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 = '230' 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 = '230' 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 CA140521009Fuel Control · malfunctioned(CAN) IN CRUISE FLIGHT NR 1 ENGINE PARTIAL POWER LOSS, 40 PERCENT TORQUE SPLIT FROM ENGINE NR 2. ENGINE NR 1 ROLLED BACK MANUALLY TO IDLE, ENGINE LIGHT OUT ILLUMINATED, THROTTLE MANUALLY ROLLED BACK UP, CONTINUED TO LAND WITH TORQUE SPLIT. GROUND RUN CARRIEDSDR O842011F00000Valve · bypassingNR 1 ENGINE WAS LOW. TROUBLESHOT AND FOUND NR 1 OVERSPEED VALVE BYPASSING AIR. PART HAD BEEN INSTALLED FOR 115.4 HRS SINCE O/H.SDR O842010F00000Starter Gen · malfunctionedGENERATOR WOULD NOT GO ON-LINE AFTER ENGINE START FOR RETURN FLIGHT BACK TO HOME BASE FROM HELIPAD AFTER PATIENT DROP-OFF.SDR 2009FA0000961Fuel Control · unserviceableCOMPONENT HAS A HISTORY OF CAUSING ENG TO MOMENTARILY DECELERATE AS THROTTLE IS ADVANCED PAST THE IDLE STOP TO FLIGHT. DECELERATION CAN BE OVERCOME BY CONTINUING TO ADVANCE THROTTLE THROUGH THE DECELERATION. ONCE THROUGH DECELERATION A MAXIMUM OF ONLY 90 PERSDR HEEA126365Pitch Horn · crackedDURING DAILY INSPECTION FOUND MAIN ROTOR BLADE PITCH HORN CRACKED AT AFT LOWER TRAILING EDGE. REPLACED PITCH HORN WHICH WAS 50.58 HOURS FROM RETIREMENT.SDR O842009F00000Bolt · sheared2 BOLTS HOLDING THE BACK PUMP COVER ON, SHEARED AND ALLOWED ALL OF THE FLUID IN THE SYSTEM TO BE PUMPED OVERBOARD CAUSING A LOSS OF THE NR 1 HYD SYS. (K)SDR QMLA1124200808054Pump · overheatedAPPROX 2-3 MILES FROM HOSPITAL FUMES IN COCKPIT AND CABIN. NO INDICATION IN THE COCKPIT, OTHER THAN THE SMELL THAT ANYTHING WAS ABNORMAL. ELECTED TO CONTINUE TO THE DESTINATION. REDUCED THE ELECTRICAL LOAD AS MUCH AS POSSIBLE AND RELAYED TO THE CREW TO TURNSDR HEER117546Swashplate · brokenTHE MECHANIC NOTICED THE CYCLIC LINK HAD COME IN CONTACT WITH THE INNER RING AND DURING HIS INVESTIGATION TO DETERMINE THE CAUSE OF THIS UNUSUAL CONDITION, HE FOUND SEVERAL PARTS TO BE EXCESSIVELY DAMAGED CAUSED BY A BROKEN BOLT 20-057-6-16D, TOTAL TIME 1688.SDR CA070502002Hanger Assy · failed(CAN) T/R HANGAR BEARING ASSY FAILURE WAS DISCOVERED AFTER THE PILOT WAS ALERTED BY AN UNUSUAL NOISE UPON ENGINE START. (TC NR 20070502002)SDR O84A115223Hanger Assy · wornFWD TAIL ROTOR HANGER BEARING FAILED. SAFETY STRAP WAS THE ONLY THING HOLDING DRIVESHAFT IN PLACE. PILOT AND CREW NOTICED A MOMENTARY KNOCKING NOISE AFTER NR 1 ENGINE AT IDLE ONLY. CONTACTED BELL PRODUCT SUPPORT AND REPLACED HANGER BEARING ASSY. AFTER INSPSDR O84A114543Starter Gen · unserviceableNR 1 GENERATOR FAILED IN CRUSE FLIGHT AND AFTER SHUTDOWN COULD NOT START NR 1 ENGINE DUE TO STARTER WOULD NOT MOTOR. ONE BRUSH WORN BEYOND LIMITS. REPLACED STARTER / GENERATOR.SDR HEEA107326Engine · power lossON TAKEOFF, THE NR 2 ENGINE LOST POWER. PILOT PERFORMED SINGLE ENGINE LANDING. REPLACED ENGINE ASSEMBLY.SDR 2005FA0001132Bearing · vibrationLT COLLECTIVE LEVER SUPPORT BEARING FAILED CAUSING MAIN ROTOR VERT VIBRATION AND LOWER COLLECTIVE LEVER IDLER ELASTROMERIC BEARINGS TO FAIL AND SOME WERE IN MAIN TRANSMISSION UPPER LUGS/ATTACHMENT POINT TO WEAR. DISCUSSED WITH MFG PAODUCT SUPPORT.SDR HEEA094158Starter Gen · failedDURING CRUISE FLIGHT, NR 2 DC GENERATOR LIGHT ILLUMINATED. PILOT FOLLOWED AIRCRAFT EMERGENCY CHECKLIST FOR SINGLE DC GENERATOR FAILURE AND LANDED AIRCRAFT. MAINTENANCE REPLACED NR 2 STARTER GENERATOR.SDR BAQA091650Starter Gen · malfunctionedSTARTER GEN PRODUCING LOW STARTING SPEED, SPARKS ON STARTUP, LOUD RADIO NOISE. PART REPLACED WITH SERVICABLE UNIT.SDR CA040217011Blade · damaged(CAN) DURING ROUTINE FLIGHT, A 6.5 INCH PIECE OF DOUBLER BROKE OFF FROM THE BLADE, CAUSING VIBRATIONS.SDR HEEA092088Connector · contaminatedDURING FLIGHT, NR2 ENGINE OVERSPEED LIGHT ILLUMINATED. MAINTENANCE CLEANED OIL CONTAMINATION FROM THE CONNECTOR TO THE NR 2 ENGINE OVERSPEED CONTROL.SDR BAQA090021Bearing · wornISOLATION MOUNT BEARING OUT OF LIMITS.SDR HEEA088920Panel · brokenLIGHTED PANEL RECEIVED BROKEN WHEN UNPACKED.SDR HEEA088495Isolation Mount · damagedSEPERATION BETWEEN ELASTOMER AND CENTER PORTION OF MOUNT.SDR HEEA086664Transponder · intermittentATC TRANSPONDER FOUND FAULTY. INTERMITTENT OPERTION. CONTROL HEAD WILL DISPLAY "FAIL". IN SHOP REPAIR.SDR TU32003F00006Mount · wornATTACHING END OF FLEXTURE WORN AND NEEDS BUFFER PAD REPLACED.SDR TU32003F00005Liner · wornATTACHING END AT FLEXTURE WORN AND NEEDS BUFFER PAD REPLACED.SDR TU32003F00004Bearing · debondedRUBBER DEBONDED BEYOND LIMITS.SDR TU32003F00002Bearing · debondedELASTOMERIC DEBONDED FROM BEARING HOUSING.SDR TU32003F00001Bearing · debondedELASTOMERIC DEBONDED FROM BEARING HOUSING. (SN/ LK0326, LK1013, LK0308, LK0810)SDR TU32003F00000Bearing · wornBEARINGS WORN BEYOND LIMITS WITH SHORT AMOUNT OF FLIGHT TIME ON COMPONENT.SDR HEEA084425Search Light · malfunctionedSEARCH LIGHT DOES NOT RETRACT ALL THE TIME.SDR HEEA084424Coupling · leakingCOUPLING LEAKING GREASE. REPLACED OUTER COUPLING DUE TO PITTING IN RETAINER GROOVE. REPAIRED.SDR YT2R727264Switch · inoperativePRESSURE SWITCH SLOWED TO SHUTOFF CAUTION LIGHT.SDR YT2R727265Switch · leakingENGINE OIL PRESSURE SWITCH LEAKING.SDR SVB2003F00000Seal · leakingRAPID SERVO LEAK EMPTIED NR 1 HYDRAULIC SYSTEM IN LESS THAN 6 MINUTES. COLLECTIVE CYCLIC SERVO CONTINUED TO FUNCTION ON NR 2 HYDRAULIC SYSTEM BUT TAIL ROTOR CONTROLS WERE INOPERATIVE REQUIRING A FORCED LANDING.SDR CA030305006Blade · cracked(CAN) THE BLADE WAS SENT IN FOR A HARD LANDING INSPECTION (NOT A BLADE STRIKE). UPON INSPECTION THE ROTOR BLADE WAS FOUND CRACKED ON THE UPPER SURFACE STATION 224.0 NEAR THE TIP INERTIA WEIGHT. THE CRACK ORIGINATED AT A FASTENER HOLE AND PROGRESSED THROUGH THESDR HEEA082568Gearbox · shortedSEARCH LIGHT HAS AN ELECTRICAL SHORT LOCATED IN THE ROTATION AXIS GEARBOX.SDR TU3R12048Bearing · delaminatedDURING MAIN ROTOR TRACK AND BALANCE FLIGHTS, THE CREW WOULD HAVE THE RIDE, ACCEPTABLE BY FEEL AND BY READINGS, AND RELEASE THE AIRCRAFT FOR SERVICE. THE NEXT FLIGHT THE RIDE WOULD BE WORSE. DURING THE INSPECTION OF THE ROTOR SYSTEM, THE HYDRAULIC CART WAS CSDR HEEA080439Computer · damagedFOUND PROBLEM TO BE IN THE "FORCE TRIM CB ON" LOGIC. PREFLIGHT TEST IS NORMAL HOWEVER AUTOPILOT WILL NOT ENGAGE. ENTERED DIAGNOSTIC MODE AND INTO THE DISCRETE I/O SCREEN. FOUND BIT NR 13 OF PORT 1 IN THE DISCRETE INPUTS TO BE "1" WITH THE FORCE TRIM CB IN. SDR HEEA080106Brushes · wornSTARTER GEN HAS WORN BRUSHES.SDR HEEA079739Computer · failedCOMPUTER WILL NOT ENGAGE AUTO PILOT WHEN AP BUTTON IS DEPRESSED.SDR HEEA079412Brushes · wornSTARTER GEN BRUSHES EXCESSIVELY WORN.SDR HEEA079091Indicator · malfunctionedENGINE NG INDICATOR HAS A FLUCTUATING NEEDLE.SDR HEEA078704Turbine Wheel · damagedTURBINE REMOVED FOR OVERHAUL. UPON INSPECTION OF TURBINE PARTS NOTED LIGHT SULFIDATION ON BACK SIDE OF 1ST STAGE WHEEL LEADING EDGE BLADES. SCRAPPED.SDR HEEA078537Gyro · failedINOPERATIVE WITH ATTITUDE FAIL DISPLAYED ON EADI. SENT TO GREATLAKES AVIONICS FOR INSPECTION AND REPAIR.SDR HEEA078024Isolation Mount · failedIN CRUISE FLIGHT, AN AIRFRAME VIBRATION DEVELOPED. MAINTENANCE FOUND THE LATERAL ISOLATION MOUNT FAILED. MAINTENANCE REPLACED THE ISOLATION AMPLIFIER.SDR HEEA077440Bearing · delaminatedBEARING HAS DELAMINATED ELASTOMER.SDR HEEA076980Bearing · delaminatedDELAMINATION. PENDING VENDOR REPAIR.SDR HEEA076581Indicator · precessesINTERMITTENT PROBLEM OF PRECESSING 30 DEGREES. REPLACED WITH SERVICEABLE PART.SDR 2002FA0000029Pitch Horn · crackedCRACK FOUND ON MAIN ROTOR GRIP AT BOLT HOLE WHERE GRIP ATTACHES TO PITCH HORN. CRACK EXTENDED FROM BOLT HOLE FOR 1.5 FEET TO OUTSIDE OF GRIP.SDR HEEA073641Receiver · malfunctionedCAUSES DISPLAY TO FLICKER AND TURN OFF. SENDING TO VENDOR FOR REPAIR.SDR 20010529CW008Quill · misoverhauledEXCESSIVE OIL LEAKAGE, PAST CORK PN 120-179-13A. IN INNER QUILL ASSEMBLY OF OUTBOARD QUILL. CORK INSTALLED INCORRECTLY BY OVERHAUL FACILITY. RIGHT HAD OUTBOARD QUILL PN 222-040-022-108 OF SAME TRANSMISSION, HAD SAME PROBLEM AT THE SAME TIME.SDR TI1R001407Symbol Generator · defectiveSG465 - WOULD NOT ALLOW AUTOPILOT TO ENGAGE. REMOVED AND REPLACED.
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