Bell 212

Service difficulty reports · 1,185

Newest first. General aviation reporting is voluntary.

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.

SDR HEEA060131Valve · malfunctionedUNCOMMANDED FLOAT INFLATION. AT TIME OF INFLATION, AIRCRAFT HAD BEEN SHUT DOWN FOR TWO HOURS, THE BATTERIES WERE OFF, THE MANUAL INFLATION HANDLE WAS IN THE DOWN AND SAFTIED POSITION. INSPECTED AIRCRAFT INFLATION RIGGING, FOUND OK. ELECTRICAL SQUIB HAD NOT Jan 21, 1999 · N5736D · Bell 212 · Emergency Flotation SectionSDR HEEA060130Cartridge · damagedFUEL CARTRIDGE UNIT MISSING INLET SCREEN AND UMBRELLA CHECK VALVE.Jan 21, 1999 · Bell 212 · Fuel Boost PumpSDR HEEA060129Indicator · reads highITT INDICATOR READS 125 DEGREES HIGH.Jan 21, 1999 · N102PH · Bell 212 · Indicating/Recording SystemSDR HEEA060128Valve · crackedLOWER FITTING CRACKED ON VALVE.Jan 21, 1999 · N3208H · Bell 212 · Hydraulic System, MainSDR HEEA060127Indicator · stickingTORQUE METER INDICATOR'S NR 1 NEEDLE STICKS.Jan 21, 1999 · N5010F · Bell 212 · Engine BMEP/Torque IndicatingSDR HEEA060126Bearing · damagedBALLS BREAKING DOWN. REPLACED WITH SERVICEABLE BEARINGS.Jan 21, 1999 · N3131S · Bell 212 · Main Rotor Mast/SwashplateSDR HEEA060125Valve · failedMIXING VALVE NOT FUNCTIONING.Jan 21, 1999 · Bell 212 · Heating SystemSDR HEEA060124Pump · malfunctionedLOW FUEL PRESSURE.Jan 21, 1999 · N1079U · Bell 212 · Fuel Boost PumpSDR HEEA060081Engine · overtempITT ABOVE 900 DEGREES FOR OVER 40 SECONDS.Jan 21, 1999 · N1082G · Bell 212 · Engine (Turbine/Turboprop)SDR CA990129026Seal · leaking(CAN) MAIN INPUT SEAL LEAKING. REPLACED.Jan 13, 1999 · Bell 212 · Main Rotor Transmission MountSDR CA990129025Servo · sticking(CAN) SERVO STICKING DURING CONTROL INPUTS UNDER HYDRAULIC SYSTEM PRESSURE.Jan 13, 1999 · Bell 212 · Rotorcraft Servo SystemSDR CA990125004Transmission · making metal(CAN) SERVICEABLE TRANSMISSION INSTALLED AND ALTERNATE RUN-IN PROCEDURE CARRIED OUT IAW WITH BELL MM. FILTERS REMOVED AND FOUND CLEAN. TWO TEST FLIGHTS OF 0.3 AND 0.2 CARRIED OUT. DURING SECOND FLIGHT, THE TRANSMISSION CHIP WARNING LIGHT CAME ON AND AIRCRAFDec 29, 1998 · Bell 212 · Engine/Transmission CouplingSDR CA990119002Engine · malfunctioned(CAN) NR 1 ENGINE EXHIBITED HIGH ITT, CAUSING A MARGINAL POWER ASSURANCE CHECK. THE ENGINE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. PART TC: 7,225.Dec 23, 1998 · Bell 212 · Engine (Turbine/Turboprop)SDR CA981123021Brake · malfunctioned(CAN) PILOT REPORTED MAGNETIC BRAKE INOPERATIVE IN THE FORE AND AFT AXIS.Nov 6, 1998 · Bell 212 · Main Rotor BrakeSDR 98ZZZX4746Engine · failedON 10-28-98 DURING RECONNAISSANCE OF OGLNY, CA, FIRE NOTICED, RPM LOW 97 PERCENT, THEN NOTICED LARGE TORQUE SPLIT. WITH N1 ON NR 2 ENGINE AT IDLE AND ITT 900 DEGREES CELSIUS, PILOT WENT TO MANUAL THROTTLE, BUT NO RESPONSE BY ENGINE.Oct 28, 1998 · N1082G · Bell 212 · Engine (Turbine/Turboprop)SDR HEEA0016488Inverter · inoperativeINVERTER INOPERATIVE.Oct 27, 1998 · N1079U · Bell 212 · AC InverterSDR HEEA0016487Gyro · inoperativeGYRO INOPERATIVE.Oct 27, 1998 · N5010F · Bell 212 · Integrated Flight SystemSDR HEEA0016423Inverter · failedINVERTER WOULD NOT COME ON LINE AT INITIAL INSTALLATION FROM STOCK.Oct 23, 1998 · N5010F · Bell 212 · AC InverterSDR HEEA0016422Inverter · malfunctionedINVERTER TRIPS CIRCUIT BREAKER.Oct 23, 1998 · N5010F · Bell 212 · AC InverterSDR HEEA0016421Receiver · failedGPS RECEIVER WILL NOT HOLD SATELLITES.Oct 23, 1998 · N1082G · Bell 212 · Global Positioning SystemSDR HEEA0016420Flux Valve · inaccurateREADING IS OFF 80 DEGREES.Oct 23, 1998 · N5010F · Bell 212 · Directional Gyro and Indicating SystemSDR HEEA0016419Valve · incorrectCOMPASS HAS INCORRECT HEADINGS, OUTPUT UNRELIABLE.Oct 23, 1998 · N5010F · Bell 212 · Directional Gyro and Indicating SystemSDR HEEA0016418Control Unit · failedCONTROL UNIT WILL NOT COME ON LINE.Oct 23, 1998 · N5010F · Bell 212 · DC Generating SystemSDR HEEA0016417Transceiver · malfunctionedVHF TRANSCEIVER HAS STATIC, HARD TO RECEIVE.Oct 23, 1998 · N1082G · Bell 212 · VHF Communications SystemSDR HEEA0016416Control Unit · failedTORQUE CONTROL UNIT CAUSES TORQUE OSCILLATION ON NR 2 ENGINE.Oct 23, 1998 · N5736J · Bell 212 · Fuel Control/Turbine EnginesSDR HEEA0016415Trim Compensator · inaccurateTRIM COMPENSATOR ADJUSTED TO 100. WILL NOT LOWER TEMP INDICATION TO WITHIN RANGE.Oct 23, 1998 · N1079U · Bell 212 · Engine EGT/TIT Indicating SystemSDR HEEA0016414Compressor · failedNOISE COMING FROM COMPRESSOR.Oct 23, 1998 · N1082G · Bell 212 · Turbine Engine Compressor SectionSDR HEEA0016413Flux Valve · inoperativeCOMPASS IS INOPERATIVE, IT HAS ERRATIC OUTPUT.Oct 23, 1998 · N5736J · Bell 212 · Directional Gyro and Indicating SystemSDR HEEA0016412Tarsyn · failedTARSYN - PIN C OF BOTTOM CONNECTOR HAS PINS BACKING OUT OF CONNECTOR.Oct 23, 1998 · N5010F · Bell 212 · Autopilot SystemSDR HEEA0016411Tarsyn · failedTARSYN FAILS TEST 8.5 ON SST.Oct 23, 1998 · N5010F · Bell 212 · Autopilot SystemSDR HEEA0016410Generator · failedSTARTER/GENERATOR WILL NOT COME ON-LINE.Oct 23, 1998 · N1079U · Bell 212 · Starter-GeneratorSDR HEEA0016409Gyro · failedRT FLAG ON ADI NOT PULLED.Oct 23, 1998 · N5010F · Bell 212 · Attitude Gyro and Indicating SystemSDR HEEA0016408Indicator · stickingITT INDICATOR STICKS AT 580 DEGREES.Oct 23, 1998 · N5010F · Bell 212 · Engine EGT/TIT Indicating SystemSDR HEEA0016407Indicator · fluctuatingITT INDICATOR GAUGE FLUCTUATING.Oct 23, 1998 · Bell 212 · Engine EGT/TIT Indicating SystemSDR HEEA0016406Indicator · stickingN1 NEEDLE ERRATIC AND STICKS.Oct 23, 1998 · N5736J · Bell 212 · Engine BMEP/Torque IndicatingSDR HEEA0016405Altimeter · failedINDICATOR - INTERNAL FAILURE, LOOSE PARTS.Oct 23, 1998 · N5736D · Bell 212 · Altimeter, Barometric/EncoderSDR HEEA0016404Detector · malfunctionedRPM INDICATOR ACTIVATES ALARM AT RANDOM.Oct 23, 1998 · N5736J · Bell 212 · Main Rotor Indicating SystemSDR HEEA0016403Caution Panel · failedPANEL ASSY LIGHTS FLICKER INTERMITTENTLY.Oct 23, 1998 · N1082G · Bell 212 · Central WarningSDR HEEA0016402Dual Ammeter · stickingDUAL AMMETER NEEDLE STICKING.Oct 23, 1998 · N5736J · Bell 212 · DC Indicating SystemSDR HEEA0016401Indicator · malfunctionedENGINE OIL TEMPERATURE STAYS AT ZERO.Oct 23, 1998 · N5736J · Bell 212 · Engine Oil PressureSDR HEEA0016400Indicator · malfunctionedON INITIAL INSTALLATION, TEMPERATURE INDICATION PEGS TO THE HIGH SIDE WITH POWER APPLIED. REPLACED WITH A SERVICEABLE INDICATOR.Oct 23, 1998 · N102PH · Bell 212 · Engine Oil TemperatureSDR HEEA0016399Saddle Assy · crackedINBOARD SECTION OF SADDLE ASSEMBLY CRACKED. CRACK EXTENDS FORE - AFT .75 INCH, ONE INCH BELOW THE INBOARD LOWER BOLT HOLE WITH THE LOWER INBOARD BOLT HOLE BEING THE CENTER POINT. REPLACED WITH SERVICEABLE SKID TUBE ASSEMBLY.Oct 23, 1998 · N3131S · Bell 212 · Main Landing Gear Attach SectionSDR HEEA0016398Support · mismanufacturedSUPPORT MISMANUFACTURED. AREA THAT BUTTS TO CAP ANGLE NEEDS TO BE ONE INCH. SUBMITTER STATED FLAT SURFACE NOT .75 INCH.Oct 23, 1998 · Bell 212 · Fuselage Miscellaneous StructureSDR HEEA0016397Inverter · malfunctionedINVERTER HAS LOW VOLTAGE OUTPUT.Oct 23, 1998 · N1079U · Bell 212 · AC InverterSDR HEEA0016396Indicator · failedNO ADF POINTER INFO DISPLAYED.Oct 23, 1998 · N5010F · Bell 212 · Integrated Flight SystemSDR HEEA0016395Indicator · failedHYDRAULIC PRESSURE NEEDLE WILL NOT RETURN TO ZERO.Oct 23, 1998 · N5010F · Bell 212 · Hydraulic Pressure IndicatorSDR HEEA0016394Indicator · failedGS FLAG WILL NOT PULL.Oct 23, 1998 · N5010F · Bell 212 · Attitude and Direction Data SystemSDR HEEA0016393Indicator · stickingHSI INDICATOR'S TO/FROM FLAG STICKS, NR 2 BEARING POINTER RATCHETS.Oct 23, 1998 · N5010F · Bell 212 · Attitude and Direction Data SystemSDR HEEA0016392Indicator · stickingHSI INDICATOR'S COMPASS CARD STICKS.Oct 23, 1998 · N27805 · Bell 212 · Attitude and Direction Data SystemSDR HEEA0016391Transponder · failedNO CODE TRANSMITTER. NO REPLY LIGHT. NO TEST LIGHT. TIME SINCE REPAIR 0:00 HOURS.Oct 23, 1998 · N5010F · Bell 212 · ATC Transponder System
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