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 = '212' 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 = '212' 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 CA030213003Case · punctured(CAN) PIN SIZE HOLE LOCATED ON NR 2 PT6T-3 POWER SECTION GAS GENERATOR CASE AT APPROXIMATELY 7 O'CLOCK POSITION 3 3/4 INCHES AFT OF FIRST CIRCUMFIRENTIAL SEAM WELD (BY P3 AIR BOSS SUPPLYING AIR TO TORQUEMETER CLUTCH SEAL) WHILE PERFORMING VISUAL INSPECTION OF SDR CA030603010Bulkhead · cracked(CAN) TAIL BOOM ATTACH BULKHEAD AT STA 243.937, P/N 212030156047. CRACK UNDER 1 INCH LENGTH. BULKHEAD REPLACED WITH NEW.SDR CA030603009Angle · cracked(CAN) CRACK IS IN ANGLE ONLY, NOT FITTING.SDR CA030220002Bearing Race · spalled(CAN) A WEEK PREVIOUS, THE BELL 212 HAD A CHIP LIGHT ON THE M/R TRANSMISSION. THE CHIP PLUGS WERE PULLED AND THE ENGINEER FOUND FINE FUZZ AND SLIVERS, INSIGNIFICANT TO WARRANT FURTHER INVESTIGATION BUT TO MONITOR. NEXT WEEK THE PILOT REPORTED THAT THE CHIP LIGSDR HEEA083550Sleeve · corrodedTAIL ROTOR GEARBOX SLEEVE IS CORRODED.SDR HEEA083047Gear · wornMAIN ROTOR GEARBOX GEAR HAS WORN WHERE SEAL RIDES.SDR CA030108018Bearing · failed(CAN) PILOT OBSERVED NR 1 GENERATOR FAIL CAUTION LIGHT FLICKERING WHILE IN NORMAL CRUISE FLIGHT. NORMAL OPERATION CONTINUED ON NR 2 SYSTEM. NR 1 STARTER-GENERATOR WOULD NOT CRANK ON NEXT START AND WAS REPLACED WITH A SERVICEABLE UNIT. UNIT IS AWAITING DISSASEMSDR CA021231002Fuel Control · malfunctioned(CAN) WHILE STARTING, THE START WENT HOT & THE START WAS ABORTED. THE NEXT START WAS A VERY LONG START WITH THE N1 HANGING UP AT 71 PERCENT WITH NO ACCELERATION PAST 71 PERCENT. THE HELICOPTER WAS STARTED USING THE MANUAL FUEL CONTROL AND THE START WAS NORMAL.SDR HEEA082574Float · failedDURING MANUAL INFLATION INSPECTION, BAG FAILED AT 3 EACH INLET AREAS. BAG MATERIAL SEPARATED AT SWIVEL ATTACHMENT ALLOWING NITROGEN TO ESCAPE OUTSIDE THE BAG.SDR HEEA082573Inverter · failedAC INVERTER FAILED IN FLIGHT.SDR HEEA082572Cvr · malfunctionedCOCKPIT VOICE RECORDER CAUSES TEST LIGHT TO STAY ON.SDR HEEA082571Damper · wornDAMPER HAS WORN INNER MEMBER AND BEARING LOOSE. REPAIRED. REPLACED HOUSING P/N J99941 DUE TO WEAR.SDR HEEA082570Transistor · failedVHF TRANSCIEVER HAS GARBLED TRANSMIT AND RECEIVE. REMOVED CORROSION FROM CHASSIS. REPLACED BAD Q110 TRANSISTOR SOCKET. FOUND REALIGNED RECEIVER AND TRANSMITTER. UNIT BENCH CHECK GOOD.SDR HEEA082564Bearing · roughINOPERATIVE. BALL BEARING ROUGH. REPAIRED AND REPLACED BALL BEARING.SDR HEEA082563Interphone · malfunctionedUNIT BLEEDS OVER WHEN FM IS SELECTED. PERFORMED PRELIMINARY INSPECTION. CLEANED S1 SELECTOR SWITCH. REPAIRED PROBLEM. ALSO REPLACED BAD LIGHT PANEL AND COMPLETED TESTING UNIT. UNIT BENCH CHECK GOOD.SDR CA021204001Line · broken(CAN) THE GOVERNOR WAS LAGGING BEHIND. THE ENGINEER CARRIED OUT SOME ADJUSTMENTS BUT THE ADJUSTMENTS DID NOT HELP. A P3 AIR LEAK CHECK WAS CARRIED OUT AND THE ENGINEER DISCOVERED AIR LEAKING NEAR THE P3 AIR FILTER. FURTHER INVESTIGATION REVEALED THE LINE WAS BSDR CA021016003Chip Detector · flaking(CAN) TIN PLATING OF CHIP DETECTOR POLES FOUND TO BE FLAKING OFF, POTENTIAL FOR ERRONEOUS INDICATION. PART REPLACED WITH SERVICEABLE UNIT AND SENT TO MANUFACTURER FOR ANALYSIS.SDR CA021001004Bracket · cracked(CAN) IN THE PROCESS OF DOING A 3000 HOUR INSPECTION ON THE TAILBOOM LEFT HAND ELEVATOR, THE ENGINEER FOUND THE ELEVATOR ATTACHMENT LUG BRACKET CRACKED. THE CRACK WAS ON THE AFT SIDE ATTACHMENT LUG BRACKET B ELOW THE ATTACHMENT LUG, BETWEEN THE 1ST AND 2ND RISDR ERAA080462Skin · crackedTAILBOOM HAS CRACK ON SADDLE DOUBLER RT BASE OF VERTICAL FIN. FOUND SADDLE DOUBLER TO BOTH BE CRACKED AND LOWER SKIN BENEATH DOUBLERS CRACKED. REMOVED BOTH SADDLE DOUBLERS AND SKIN AND FOUND LOWER SKIN TO BE CRACKED. MUST BE SENT OFF TO REPAIR IN FIXTURE.SDR HEEA080444Fuel Control · malfunctionedNR 2 ENGINE HAS N1 AND TORQUE OSCILLATIONS. REPLACED WITH SERVICEABLE FUEL CONTROL.SDR HEEA080443Fuel Control · malfunctionedENGINE HAD TORQUE AND N1 OSCILLATIONS. REPLACED WITH SERVICEABLE FUEL CONTROL.SDR HEEA080442Bearing · wornWORN BEARING P/N MS027647-4. REPLACED BEARING AND RETURNED TO SERVICE.SDR EHA2002F00009Fuel Control · failedON APPROACH TO LANDING AT A REMOTE LOCATION, THE PILOT EXPERIENCED A LOW SIDE GOVERNING FAILURE ON THE NR 2 AUTOMATION FUEL CONTROL UNIT. THE AFCU WAS PUT ON IAW MEL AND A FERRY FLIGHT PERMIT WAS ISSUED. THE AIRCRAFT RETURNED AND THE AFCU WAS CHANGED.SDR CA020827006Bearing · spalled(CAN) THE PILOT WAS FLYING WHEN THE MASTER CAUTION LIGHT ACTIVED. THE ENGINE CHIP LIGHT ON THE NR 1 SIDE ALSO ACTIVED. THE PILOT LANDED AS SOON AS PRACTICAL. THE REDUCTION GEARBOX AND BOTH POWER SECTIONS WERE REMOVED. THE SOURCE OF METAL WAS LOCATED. IT WSDR CA020718011Engine · failed(CAN) AFTER TAKEOFF ON A SCHEDULED TRIP FROM THE FIRE CAMP, THE PILOT LEELLED THE AIRCRAFT AND REDUCED POWER TO NORMAL CRUISE POWER. AT THIS MOMENT HE HEARD A LOUD BANG AND FELT A PRONOUNCED YAW. THE NR 1 ENGINE OUT LIGHT ILLUMINATED AND ALL NR 1 ENGINE INSTRUSDR HEEA080114Diaphragm · damagedINCREASE OF 75 DEGREES ITT AND 4.5 PERCENT N1 IN CRUISE FLIGHT. FOUND HOLE IN DIAPHRAGM. REPLACED.SDR HEEA080109Quill · leakingQUILL ASSY LEAKING. WORN SPACER P/N 212-040-156-001. REPLACED SPACER.SDR HEEA080108Float · damagedHOLE IN FLOAT BAG.SDR HEEA080107Cylinder · corrodedCAUSING A LEAK DURING TEST BETWEEN LOWER CYLINDER AND CONNECTING CYLINDER. FOUND A SMALL PIT IN LOWER CYLINDER I.D. IN AREA WHERE THE ORING SEALS ON THE CONNECTING CYLINDER. SENT TO FORTNER ACCESSORY SERVICE CORP. FOR INSPECTION AND REPAIR.SDR CA020718008Support · broken(CAN) AFTER LANDING THE AIRCRAFT, THE PILOT HEARD A LOUD BANG. THE AIRCRAFT DID NOT MOVE AND THERE WAS NO INDICATON OF ANY MALFUNCTION ON THE INSTRUMENTS. THE PILOT OPENED THE CREW DOOR AND SAW THE RT SKID TUBE SLIPPED OUT TO THE RIGHT. INSPECTION REEALED THATSDR CA020626018Valve · failed(CAN) FLOAT BAGS FOUND TO BE PARTIALLY INFLATED, BOTTLE PRESSURE DOWN 1100 PSI. BOTTLE HAD BEEN LOOSING CHARGE OVER TIME. INVESTIGATION/TROUBLESHOOTING INCLUDED REPLACEMENT OF RELIEF VALVE AND CHARGE VALVE. FINAL DISSASEMBLY DETERMINED SHEAR HEAD TO HAVE FAISDR CA031110005Line · chafed(CAN) DURING THE PRE-FLIGHT COCKPIT CHECKS WHILE THE AIRCRAFT WAS ON THE GROUND WITH ENGINES STARTED, THE PILOT NOTICED NR 2 HYDRAULIC PRESSURE LOSS. THE AIRCRAFT WAS SHUT DOWN FOR FURTHER INVESTIGATION. A HYDRAULIC LINE IN THE (HELL HOLE) WAS FOUND TO BE CHSDR HEEA080095Valve · malfunctionedWHEN ENGINES ARE REDUCED TO IDLE TRANSMISSION OIL PRESSURE DROPS BELOW LOW RED AND TRANSMISSION OIL PRESSURE LIGHT ILLUMINATES. ADVANCING EITHER ENGINE TO 70 PERCENT N1 RESTORES PRESSURE TO NORMAL RANGE. WHEN OIL PRESSURE RELIEF VALVE WAS REMOVED IT WAS FOUNSDR HEEA080094Damper · damagedRIGHT HAND FRICTION DAMPER LOWER ATTACHMENT EARS BROKEN. REPAIRED.SDR CA020815002Case · cracked(CAN) POWER SECTION WAS REMOVED DUE LOW POWER.SDR EHA2002F00005Fire Loop · brokenAPPROX 0.5 HOURS AFTER TAKEOFF, ENROUTE FOR CROSS COUNTRY, THE NR 1 ENGINE FIRE (T) HANDLE ILLUMINATED IN FLIGHT. HANDLE WAS PULLED TO FIRE NR 1 ENGINE MAIN FIRE BOTTLE, NR 1 ENGINE WAS SHUT DOWN AND SECURED, AND HELICOPTER RETURNED TO BASE. UPON INSPECTION SDR HEEA079752Indicator · malfunctionedRADAR SCREEN FLASHES ON THEN OFF WITH DISTORTED IMAGING. COULD NOT DUPLICATE PROBLEM. INSTALLED MOD 9. REPLACED U1901, U1902, U1903, IC ON PAGE DISPLAY BOARD. REPAIRED. BENCH CHECK GOOD.SDR HEEA079751Switch · failedCONTROL HEAD ON/OFF SWITCH INTERMITTENT. ON/OFF SWITCH BAD. REPLACED BAD S2 ON/OFF SWITCH. REPAIRED. BENCH CHECK GOOD.SDR HEEA079750Control Head · malfunctionedCONTROL HEAD WILL NOT RECEIVE ON 120.5 MHZ. FOUND BAD CR3 DIODE. BENCH CHECK GOOD.SDR HEEA079749Ferrule · looseHYD LINE LEAKING AT FITTING FERRULE LOOSE ON LINE. SCRAPPED.SDR HEEA079748Line · leakingHOLE IN HYDRAULIC LINE. SCRAPPED.SDR HEEA079747Indicator · inoperativeENGINE N1 INDICATOR INOPERATIVE.SDR HEEA079746Transceiver · inoperativeVHF TRANSCEIVER NON FUNCTIONAL.SDR HEEA079745Coupling · stuckVHF ANTENNA COUPLING INTERMITTENTLY STICKS DURING TUNING PROCESS AND FILTER FITTING LOOSE.SDR HEEA079744Transceiver · inoperativeVHF TRANSCEIVER WILL NOT TRANSMIT. FOUND TRANSMITTER VERY INTERMITTENT WHEN VIBRATED. FOUND COLD SOLDER ON PIN 1 OF P301 CONNECTOR. RESOLDERED PINS ON P301 CONNECTOR. REPAIRED. BENCH CHECK GOOD.SDR HEEA079743Transceiver · malfunctionedVHF TRANSCEIVER VERY GARBLED TRANSMISSION. REMOVED CORROSION BUILD UP UNDERNEATH VCO SHIELD ON BOTTOM OF SYNTHESIZER BOARD. BENCH CHECK GOOD.SDR HEEA079742Transceiver · weakVHF TRANSCEIVER WEAK AND GARBLED. REPLACED WITH SERVICEABLE PART.SDR HEEA079741Transceiver · malfunctionedNO TRANSMIT. FOUND TRANSMIT POWER AND MODULATION FLUCTUATING. REMOVED CORROSION FROM RECEIVER/MODULATOR BOARD AND BOTTOM OF SYNTHESIZER BOARD IN VCO SECTION. APPLIED HUMISEAL TO VCO SECTION ON BOTTOM OF SYNTHESIZER BOARD FOR CORROSION CONTROL. REALIGNED TRASDR HEEA079740Transceiver · inoperativeVHF TRANSCEIVER WILL NOT TRANSMIT OR RECEIVE. REPLACED WITH SERVICEABLE PART.SDR HEEA079736Interphone · inoperativeFM2 SWITCH WILL NOT TURN OFF FM. CLEANED S1 SWITCH. REPLACED S1 SWITCH. ALSO REPLACED BAD R72 VOLUME CONTROL, BAD S4, S5, S6, S7, S8 AND S11 SWITCHES, BAD SELECTOR AND VOLUME KNOBS AND BAD FACEPLATE. REPAIRED. BENCH CHECK GOOD.
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