Bell 214ST

Service difficulty reports · 1,513

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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 = '214ST'
  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.

SDR HEEA113269Hose · rupturedNR 1 HYDRAULIC PUMP CAPTION ILLUMINATED WITH PRESSURE AT ZERO, PRESSURE FLUCTUATED A COUPLE OF TIMES ACCOMPANIED WITH A LOUD NOISE. MAINTENANCE FOUND NR 1 SYSTEM PRESSURE HOSE TO THE CYCLIC SERVO RUPTURED.Dec 17, 2006 · N8045T · Bell 214ST · Hydraulic System, MainSDR HEEA111397Oil Cooler · contaminatedOIL COOLER CAUTION LIGHT ILLUMINATED IN FLIGHT WITH ASSOCIATED UTILITY HYD CAUTION LIGHT FLICKERING. APPROPRIATE EMERGENCY PROCEDURE PERFORMED. MAINTENANCE CLEANED GRASS BUILDUP FROM OIL COOLER CORE.Oct 6, 2006 · N5748M · Bell 214ST · Hydraulic System, MainSDR HEEA111000Pump · failedNR 2 FUEL TRANSFER PUMP FAILED, CONTINUED WITH NO FURTHER PROBLEMS. MAINTENANCE REPLACED THE NR 2 TRANSFER PUMP.Aug 31, 2006 · N59806 · Bell 214ST · Aircraft Fuel Distribution SystemSDR HEEA109638Pressure Switch · malfunctionedDURING CRUISE FLIGHT THE NR 1 HYD CAUTION LIGHT CAME ON. PERFORMED THE EMERGENCY CHECKLIST AND THEN DEVIATED TO FOU. MAINTENANCE REPLACED PRESSURE SWITCH.Jun 13, 2006 · N8045T · Bell 214ST · Hydraulic Pressure Regulator, MainSDR HEEA109301Clip · failedON FINAL TO GB426 NR 2 HYDRAULIC FAILED, LIGHT AND GAUGE LOSS OF PRESSURE. SHUTDOWN. MAINTENANCE REPLACED PUMP RETAINER CLIP.May 18, 2006 · N59806 · Bell 214ST · Hydraulic System, MainSDR HEEA109166Pump · failedAFTER TAKEOFF, THE NR 1 TRANSFER LIGHT CAME ON. MAINTENANCE REPLACED THE NR 1 FUEL TRANSFER PUMP.May 10, 2006 · N5748M · Bell 214ST · Fuel Boost PumpSDR ALG2006F00036Wire · shortedIN FLIGHT, BOTH ELEVATORS FAILED, AARS ROLL FAILED, SCAS PITCH FAILED, AND FBW ELEVATORS WENT FULL UP. THE AIRCRAFT ROLLED LT AND PITCHED UP. WITH FULL FWD AND FULL RT CYCLIC, PILOTS DID NOT REGAIN CYCLIC CONTROL UNTIL THE AIRSPEED HAD DROPPED BELOW 100 KTS.Apr 17, 2006 · N391AL · Bell 214ST · Auto Flight System WiringSDR ALG2006F00035Current Limiter · inoperativeIN FLIGHT, EN ROUTE, THE FOLLOWING INDICATION WENT TO (0). NR 1 NG, NR 1 ENG PRESS, TEMP, C-BOX PRESS, NR 1 HYD PRESS, NR 2 HYD TEMP. NO CAUTION LIGHTS ILLUMINATED. AC DIVERTED, MAINTENANCE REMOVED AND REPLACED NR 1 CURRENT LIMITER, (PN 209-375-096-103). (Mar 31, 2006 · N392AL · Bell 214ST · DC RegulatorSDR HEEA108122Swashplate · out of adjust3 MINUTES AFTER TAKEOFF, A LOW RUMBLE WAS HEARD FOLLOWED BY A VERTICAL VIBRATION. AIRCRAFT WAS FLOWN AND SHUT DOWN WAS ACCOMPLISHED. UPON INSPECTION THE AIRCRAFT GREASE WAS FOUND SPLATTERED OVER THE UPPER TRANSMISSION COWLING. MAINTENANCE FOUND THE SWASHPLFeb 16, 2006 · N3897N · Bell 214ST · Main Rotor Mast/SwashplateSDR HEEA107966Window · missingDURING TAKEOFF CREW HEARD POPPING NOISE AND NOTICED PILOT'S SKYLIGHT MISSING, APPARENTLY CAME OFF DURING TAKEOFF.Feb 7, 2006 · N59806 · Bell 214ST · Flight Compartment WindowsSDR HEEA107922Packing · cutDURING CRUISE FLIGHT NR 2 ENGINE OIL PRESSURE DECREASED TO APPROXIMATELY 15 PSI OVER ABOUT 60 SECONDS. ENGINE OIL PRESSURE EMERGENCY PROCEDURE WAS PERFORMED. AIRCRAFT DIVERTED FOR OEI LANDING. MAINTENANCE FOUND A CUT PACKING ON THE ENGINE CHIP PLUG ALLOWINJan 17, 2006 · N8045T · Bell 214ST · Engine Oil PressureSDR HEEA107418Pump · poppedDURING CRUISE FLIGHT, THE NR 2 TRANSFER LIGHT ILLUMINATED AND CIRCUIT BREAKER POPPED. FOLLOWED EMERGENCY PROCEDURE AND LANDED. MAINTENANCE REPLACED NR 2 TRANSFER PUMP.Dec 14, 2005 · N3897N · Bell 214ST · Fuel Transfer ValveSDR ALG2005F00121Filter · failedON TAKEOFF, NR 2 ENGINE FUEL FILTER LIGHT CAME ON, AND THE PILOT LANDED THE AC. THE MECHANIC REMOVED AND REPLACED NR 2 ENGINE FUEL FILTER ELEMENT, GROUND RUN AND LEAK CHECKED IAW MM, AC WAS RETURNED TO SERVICE. (K)Dec 6, 2005 · N391AL · Bell 214ST · Aircraft Fuel Filter/StrainerSDR HEEA107317Wire · chafedSCAS FAILED IN FLIGHT. ATTEMPTED TO RESET IT BUT IT BLEW THE CIRCUIT BREAKER. SECURED OFF AND CONTINUED TO BASE WITHOUT INCIDENT. MAINTENANCE REPAIRED CHAFED WIRE WHICH RUNS BETWEEN THE SCAS AMP AND THE YAW ACTUATOR.Dec 1, 2005 · N59806 · Bell 214ST · Auto Flight System WiringSDR HEEA107322Wire · brokenIN FLIGHT, NR 2 FUEL VALVE CAUTION LIGHT ILLUMINATED. DEVIATED TO HOUMA AND NOTIFIED MAINTENANCE. MAINTENANCE FOUND BROKEN WIRE BEHIND INSTRUMENT PANEL APPROXIMATELY 8.Nov 2, 2005 · N8045T · Bell 214ST · Instrument System WiringSDR ALG2005F00056Line · leakingENROUTE, A HOWLING NOISE STARTED AND BECAME LOUDER, THE PILOT NOTICED NR 1 HYD PRESSURE FLUCTUATED BETWEEN 200-300 PSI. THE PILOT TURNED OFF NR 1 HYD NOISE WENT AWAY. UPON LANDING THE MECHANIC FOUND NR 1 PRESSURE LINE TO THE COLLECTIVE SERVO IS LEAKING. HE Jul 30, 2005 · N390AL · Bell 214ST · Hydraulic System, MainSDR HEEA107351Engine · malfunctionedIN CRUISE, NR 1 ENGINE NR AND NG AND MGT WENT HIGH, TORQUE AND NP SHOWED ZERO, REDUCED NR 1 THROTTLE AND PERFORMED CHECKLIST AND SHUT ENGINE DOWN. ROTOR RPM WENT TO 107 FOR 10 SECONDS. INSPECTED ENGINE AND REPLACED YELLOW ENGINE HARNESS AND ECU.Jul 22, 2005 · N3897N · Bell 214ST · Engine (Turbine/Turboprop)SDR HEEA107332Nut · splitSHORTLY AFTER TAKEOFF, THE NR 2 HYDRAULIC LIGHT ILLUMINATED. RETURNED TO MORGAN CITY. MAINTENANCE FOUND A JAM NUT ON A FITTING ON THE HYDRAULIC MANIFOLD SPLIT ALLOWING THE PACKING TO UNSEAT UNDER PRESSURE CAUSING THE LOSS OF HYDRAULIC FLUID. REPLACED THE NJun 24, 2005 · N5748M · Bell 214ST · Hydraulic Pump (Electric/Engine), MainSDR CA050309001Tube · chafed(CAN) DURING ROUTINE MAINTENANCE, THE SUBJECT TUBE WAS FOUND WITH A (0.375 INCH X 0.187 INCH) HOLE THAT ORIGINATED FROM CHAFING WITH A HYDRAULIC OIL LINE. THE HOLE WAS LOCATED APPROXIMATELY IN THE CENTER OF THE TUBE. THE TOTAL CHAFING DAMAGE IN THIS AREA, COMar 1, 2005 · Bell 214ST · Hydraulic System, MainSDR HEEA107347Tube · leakingIN CRUISE FLIGHT UTILITY HYDRAULIC AND OIL COOLER SEGMENT LIGHTS ILLUMINATED. FOLLOWED APPROPRIATE EMERGENCY CHECKLISTS AND RETURNED TO MCY. MAINTENANCE FOUND PIN HOLE IN TUBE UNDER ADEL CLAMP.Feb 22, 2005 · N59806 · Bell 214ST · Hydraulic System, MainSDR HEEA107339Pressure Switch · malfunctionedDURING CRUISE FLIGHT TRANSMISSION CAUTION LIGHT ILLUMINATED. MAINTENANCE REPLACED THE PRESSURE SWITCH AND THERMO SWITCH 214-040-805-001.Feb 9, 2005 · N59806 · Bell 214ST · Rotor Drive Indicating SystemSDR ALG2004F00059Warning Light · activatedFIVE MINUTES AFTER TAKEOFF, AC815 TRANSMISSION CHIP LIGHT ILLUMINATED, PILOT RETURNED TO RIG. MECHANIC REMOVED, CLEANED, AND INSPECTED ALL TRANSMISSION CHIP PLUGS, NO CONTAMINANTS NOTED. CONNECTOR PLUGS WERE EXAMINED AND FOUND SERVICEABLE. AC WAS RETURNED TOct 11, 2004 · N392AL · Bell 214ST · Main Rotor Mast/SwashplateSDR HEEA096490Bleed Valve · malfunctionedWHILE HOVERING FOR TAKEOFF, NR 2 MGT STARTED RISING. MGT SPIKED AT 933 DEGREES THREE TIMES, THEN STAYED AT 933 DEGREES. AIRCRAFT WAS SENT DOWN AND MGT RETURNED TO NORMAL FLAT PITCH.Jun 22, 2004 · N59806 · Bell 214ST · Compressor Bleed ValveSDR HEEA096018Bleed Valve · malfunctionedWHILE HOVERING FOR TAKEOFF,NR 2 MGT STARTING RISING. MGT SPIKED AT 933 DEGREES THREE TIMES, THEN STAYED AT 933 DEGREES. AIRCRAFT WAS SENT DOWN AND MGT RETURNED TO NORMAL FLAT PITCH.Jun 22, 2004 · N59806 · Bell 214ST · Compressor Bleed ValveSDR ALG2004F00023Ecu · failedNR 1 ENGINE FAILED DURING TAKE OFF, AIRCRAFT RETURNED TO PLATFORM. MAINT REMOVED NR 1 ENGINE HMU AND INSTALLED SERVICEABLE HMU. ALSO REMOVED NR 1 ENGINE ECU AND INSTALLED SERVICEABLE ECU.May 11, 2004 · N391AL · Bell 214ST · Fuel Control/Turbine EnginesSDR HEEA094228Bearing · failedTRANSMISSION CHIP LIGHT ILLUMINATED IN FLIGHT. AIRCRAFT LANDED AT POINT SU FUR. MAINTENANCE FOUND BEARINGS IN THE ROTOR BRAKE QUILL HAD FAILED.Apr 12, 2004 · N59806 · Bell 214ST · Main Rotor GearboxSDR HEEA093678Hose · rupturedNR 1 HYDRAULIC SYSTEM FAILED IN FLIGHT. LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A HOSE RUPTURED. REPLACED HOSE. ALSO REPLACED PUMP DUE TO RUNNING DRY.Feb 25, 2004 · N8045T · Bell 214ST · Hydraulic System, MainSDR HEEA093479Packing · leakingTHE OIL COOLER WARNING LIGHT ILLUMINATED. RETURNED. FOUND A CUT PACKING ON FITTING ON UTILITY HYDRAULIC PUMP ALLOWING ALL FLUID TO LEAK OUT. REPLACED PACKING.Feb 17, 2004 · N8045T · Bell 214ST · Hydraulic System, MainSDR HEEA093477Coupling · crackedOIL COOLER CAUTION LIGHT ILLUMINATED IN FLIGHT. REPLACED CRACKED UNION ON THE UTILITY HYDRAULIC PUMP.Feb 15, 2004 · N8045T · Bell 214ST · Hydraulic System, MainSDR HEEA093478Warning Light · illuminated45 MINUTES AFTER TAKEOFF, PILOT REPORTED LOW PRESSURE READING ON NR 2 OIL PRESSURE GAUGE. RETURNED TO MCY.Jan 25, 2004 · N5748M · Bell 214ST · Engine Oil PressureSDR HEEA092089Ecu · malfunctionedSHORTLY AFTER TAKE OFF NR 1 ENGINE TORQUE FLUCTUATED. MAINTENANCE FOUND ECU DEFECTIVE.Jan 10, 2004 · N59806 · Bell 214ST · Fuel Control/Turbine EnginesSDR HEEA092091Ecu · malfunctionedAFTER TAKEOFF TORQUE GUAGES FLUCTUATED. RETURNED TO BASE.Jan 9, 2004 · N59806 · Bell 214ST · Fuel Control/Turbine EnginesSDR HEEA092092Coupling · shearedOIL COOLER BLOWER LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE FOUND UNION ON UTILITY HYDRAULIC PUMP SHEARED CAUSING THE LOSS OF HYDRAULIC FLUID.Jan 8, 2004 · N59806 · Bell 214ST · Hydraulic Pump (Electric/Engine), MainSDR HEEA092083Coupler · brokenENROUTE THE OIL COOLER CAUTION LIGHT ILLUMINATED. MAINTENANCE FOUND A UNION BROKEN CAUSING THE LOSS OF ALL HYDRAULIC FLUID. REPLACED UNION AND UTILITY HYDRAULIC PUMP.Dec 31, 2003 · N59806 · Bell 214ST · Hydraulic Pump (Electric/Engine), MainSDR HEEA092090Reducer · shearedDURING FLIGHT NR 2 HYDRAULIC SYSTEM FAILED. MAINTENANCE FOUND A REDUCER SHEARED ALLOWING A LOSS OF ALL HYDRAULIC FLUID.Nov 13, 2003 · N59806 · Bell 214ST · Hydraulic System, MainSDR HEEA089035Engine · malfunctionedENROUTE FROM GB-426, AIRCRAFT LOST POWER ON NR 2 ENGINE. CONTINUED TO MCY AND PERFORMED SINGLE ENGINE LANDING.Aug 27, 2003 · N59806 · Bell 214ST · Engine (Turbine/Turboprop)SDR HEEA088923Bearing · damagedWHEN BEARING GREASED, BLACK GREASE COMES OUT.Aug 22, 2003 · N8045T · Bell 214ST · Main Rotor ControlSDR HEEA088445Adc · malfunctionedAIR DATA COMPUTER FAILED 4. STAYS ON CONSTANTLY.Jul 29, 2003 · Bell 214ST · Air Data ComputerSDR HEEA088620Battery · dischargedMASTER BATTERY DEAD.Jul 26, 2003 · N8045T · Bell 214ST · Battery/Charger SystemSDR HEEA088515Gps · malfunctionedGPS GIVES COMM FAILURE.Jul 21, 2003 · N3897N · Bell 214ST · Global Positioning SystemSDR HEEA088502Battery · dischargedMASTER BATTERY WILL NOT HOLD A CHARGE. SENT TO UNITED BATTERIES FOR INSPECTION AND REPAIR.Jul 15, 2003 · N5748M · Bell 214ST · Battery/Charger SystemSDR HEEA088464Starter · inoperativeSTARTER WOULD NOT ENGAGE.Jul 14, 2003 · N59806 · Bell 214ST · Engine StarterSDR HEEA088079Check Valve · inoperativeCAUSING TRANSFER LIGHT TO STAY ON.Jul 10, 2003 · Bell 214ST · Aircraft Fuel Distribution SystemSDR HEEA088465Starter Gen · malfunctionedSTARTER GENERATOR KICKS OFF LINE.Jul 9, 2003 · N59806 · Bell 214ST · DC Generator-AlternatorSDR HEEA088050Amplifier · malfunctionedSCAS AMPLIFIER KICKS OFF LINE.Jul 8, 2003 · Bell 214ST · Speed-Attitude Correction SystemSDR ALGA087947Starter · brokenREPAIR DUE TO THE STARTER WOULD NOT ENGAGE.Jul 4, 2003 · N390AL · Bell 214ST · Engine StarterSDR HEEA088029Actuator · malfunctionedCAUSING SCAS ROLL TO DISENGAGE.Jul 2, 2003 · N3897N · Bell 214ST · Autopilot Main ServoSDR HEEA088075Battery · weakBATTERY WEAK.Jul 1, 2003 · N8045T · Bell 214ST · Battery/Charger SystemSDR HEEA088074Battery · weakBATTERY WEAK.Jul 1, 2003 · N8045T · Bell 214ST · Battery/Charger SystemSDR HEEA088060Starter · malfunctionedSTARTER KICKS OFF DURING START.Jul 1, 2003 · N8045T · Bell 214ST · Engine Starter
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