N430CM

Service difficulty reports · 30

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N430CM' AND registry_match = 'registration'
  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 AC2A20130709001Line · failedWHILE IN A HOVER, DURING A TRACK AND BALANCE FLIGHT THE NR 1 HYD SYSTEM FAILED. INDICATED BY A MASTER CAUTION LIGHT AND LOSS OF NR 1 SYSTEM HYD PSI AND THE PEDALS GOT STIFF. PERFORMED LANDING AND CHECKED HYD PSI AND SHUT THE NR 1 SYSTEM OFF IAW THE EMERGENCYJul 3, 2013 · N430CM · Bell 430 · Hydraulic System, MainSDR AC2A0CM01312011Window · damagedBIRD STRIKE ABOVE LT WINDOW.Jan 30, 2011 · N430CM · Bell 430 · Flight Compartment WindowsSDR AC2A0CM01242011Fadec · failedNR1 M/ECU LIGHT ILLUMINATED IN FLIGHT ALONG WITH ECU INDICATION ABOVE NR1 ENGINE INDICATOR. FADEC ON NR 1 ENGINE FAILED.Jan 24, 2011 · N430CM · Bell 430 · Fuselage Miscellaneous StructureSDR AC2A2008102278763Volt Regulator · inoperativeAFTER RESETTING THE NR 2 GENERATOR FOR 3 TIMES IT WAS DETERMINED THAT THE VOLTAGE REGULATOR WAS THE PROBLEM.Oct 22, 2008 · N430CM · Bell 430 · DC RegulatorSDR AC2A119193Pin · debondedPIN DEBONDED.Mar 14, 2008 · N430CM · Bell 430 · Main Rotor SystemSDR AC2A114171Bearing · crackedBEARINGS SCUFFING AND CRACKEDJan 27, 2007 · N430CM · Bell 430 · Tail Rotor BladesSDR AC2A114169Restraint · wornWORN DUE TO SHEAR RESTRAINT BEING WORNJan 27, 2007 · N430CM · Bell 430 · Main Rotor SystemSDR AC2A114168Restraint · wornWORN ELASTAMERJan 27, 2007 · N430CM · Bell 430 · Main Rotor SystemSDR AC2A113419Sensor · malfunctionedNR 1 ENGINE NP2 RPM PICKUP MALFUNCTIONED/FAILED. INSTALLED SERVICABLE PART.Jan 3, 2007 · N430CM · Bell 430 · Engine RPM Indicating SystemSDR AC2A113281Transmitter · failedSHORTLY AFTER TAKING OFF FROM ST37 I EXPERIENCED A NR 2 ECU FAILURE TO THE HIGH SIDE. FOLLOWED THE EMERGENCY CHECKLIST BY GOING TO MANUAL CONTROL OF NR 2 ENGINE AND RETURNED TO BASE WITHOUT FURTHER INCIDENT. THE MECHANICS DETERMINED THAT THE NR 2 ENGINE TORQUDec 18, 2006 · N430CM · Bell 430 · Engine BMEP/Torque IndicatingSDR AC2A110312Tail Boom · crackedTAILBOOM CRACK UNDER NR 2 HANGAR BEARING MOUNT. BEARING MOUNT PULLED LOOSE. FOUND DURING ROUTINE PHASE INSPECTION.Jul 19, 2006 · N430CM · Bell 430 · Rotorcraft Tail BoomSDR AC2A100900Strobe · burned outONE ROW OF LEDS BURNED OUT / REPLACED LIGHT ASSY.May 8, 2005 · N430CM · Bell 430 · Exterior LightingSDR AC2A100892Pin · debondedPIN DEBONDED/ REPLACED RESTRAINT.May 3, 2005 · N430CM · Bell 430 · Main Rotor HeadSDR AC2A100893Pin · debondedPIN DEBONDED/ REPLACED RESTRAINT.May 3, 2005 · N430CM · Bell 430 · Main Rotor HeadSDR AC2A100762Battery · weakBATTERY IS WEAK. CHARGED BATTERY AND PERFORMED CAPACITY CHECK. FAILED 1ST CHECK (23 MINUTES). PERFORMED CONDITIONING CHARGE, RESTED AND PERFORMED 2ND CHECK. FAILED 2ND CHECK (30 MINUTES). WORK PERFORMED IAW MFG BATTERY MANUALS. REPLACED BATTERY.Mar 19, 2005 · N430CM · Bell 430 · Battery/Charger SystemSDR AC2A093681Trim Tab · crackedTRIM TAB ON MAIN ROTOR BLADE IS CRACKED. REPLACED TRIM TAB.Mar 6, 2004 · N430CM · Bell 430 · Main Rotor BladesSDR AC2A093680Stud · crackedSTUD IS CRACKED WHERE THREADS ATTACHES TO FLANGE. REPLACED STUD ASSEMBLY.Mar 6, 2004 · N430CM · Bell 430 · Main Rotor ControlSDR AC2A092346Stud · crackedCRACKED WHERE THREADED PORTION TRANSITIONS TO FLANGED PART. REPLACED PART.Jan 22, 2004 · N430CM · Bell 430 · Main Rotor HeadSDR AC2A092342Stud · cracked4 DOWN STOP STUDS CRACKEDJan 18, 2004 · N430CM · Bell 430 · Main Rotor HeadSDR 2003F00639Chip Detector · failedC/FL (CHIP DETECTOR FAILURE) LIGHTS INTERMITTENT.Oct 16, 2003 · N430CM · Bell 430 · Main Rotor Indicating SystemSDR AC2A093328Chip Detector · shortedCHIP DETECTOR CIRCUIT-SHORTED. DETECTOR CAUSES PLANETARY LIGHT TO STAY ILLUMINATED. REPLACED PART.Jul 26, 2003 · N430CM · Bell 430 · Main Rotor Indicating SystemSDR AC2A086760Display · malfunctionedFOUND CIRCUIT BREAKER POPPED FOR EFIS UNIT. WOULD NOT RESET. REPLACED EFIS UNIT WITH NEW.May 21, 2003 · N430CM · Bell 430 · Integrated Flight SystemSDR AC2A086462Cam Follower · brokenCAM FOLLOWER IS BROKEN. BEARINGS BECOME CORRODED AND THE OUTER RACE SEPARATES FROM THE INNER RACE. DAMAGE WAS FOUND ON THE LEADING EDGE OF ONE TAIL ROTOR BLADE ON THIS AIRCRAFT, THE PREVIOUS DAY. IT IS SUSPECTED THAT THE BEARING OUTER RACE BECAME DISCONNECTMay 13, 2003 · N430CM · Bell 430 · Passenger/Crew DoorsSDR AC2A086459Impeller · brokenCORNER OF IMPELLER BLADE IS BROKEN OFF. BROKEN AREA MEARURES 1/4 X 1/2 INCH. BROKE IMPELLER PIECE WAS FOUND IN THE TURBINE. REMOVED ENGINE FROM AIRCRAFT AND REPLACED IMPELLER.May 9, 2003 · N430CM · Bell 430 · Turbine Engine Compressor SectionSDR AC2A086262Connector · damagedTRANSMISSION SUMP CHIP LITE WOULD NOT PULSE. CLEANED MOISTURE FROM SUMP CONNECTOR PLUG. AIRCRAFT GROUND RUN O.K.Apr 9, 2003 · N430CM · Bell 430 · Main Rotor GearboxSDR AC2A084143Link · wornTAIL ROTOR PITCH CONTROL LINKS ARE WORN. REPLACED TAIL ROTOR PITCH CONTROL LINKS.Jan 30, 2003 · N430CM · Bell 430 · Tail Rotor HeadSDR AC2A084073Cylinder · defectiveROTOR BRAKE CYLINDER WEAK AT TIMES. REPLACED ROTOR BRAKE CYLINDER.Jan 28, 2003 · N430CM · Bell 430 · Main Rotor BrakeSDR AC2A082962Lens · crackedTAILBOOM STROBE LENS IS CRACKED. REPLACED LENS.Dec 22, 2002 · N430CM · Bell 430 · Exterior LightingSDR AC2A082960Lens · crackedTAILBOOM STOBE LENS IS CRACKED. THIS LENS HAD 10 (TEN) HOURS TOTAL TIME. REPLACED LENS.Dec 18, 2002 · N430CM · Bell 430 · Exterior LightingSDR AC2A081090Solenoid · defectiveSOLENOID IS DEFECTIVE. SNAP RING ON SHAFT UNDER THE SPRING DOES NOT STAY IN GROOVE. REPLACED SOLENOID.Apr 1, 2002 · N430CM · Bell 430 · Fuel Controlling System
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