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 = '222U' 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 = '222U' 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 99ZZZX2879Shroud · flakingCOATING FLAKING OFF OF IMPELLER SHROUD PREMATURELY. REF: MCN 69. REMOVED AND REPLACED.SDR 99ZZZX2164Ring · damagedREPLACED WITH NEW OUTER RING FROM BELL HELICOPTER.SDR 99ZZZX2842Switch · failedNEW PART DEFECTIVE. ILLUMINATED NR 1 HYDRAULIC LIGHT. REPLACEMENT OF SWITCH EXTINGUISHER.SDR 99ZZZX1798Bearing · wornBEARING WORN BEYOND SERVICEABLE LIMITS. INSTALLED AT ASE GREER FACILITY. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR CA981209002Seal · cracked(CAN) SEAL ASSEMBLY CONSISTING OF FRAME, RING AND ANGLE FOUND WITH CRACK IN SPOT WELDS ATTACHING ANGLE TO TAILPIPE BODY AND CRACKS IN SPOT WELDS ATTACHING RING TO FRAME.SDR 99ZZZX689Exciter · inoperativeEXCITER INOPERATIVE. ENGINE FAILED TO START. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR 99ZZZX1259Pump · leakingFUEL PUMP LEAKING FUEL FROM OVERBOARD DRAIN. REMOVED AND REPLACED.SDR HEEA0015386Compass · contaminatedCOMPASS, AIR BUBBLE IN 10 ERROR.SDR HEEA0014038Battery · failedBATTERY WAS FOUND AT 6 VOLTS ON 3-11-98. BATTERY WAS CHARGED TO 22.5 VOLTS. WHILE DISCONNECTED FROM AIRCRAFT, VOLTAGE DROPPED FROM 22.5 VOLTS TO 18 VOLTS IN ONE HOUR. VOLTAGE WAS MEASURED AT 15.4 VOLTS AFTER 5 HOURS. AIRCRAFT BATTERY WAS INSTALLED NEW AT 4SDR 98ZZZX1755Annunciator Pnl · defectiveANNUNCIATOR PANEL NR 2 ENGINE FUEL VALVE CAUTION AND NR 2 FUEL LOW LIGHTS INOPERATIVE. REMOVED AND REPLACED.SDR 98ZZZX324Bulkhead · crackedFOUND 2 EACH CRACKS IN AFT MAIN ROOF BEAM AT LT NODAL BEAM SUPPORT. BS 270, WL 79.0, LBL 9.90.SDR 98ZZZX941Coupling · corrodedOUTER COUPLING HAS CORROSION ON INTERNAL SPLINES. LESS THAN 1 YEAR IN SERVICE. REMOVED AND REPLACED.SDR 98ZZZX940Coupling · corrodedOUTER COUPLING HAS CORROSION ON INTERNAL SPLINES, LESS THAN 1 YEAR ON SERVICE. REMOVED AND REPLACED.SDR 97ZZZX5218Manifold · crackedFUEL LEAK NOTED ON POST-FLIGHT INSPECTION. FUEL MANIFOLD WAS FOUND TO HAVE A CRACK OR HOLE AT 5 O'CLOCK POSITION. UNABLE TO DETECT WITH NAKED EYE. FUEL POOLED IN ENGINE COMPARTMENT AREA MAKING THIS A VERY DANGEROUS SITUATION. FUEL LEAKING ONTO THE TURBINE SDR 98ZZZX284Mount · defectiveENGINE MOUNT BEARING NOT PROPERLY STAKED. REMOVED AND REPLACED.SDR 97ZZZX4835Tube · crackedREPLACED CRACKED PY LINE AT FUEL CONTROL UNIT.SDR 98ZZZX602Coupling · corrodedCOUPLING HAS CORROSION, PITTING ON TEETH. DAMAGED BEYOND LIMITS. REJECTED. REMOVED AND REPLACED.SDR 98ZZZX601Coupling · corrodedM/R DRIVE INNER COUPLING PITTING CORROSION ON TEETH. REJECTED. REMOVED AND REPLACED.SDR 97ZZZX4093Fuel Manifold · leakingTUBE OR WELD CRACKED WHERE TUBE ENTERS FUEL NOZZLE FITTING. THIS IS THE SIXTH OCCURRENCE SINCE MAY, 1997. THREE WERE P/N 4-401-376-01 MANIFOLDS AND 3 WERE P/N 4-301-236-04 MANIFOLDS. THIS IS BEING ADDRESSED BY ALLIED SIGNAL.SDR HEEA0010790Actuator Assy · wornACTUATOR ASSY WORN BEARINGS.SDR CA970722004Fuel Manifold · leaking(CAN) THE SMELL OF FUEL WAS EVIDENT DURING DESCENT. POST FLIGHT INVESTIGATION FOUND THE FUEL MANIFOLD LEAKING AT A BRAZED WELD. THE FUEL MANIFOLD WAS REPLACED.SDR HAIW6HR0088Torque Sensor · failedTORQUE SENSOR HAS RESISTANCE-HIGH. INDICATOR NEEDLE INTERMITTENTLY DROPS OFF TO ZERO. UNIT WAS INSTALLED FOR APPROX. 1 MONTH AND HAS 36.5 HRS. SINCE BEING REPAIREDSDR 97ZZZX3600Flexure · debondedINSPECTION PRIOR TO INSTALLATION REVEALED SHEAR PAD TO BE DEBONDED. PART RECEIVED BAD FROM STOCK.SDR HEEA0010053Altimeter · sticksALTIMETER HAS EXCESSIVE FRICTION ERROR AND NEEDLE STICKS.SDR HAIW6HR0087Panel Assy · crackedPANEL ASSY IS CRACKED. APPROX. 10 INCH CRACK STARTING @ R/H AFT CORNER GOING FOWARD AND TOWARDS THE LEFT. THIS CRACK HAPPENED DUE TO STA. 233 FRAME ASSY. P/N: 222-031-503-101 CRACKING. PERFORMED BHT FIELD REPAIR PROCEDURE 96R1-037, D.O.Y. S.O.C. SERIAL # ASDR HAIW6HR0086Roof · crackedPART IS CRACKED. ROOF WAS CRACKED DUE TO FRAME ASSY P/N: 222-031-503-101 (STA 233) CRACKING. INSTALLED STRAP DOUBLER P/N: 222-031-517-179 I/A/W BHT TB 222U-91-56, DATED 1-15-91.SDR HAIW6HR0085Frame Assy · crackedFRAME ASSY IS CRACKED. CRACKED @ R/H CORNER THRU FASTNER HOLES. PERFORMED REPAIR I/A/W BHT FIELD REPAIR PROCEDURE 96R1-036 REV. A D.O.T. S.O.C. SERIAL # A4753, DATED 3-19-97.SDR 97ZZZX3599Indicator · inoperativeATTITUDE INDICATOR INOPERATIVE. ONLY 7.6 HRS SINCE INSTALLED AFTER OVERHAUL.SDR 97ZZZX2722Tailboom · crackedA CRACK OF OVER 2 INCHES WAS FOUND ON RT SIDE OF TAILBOOM DURING PILOT POST-FLIGHT CHECK. OTHER OPERATORS HAVE EXPERIENCED CRACKS IN THE SAME AREA. BELL HAS ISSUED A TECHNICAL BULLETIN (TB 222U-94-65) TO ADDRESS THE PROBLEM. SUBMITTER RECOMMENDATION, HAVE BSDR HAIW6HR0084Torque Sensor · fluctuatesROTOR TORQUE NEEDLE FLUCTUATES ABOVE 85% ROTOR TORQUE. PART IN SERVICE 4 MONTHS / 178.9 HOURS. REPLACED SENSOR.SDR 97ZZZX2721Skin · tornA TEAR IN THE HORIZONTAL STABILIZER SKIN WAS FOUND DURING INSPECTION. THE DAMAGE WAS LOCATED ON THE RT INBOARD LEADING EDGE. THE DAMAGE MAY HAVE BEEN CAUSED DURING IMPROPER OR ROUGH INSTALLATION. THE DAMAGE WAS REPAIRED UNDER MANUFACTURER'S INSTRUCTIONS AND SDR 98ZZZX578Manifold · leaksSUBMITTER STATES EXCESSIVE FUEL MANIFOLD LEAKS OVER THE LAST 18 MONTHS. ALLIED SIGNAL IS IN THE PROCESS OF RELEASING AN ASB LIMITING THE LIFE OF THE FUEL MANIFOLD TUBES. OTHER OPERATORS SUBMITTER CONTACTED ARE HAVING THE SAME PROBLEMS. OMNIFLIGHT HAS GONE TSDR 97ZZZX3624Indicator · failedATTITUDE INDICATOR, FLAG WILL NOT STAY PULLED.SDR 97ZZZX3666Light · failedWILL NOT EXTEND OR ROTATE. WAS REPAIRED FOR SAME DISCREPANCY ON LAST REPAIR AND WOULD NOT WORK WHEN ISSUED FROM STOCK.SDR HAIHEEA9594Blade · damagedBLADE TRIMMED ON THE INBOARD LEADING EDGE ABRASION STRIP WITH NO CONTOUR RADIUS.SDR HAIHEEA9593Blade · crackedM/R BLADE HAS A CRACK IN THE TIP SHOE.SDR AU970881Pump · failed(AUS) LH ENGINE DRIVEN OIL PUMP FAULTY. OIL PRESSURE FLUCTUATING.SDR 97ZZZX1995Line · crackedTHE NR 2 ENGINE AIR LINE TO FUEL CONTROL UNIT CRACKED CAUSING ENGINE TO DECELERATE TO FLIGHT IDLE. UPON COMMUNICATION WITH MANUFACTURER, FOUND THAT THIS HAS HAPPENED BEFORE. PERFORMED A ONE TIME FLEET INSPECTION AND FOUND 3 MORE LINES THAT HAD FRETTING UNDERSDR 97ZZZX3625Indicator · failedPILOT SMELLED BURNING ODOR. OFF FLAG PULLED. ATTITUDE INDICATOR FAILED AFTER ONLY 40.9 HOURS INSTALLED.SDR 97ZZZM578Shaft · destroyedTHE PILOT NOTICED NR 2 ENGINE OIL TEMPERATURE WAS CLIMBING TOWARDS RED LINE. THE PILOT EXECUTED PRECAUTIONARY LANDING. MAINTENANCE PERSONNEL FOUND THE OIL COOLER BLOWER SHAFT HAD SHEARED AND THE FLOPPING AROUND HAD DAMAGED THE DRIVE GEAR IN THE ENGINE AND THSDR AU970415Gear · failed(AUS) NO1 ENGINE ACCESSORY GEARBOX MODULE TORQUEMETER GEAR ASSEMBLY DAMAGED - GEAR HAD SHEARED THE HEAD OFF ONE OF THE EIGHT BOLTS USED TO HOLD THE ASSEMBLY TOGETHER - TORQUEMETER PISTON HAD WORN A GROOVE IN THE HOUSING - METAL CONTAMINATION OF ENGINE OIL SYSTSDR HAIW6HR0076Light · bindingPART IS BINDING. ASSY. WILL NOT MOVE IN ANY DIRECTION. PART HAS BEEN IN SERVICE 3 MONTHS. REQUEST ASSY. TO BE REPAIRED UNDER WARRANTY. REPLACED LIGHT ASSY WITH SERVICEABLE UNIT.SDR 97ZZZM652Fitting · brokenFOUR MINUTES AFTER TAKEOFF, NR 2 ENGINE WENT TO FLT IDLE. A SINGLE ENGINE LANDING WAS INITIATED. MAINTENANCE PERSONNEL FOUND A T-FITTING ON THE PC FILTER HOUSING BROKEN OFF. THE FILTER ASSY WAS REPLACED, THE ENGINE WAS OPERATIONAL CHECKED AND RETURNED TO SESDR 97ZZZX3573Indicator · inoperativeATTITUDE INDICATOR INOPERATIVE.SDR HAIW6HR0072Fuel Manifold · defectiveENGINE SHOOTS OUT 2 FOOT FLAME PAST EXHAUST EJECTOR DURING START WITHOUT ANY MGT INDICATION UNTIL START PROGRESSES, THEN REMAINDER OF START IS NORMAL. SUSPECT EXCESS FUEL GETTING INTO ENGINE AT BEGINNING OF START ENGAGEMENT. SHIPPED CORE RETURN MANIFOLD TO RMHSDR 97ZZZX925Spring Carrier · spalledENGINE HAD HISTORY OF CHIP LIGHT ILLUMINATION. ALWAYS BURNED OFF. VISUAL INSPECTION FOUND CHIPS EXCEEDING LIMITS IAW SB LT101-77-30-0104. REMOVED ENGINE FOR REPAIR.SDR HAIW6HR0068Bearing · worn excessivelyPART IS WORN EXCESSIVELY. ELASTORMERIC EXTRUSION, DELAMINATION & SEPERATION. UNIT FIRST PUT INTO SERVICE 08-03 1983.SDR HAIW6HR0067Bearing · worn excessivelyPART IS WORN EXCESSIVELY. ELASTOMERIC MATERIAL IS SEPERATING. BEARING WAS PUT IN SERVICE 14 JUL. 1989. PART HELD FOR FUTURE EVALUATION.SDR HAIW6HR0066Bearing · worn excessivelyPART IS WORN EXCESSIVELY. ELASTOMERIC MATERIAL IS SEPERATING. BEARING WAS PUT IN SERVICE 16 JAN. 1988. PART HELD FOR FUTURE EVALUATION.SDR HAIW6HR0063Light · seizedPART IS SEIZED. ASSY. WILL NOT EXTEND OR RETRACT. ASSY. HAS BEEN IN SERVICE 2 WEEKS SINCE REPAIR.
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