. AS THE ROTOR WAS TURNED, SUBSEQUENT INSPECTION FOUND THE GEAR OIL PUMP OF THE MAIN ROTOR TRANSMISSION REQUIRED A VERY HIGH BREAK-AWAY TORQUE TO BEGIN ROTATION AND AFTER THAT, IT WAS RATCHETY. USDR 95ZZZX2934Torque Gauge · fluctuatesTORQUE GAUGE FLUCTUATES IN-FLIGHT. REMOVED AND REPLACED GAUGE, PART SENT IN FOR REPAIR.SDR 95ZZZX2369Governor · defectivePILOT COULD NOT MAKE SMOOTH 'BEEP' ADJUSTMENTS. REMOVED AND REPLACED UNIT. FELT A NOTCH IN THE ROTATION OF THE LEVER ARM. UNIT SENT TO BE REPAIRED ON ALLISON 250 REPORT A160119.SDR 95ZZZX2372Gear Leg · looseDURING ANNUAL OF CUSTOMER AIRCRAFT, THE LANDING GEAR KEEL ATTACH FITINGS WERE FOUND LOOSE. PARTS WERE REMOVED AND NEW HARDWARE INSTALLED.SDR 95ZZZX2371Gear Leg · looseDURING ANNUAL OF CUSTOMER AIRCRAFT, THE LANDING GEAR KEEL ATTACH FITINGS WERE FOUND LOOSE. PARTS WERE REMOVED AND NEW HARDWARE INSTALLED.SDR 95ZZZX2366Ring Gear · defectiveUPON INPSECTION PRIOR TO ASSEMBLY IN A M/R TRANSMISSION, ONE OF THE BOLT HOLES WAS DISCOVERED TO HAVE VOIDS IN THE WALL OF THE HOLE DEEPER AND PERPENDICULAR TO THE THREADS. PART WAS RETURNED TO MANUFACTURER.SDR 95ZZZX2368Governor · defective'BEEP' RANGE IS ERRATIC. RPM JUMPS FROM POINT-TO-POINT DURING SMOOTH GOVERNOR TRIM MOTOR ACTUATION. UNIT SENT IN FOR REPAIR ON ALLISON 250 REPORT NR A160118.
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