# Service difficulty reports: N430CM A list on [N430CM](https://openairdocs.org/aircraft/N430CM.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR AC2A20130709001](https://openairdocs.org/sdr/AC2A20130709001.md): Line · failed · Jul 3, 2013 · N430CM · Bell 430 · Hydraulic System, Main > WHILE 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 EMERGENCY - [SDR AC2A0CM01312011](https://openairdocs.org/sdr/AC2A0CM01312011.md): Window · damaged · Jan 30, 2011 · N430CM · Bell 430 · Flight Compartment Windows > BIRD STRIKE ABOVE LT WINDOW. - [SDR AC2A0CM01242011](https://openairdocs.org/sdr/AC2A0CM01242011.md): Fadec · failed · Jan 24, 2011 · N430CM · Bell 430 · Fuselage Miscellaneous Structure > NR1 M/ECU LIGHT ILLUMINATED IN FLIGHT ALONG WITH ECU INDICATION ABOVE NR1 ENGINE INDICATOR. FADEC ON NR 1 ENGINE FAILED. - [SDR AC2A2008102278763](https://openairdocs.org/sdr/AC2A2008102278763.md): Volt Regulator · inoperative · Oct 22, 2008 · N430CM · Bell 430 · DC Regulator > AFTER RESETTING THE NR 2 GENERATOR FOR 3 TIMES IT WAS DETERMINED THAT THE VOLTAGE REGULATOR WAS THE PROBLEM. - [SDR AC2A119193](https://openairdocs.org/sdr/AC2A119193.md): Pin · debonded · Mar 14, 2008 · N430CM · Bell 430 · Main Rotor System > PIN DEBONDED. - [SDR AC2A114171](https://openairdocs.org/sdr/AC2A114171.md): Bearing · cracked · Jan 27, 2007 · N430CM · Bell 430 · Tail Rotor Blades > BEARINGS SCUFFING AND CRACKED - [SDR AC2A114169](https://openairdocs.org/sdr/AC2A114169.md): Restraint · worn · Jan 27, 2007 · N430CM · Bell 430 · Main Rotor System > WORN DUE TO SHEAR RESTRAINT BEING WORN - [SDR AC2A114168](https://openairdocs.org/sdr/AC2A114168.md): Restraint · worn · Jan 27, 2007 · N430CM · Bell 430 · Main Rotor System > WORN ELASTAMER - [SDR AC2A113419](https://openairdocs.org/sdr/AC2A113419.md): Sensor · malfunctioned · Jan 3, 2007 · N430CM · Bell 430 · Engine RPM Indicating System > NR 1 ENGINE NP2 RPM PICKUP MALFUNCTIONED/FAILED. INSTALLED SERVICABLE PART. - [SDR AC2A113281](https://openairdocs.org/sdr/AC2A113281.md): Transmitter · failed · Dec 18, 2006 · N430CM · Bell 430 · Engine BMEP/Torque Indicating > SHORTLY 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 TORQU - [SDR AC2A110312](https://openairdocs.org/sdr/AC2A110312.md): Tail Boom · cracked · Jul 19, 2006 · N430CM · Bell 430 · Rotorcraft Tail Boom > TAILBOOM CRACK UNDER NR 2 HANGAR BEARING MOUNT. BEARING MOUNT PULLED LOOSE. FOUND DURING ROUTINE PHASE INSPECTION. - [SDR AC2A100900](https://openairdocs.org/sdr/AC2A100900.md): Strobe · burned out · May 8, 2005 · N430CM · Bell 430 · Exterior Lighting > ONE ROW OF LEDS BURNED OUT / REPLACED LIGHT ASSY. - [SDR AC2A100892](https://openairdocs.org/sdr/AC2A100892.md): Pin · debonded · May 3, 2005 · N430CM · Bell 430 · Main Rotor Head > PIN DEBONDED/ REPLACED RESTRAINT. - [SDR AC2A100893](https://openairdocs.org/sdr/AC2A100893.md): Pin · debonded · May 3, 2005 · N430CM · Bell 430 · Main Rotor Head > PIN DEBONDED/ REPLACED RESTRAINT. - [SDR AC2A100762](https://openairdocs.org/sdr/AC2A100762.md): Battery · weak · Mar 19, 2005 · N430CM · Bell 430 · Battery/Charger System > BATTERY 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. - [SDR AC2A093681](https://openairdocs.org/sdr/AC2A093681.md): Trim Tab · cracked · Mar 6, 2004 · N430CM · Bell 430 · Main Rotor Blades > TRIM TAB ON MAIN ROTOR BLADE IS CRACKED. REPLACED TRIM TAB. - [SDR AC2A093680](https://openairdocs.org/sdr/AC2A093680.md): Stud · cracked · Mar 6, 2004 · N430CM · Bell 430 · Main Rotor Control > STUD IS CRACKED WHERE THREADS ATTACHES TO FLANGE. REPLACED STUD ASSEMBLY. - [SDR AC2A092346](https://openairdocs.org/sdr/AC2A092346.md): Stud · cracked · Jan 22, 2004 · N430CM · Bell 430 · Main Rotor Head > CRACKED WHERE THREADED PORTION TRANSITIONS TO FLANGED PART. REPLACED PART. - [SDR AC2A092342](https://openairdocs.org/sdr/AC2A092342.md): Stud · cracked · Jan 18, 2004 · N430CM · Bell 430 · Main Rotor Head > 4 DOWN STOP STUDS CRACKED - [SDR 2003F00639](https://openairdocs.org/sdr/2003F00639.md): Chip Detector · failed · Oct 16, 2003 · N430CM · Bell 430 · Main Rotor Indicating System > C/FL (CHIP DETECTOR FAILURE) LIGHTS INTERMITTENT. - [SDR AC2A093328](https://openairdocs.org/sdr/AC2A093328.md): Chip Detector · shorted · Jul 26, 2003 · N430CM · Bell 430 · Main Rotor Indicating System > CHIP DETECTOR CIRCUIT-SHORTED. DETECTOR CAUSES PLANETARY LIGHT TO STAY ILLUMINATED. REPLACED PART. - [SDR AC2A086760](https://openairdocs.org/sdr/AC2A086760.md): Display · malfunctioned · May 21, 2003 · N430CM · Bell 430 · Integrated Flight System > FOUND CIRCUIT BREAKER POPPED FOR EFIS UNIT. WOULD NOT RESET. REPLACED EFIS UNIT WITH NEW. - [SDR AC2A086462](https://openairdocs.org/sdr/AC2A086462.md): Cam Follower · broken · May 13, 2003 · N430CM · Bell 430 · Passenger/Crew Doors > CAM 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 DISCONNECT - [SDR AC2A086459](https://openairdocs.org/sdr/AC2A086459.md): Impeller · broken · May 9, 2003 · N430CM · Bell 430 · Turbine Engine Compressor Section > CORNER 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. - [SDR AC2A086262](https://openairdocs.org/sdr/AC2A086262.md): Connector · damaged · Apr 9, 2003 · N430CM · Bell 430 · Main Rotor Gearbox > TRANSMISSION SUMP CHIP LITE WOULD NOT PULSE. CLEANED MOISTURE FROM SUMP CONNECTOR PLUG. AIRCRAFT GROUND RUN O.K. - [SDR AC2A084143](https://openairdocs.org/sdr/AC2A084143.md): Link · worn · Jan 30, 2003 · N430CM · Bell 430 · Tail Rotor Head > TAIL ROTOR PITCH CONTROL LINKS ARE WORN. REPLACED TAIL ROTOR PITCH CONTROL LINKS. - [SDR AC2A084073](https://openairdocs.org/sdr/AC2A084073.md): Cylinder · defective · Jan 28, 2003 · N430CM · Bell 430 · Main Rotor Brake > ROTOR BRAKE CYLINDER WEAK AT TIMES. REPLACED ROTOR BRAKE CYLINDER. - [SDR AC2A082962](https://openairdocs.org/sdr/AC2A082962.md): Lens · cracked · Dec 22, 2002 · N430CM · Bell 430 · Exterior Lighting > TAILBOOM STROBE LENS IS CRACKED. REPLACED LENS. - [SDR AC2A082960](https://openairdocs.org/sdr/AC2A082960.md): Lens · cracked · Dec 18, 2002 · N430CM · Bell 430 · Exterior Lighting > TAILBOOM STOBE LENS IS CRACKED. THIS LENS HAD 10 (TEN) HOURS TOTAL TIME. REPLACED LENS. - [SDR AC2A081090](https://openairdocs.org/sdr/AC2A081090.md): Solenoid · defective · Apr 1, 2002 · N430CM · Bell 430 · Fuel Controlling System > SOLENOID IS DEFECTIVE. SNAP RING ON SHAFT UNDER THE SPRING DOES NOT STAY IN GROOVE. REPLACED SOLENOID. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/aircraft/N430CM/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.