N430CT, cancelled Dec 31, 2022

Service difficulty reports · 49

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 = 'N430CT' AND deregistration_id = 'N430CT-2022-12-31'
  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 AC2R0CT03062011Shaft · crackedOUTER SHAFT FOUND CRACKED AT TT 259.0 AT DISASSEMBLY. ENGINE WAS REMOVED FOR SMOKING ON SHUTDOWN AND VXP INDICATED VIBRATIONS TRENDING UP. RAN ON TEST CELL AND ABORTED RUN DUE TO EXCESSIVE VIBRATIONS NOTED IN ENGINE'S COMPRESSOR AND DID FIND SMOKING ON SHUTDMar 6, 2011 · N430CT · Bell 430 · Turbine SectionSDR AC2A2009060782115Bearing · wornDURING AN OVERSPEED INSP ON THE DRIVE TRAIN, WE FOUND THE NR2 HANGER BEARING ON THE TAILROTOR DRIVESHAFT HAD EXCESSIVE RADIAL PLAY. REPLACED THE HANGER BRG.Jun 7, 2009 · N430CT · Bell 430 · Tail Rotor Drive ShaftSDR AC2A2009053181959Pickup · malfunctionedENROUTE, YELLOW M/ECU2 INDICATOR, WHITE ECU INDICATOR ABOVE THE NR 2 ENGINE TQ AND NP INDICATION FLUCTUATED FOR ABOUT FIVE MINUTES BEFORE IT RETURNED TO NORMAL INDICATION. ALTERED ROUTE FOR A DIRECT FLIGHT. SHUT DOWN ACFT AT HELIPORT AND NOTIFIED MX. REPLMay 31, 2009 · N430CT · Bell 430 · Bleed Air Indicating SystemSDR AC2A2009050381739Warning Light · illuminatedFLYING FROM THE HERCULES 120 TO 299B AND THE NR1 M/ECU CAUTION LIGHT ILLUMINATED IN FLIGHT, RETURNED TO DEPARTURE AND SHUTDOWN.May 3, 2009 · N430CT · Bell 430 · Central WarningSDR AC2A2009042481568Ecu · faultyIN FLIGHT, YELLOW M/ECU2 LIGHT ILLUMINATED, FOLLOWED BY A WHITE ECU LIGHT ABOVE THE NR2 ENGINE TORQUE. RETARDING THE THROTTLE TO IDLE HAD NO EFFECT ON THE NR2 NP. TO REDUCE THE NR2 NP TO IDLE, THE ECU HAD TO BE PUT INTO MANUAL.Apr 24, 2009 · N430CT · Bell 430 · Fuel Control/Turbine EnginesSDR AC2A2009031181030Warning Message · illuminatedTAKING OFF FROM SP 77A TO WD 109 AND THE 1 M/ECU 2 LIGHT ILLUMINATED ALONG WITH THE ECU LIGHT ABOVE THE NR 1 TORQUE AND THE FADEC HORN. WENT TO THE MANUAL MODE ON THE NR 1 AND RETURNED TO DEPARTURE, LANDED AND SHUTDOWN.Mar 11, 2009 · N430CT · Bell 430 · Engine Indicating SystemSDR AC2A2009031081018Warning Message · illuminatedLANDED AT 0945 WHEN THE 1 M/ECU 2 LIGHT ILLUMINATED IN FLIGHT. MX CAME OUT TO THE ACFT & CLEARED THE FAULT WITH COMPUTER. TOOK OFF AT 1025 AND 5 MINUTES INTO THE FLIGHT THE M/ECU 2 LIGHT ILLUMINATED & THEN IT ILLUMINATED WITH THE 1 M/ECU 2. TURNED AROUND, BACMar 10, 2009 · N430CT · Bell 430 · Engine Indicating SystemSDR AC2A2008080377650Warning Message · false activationDURING THE RETURN FLIGHT FROM, EXPERIENCED A ECU (FADEC) FAILURE ON THE NR 2 ENGINE. IAW THE EMERGENCY PROCEDURES, REDUCED THE THROTTLE ON THE NR 2 ENGINE AND SWITCHED TO MANUAL CONTROL. PILOT NOTIFIED DEPARTURE APT OF THE PROBLEM AND EXECUTED AN UNEVENTFUL LAug 3, 2008 · N430CT · Bell 430 · Central WarningSDR AC2A119271Warning Light · illuminatedNR 2 ENGINE CHIP SUMP LIGHT ILLUMINATED IN FLIGHT. FOLLOWED EMERGENCY CHECKLIST AND LANDED. REMOVED CHIP PLUGS, CLEANED AND PERFORMED PENALTY RUN. FOUND SERVICEABLE.Mar 17, 2008 · N430CT · Bell 430 · Powerplant SystemSDR AC2A118979Stop · crackedSTOP CRACKED IN RADIUS.Mar 2, 2008 · N430CT · Bell 430 · Main Rotor SystemSDR 497Transducer · inoperativeAIRCRAFT TRANSMISSION OIL PRESSURE ON INTEGRATED INSTRUMENT DISPLAY SYSTEM (IIDS) DECREASING. MADE TURN TO COME BACK TO INTRACOASTAL CITY. EMERGENCY CHECKLIST PULLED OUT AND FOLLOWED. INDICATED PRESSURE WENT DOWN INTO THE RED. LANDING AREA FOUND, AND LANDEJan 21, 2008 · N430CT · Bell 430 · Main Rotor GearboxSDR 495Magnetic Seal · leakingNOTICED FLUCTUATING ENGINE OIL PRESSURE ON NR 2 ENGINE. PULLED OUT AIRCRAFT EMERGENCY PROCEDURE CHECKLIST. FOLLOWED EMERGENCY PROCEDURE. OIL PRESSURE DECREASED BELOW 52.5± 2.5 PSI. SECURED NR 2 ENGINE. COMPLETED RUN ON LANDING ON THE GRASS STRIP AT INTRACJan 20, 2008 · N430CT · Bell 430 · Turbine Engine Oil SystemSDR AC2A113718Tail Rotor · will not balanceTHIS BLADE WAS HEAVY, COULD NOT BALANCE ON AIRCRAFT. MARVEL AND IT TOOK 52.26 GRAMS SPANWISE TO BRING IT IN. INSPECTION REVEALED OPENING AT TRAILING EDGE BY WEIGHTS AND PITCH HORN MOUNTING POINT, ALSO CORROSION ON OUTER BEARING BOSS.Jan 16, 2007 · N430CT · Bell 430 · Tail Rotor BladesSDR AC2A109597Attach Fitting · crackedDURING TAILROTOR GEARBOX RETORQUE, MECHANIC SAW A CRACK ON THE TAIL ROTOR GEARBOX MOUNTING ATTACHMENT FITTING AT THE 6 O'CLOCK POSITION. PART WILL BE REPLACED.Jun 8, 2006 · N430CT · Bell 430 · Rotorcraft Tail BoomSDR AC2A109138Yoke · crackedFOUND CRACKS IN YOKE /REPLACED YOKE AND SENT CRACKED ONE TO MFG FOR EVALUATION.Apr 8, 2006 · N430CT · Bell 430 · Main Rotor HeadSDR AC2A108635Stud · crackedFOUND STUDS CRACKED DURING INSPECTION, AT BASE OF THREADED PORTION./ REPLACED STUDS.Apr 5, 2006 · N430CT · Bell 430 · Main Rotor SystemSDR AC2R099710Battery · failedPART FAILED TEST TWO CHARGE AND CAPACITY CHECKS. REPLACED BATTERY AND BOOSTED GENERATOR OUTPUT TO 28.5.Oct 30, 2004 · N430CT · Bell 430 · Battery/Charger SystemSDR AC2A097170Housing · deterioratedPART HOUSING IS DETERIORATED. ORDERED REPLACEMENT PART.Aug 22, 2004 · N430CT · Bell 430 · Emergency LightingSDR AC2A097166Sun Gear · damagedSUN GEAR WORN BEYOND LIMIT AT 3000 HOUR INSPECTION. METAL TRANSFERRED TO SHAFT. REPLACED SUN GEAR. REQUEST WARRANTY.Aug 18, 2004 · N430CT · Bell 430 · Main Rotor GearboxSDR AC2A097165Shaft · damagedMETAL TRANSFER FROM SUN GEAR. REPLACED SHAFT. REQUEST WARRANTY.Aug 18, 2004 · N430CT · Bell 430 · Main Rotor GearboxSDR AC2A097164Stud · crackedPART IS CRACKED WHERE THREADED AREA ATTACHES TO FLANGE. REPLACED STUD ASSEMBLY.Apr 4, 2004 · N430CT · Bell 430 · Main Rotor HeadSDR AC2A093329Restraint · debondedRESTRAINT DISBONDED. SHEAR RESTRAINT DISBONDED AT PIN. REPLACED RESTRAINT.Feb 17, 2004 · N430CT · Bell 430 · Main Rotor HeadSDR AC2A093330Altimeter · malfunctionedALTIMETER MALFUNCTIONED. 60 FT LOW ON CERTIFICATION CHECK. REPLACEDFeb 17, 2004 · N430CT · Bell 430 · Altimeter, Barometric/EncoderSDR AC2A086763Module · galledHYDRAULIC MODULE FILTER HOUSING THREADS GALLED ON THE RETURN SIDE. REPLACED HYDRAULIC MODULE ASSEMBLY.May 24, 2003 · N430CT · Bell 430 · Hydraulic System, MainSDR AC2A086762Line · failedNR 1 HYDRAULIC SYSTEM PRESSURE LINE FAILURE. REMOVED AND REPLACED LINE , PUMP, FILTERS.May 22, 2003 · N430CT · Bell 430 · Hydraulic System, MainSDR AC2A086464Turbine · roughCOOLING TURBINE IS ROUGH. COOLING TURBINE FAILED. REPLACED TURBINE WITH SERVICABLE TURBINE.May 18, 2003 · N430CT · Bell 430 · Cabin Cooling SystemSDR AC2A086267Light · defectivePART IS DEFECTIVE. LANDING LIGHT WILL NOT ILLUMINATE. CHANGING BULB DID NOT SOLVE PROBLEM. LIGHT ASSEMBLY WAS REPLACED.Apr 17, 2003 · N430CT · Bell 430 · Exterior LightingSDR AC2A086260Transmitter · false indicationAFTER FLIGHT IN RAIN, NR 2 HYDRAULIC PRESSURE INCREASED TO 1760 PSI AND NR 2 HYDRAULIC TEMPERATURE INCREASED TO 44 DEGREES C. CLEANED WATER FROM NR 2 HYDRAULIC PRESSURE TRANSMITTER CONNECTOR PLUG.Apr 9, 2003 · N430CT · Bell 430 · Hydraulic Indicating SystemSDR AC2A084874Probe · loosePROBE IS LOOSE. REPLACED PARTMar 2, 2003 · N430CT · Bell 430 · Outside Air Temperature Indicator/SensorSDR AC2A084873Strap · debondedFOUND RUBBER SUPPORT DISBONDED ON MLG DURING INSPECTION. REPLACED STRAP ASSEMBLIES.Mar 2, 2003 · N430CT · Bell 430 · Main Landing GearSDR AC2A084871Skin · chafedCABIN ROOF RT SIDE, HAD CHAFED SPOT FROM COWLING THROUGH HONEYCOMB PANEL STATION 210, WL 87. THE COWLING WAS POORLY FITTED TO THE AIRCRAFT, DURING THE MANUFACTURING PROCESS. THE CABIN ROOF HAD TO BE PATCHED AND THE BOTTOM EDGE OF COWLING HAD TO BE TRIMMED.Feb 25, 2003 · N430CT · Bell 430 · Fuselage Main, Plate/SkinSDR AC2A084870Sleeve · wornSLEEVE IS WORN THRU LINER. REPLACED WITH NEW PART.Feb 24, 2003 · N430CT · Bell 430 · Tail Rotor HeadSDR AC2A084869Sleeve · delaminatedLINER CAME UNBONDED FROM SLEEVE. REPLACED WITH NEW PART.Feb 24, 2003 · N430CT · Bell 430 · Tail Rotor HeadSDR AC2A084868Bearing · roughTAIL ROTOR BEARING IS ROUGH. REPALCED BEARING.Feb 24, 2003 · N430CT · Bell 430 · Tail Rotor SystemSDR AC2A084867Sleeve · wornSLEEVE IS WORN THROUGH THE LINER. REPLACED WITH NEW PART.Feb 24, 2003 · N430CT · Bell 430 · Tail Rotor HeadSDR AC2A084866Cone Set · groovedTAIL ROTOR CONE SET WAS GROOVED. REPLACED CONE SET.Feb 24, 2003 · N430CT · Bell 430 · Tail Rotor HeadSDR AC2A084865Bearing Race · wornGROOVES WORN INTO BUSHING. REPLACED WITH NEW BUSHING.Feb 24, 2003 · N430CT · Bell 430 · Tail Rotor HeadSDR AC2A084864Bearing · wornTAIL ROTOR BEARINGS ARE WORN. REPLACED WITH NEW BEARINGS.Feb 24, 2003 · N430CT · Bell 430 · Tail Rotor BladesSDR AC2A084863Lock Plate · damagedLOCK PLATE HAD TO BE REPLACED WHEN TAILROTOR WAS REMOVED FOR PROBLEM OF A WORN, RUSTED TRUNNION, AND CRACKED SPLINE ON TAIL GEARBOX OUTPUT SHAFT. REPLACED LOCKPLATE ASSEMBLY.Feb 24, 2003 · N430CT · Bell 430 · Tail Rotor SystemSDR AC2A084862Tube · chafedFUEL TUBE HAS A GROOVE ON THE EXTERNAL SIDE OF THE FLARE. REPLACED WITH NEW TUBE ASSEMBLY.Feb 24, 2003 · N430CT · Bell 430 · Aircraft Fuel Distribution SystemSDR AC2A084860Trunnion · corrodedSPLINES ON INNER SURFACE ARE RUSTED AND PITTED. THIS TRUNNION WAS ATTACHED TO TAIL GEARBOX SN A782 WHICH ALSO HAD A CRACKED SPLINE. REPLACED TRUNNION ASSEMBLY.Feb 21, 2003 · N430CT · Bell 430 · Tail Rotor HeadSDR AC2A084859Gearbox · crackedOUTPUT SHAFT SPLINES ARE RUSTED, WORN AND ONE SPLINE IS CRACKED TOWARDS INBOARD SIDE. THIS IS THE FIRST TIME THE TAIL ROTOR ASSEMBLY WAS REMOVED SINCE RECEIVING THE AIRCRAFT NEW FROM BELL HELICOPTER. REPLACE GEARBOX ASSEMBLY WITH EXCHANGE UNIT.Feb 21, 2003 · N430CT · Bell 430 · Tail Rotor GearboxSDR AC2A084148Crosstube · corrodedCROSSTUBE IS CORRODED. CROSSTUBE WAS REPLACEDFeb 10, 2003 · N430CT · Bell 430 · Main Landing Gear Strut/Axle/TruckSDR AC2A082965Contactor · defectiveSTARTER ENGAGES WHEN BATTERY IS TURNED ON. REPLACED CONTACTOR.Jan 9, 2003 · N430CT · Bell 430 · Starter-GeneratorSDR AC2A092340Gyro · malfunctionedIN CRUISE FLIGHT WITH NR 1 AUTOPILOT ENGAGED THE AIRCRAFT EXPERIENCED AN UNCOMMANDED RIGHT HAND DESCENDING TURN. VERTICAL GYRO REPLACED.Jan 6, 2003 · N430CT · Bell 430 · Autopilot SystemSDR AC2A082144Contactor · malfunctionedAFTER BEING ENGAGED, THE START CONTACTOR WOULD ONLY DISENGAGE BY TURNING BATTERY SWITCH OFF. REPLACED PART.Dec 17, 2002 · N430CT · Bell 430 · Engine Starting System WiringSDR AC2A082140Power Supply · malfunctionedPOWER SUPPLY WILL NOT CHARGE BATTERIES. REPLACED POWER SUPPLY.Dec 10, 2002 · N430CT · Bell 430 · Emergency LightingSDR AC2A0000345Connector · inoperativeREMOVED AND REPLACED CONNECTOR.Mar 19, 2002 · N430CT · Bell 430 · Flight Control System WiringSDR AC2A0000344Connector · brokenCONNECTOR P16, PIN (G) LOCK BROKEN. REPACED CONNECTOR AND IT CORRECTED PROBLEM.Mar 19, 2002 · N430CT · Bell 430 · Electrical Power System Wiring
Back to N430CT, cancelled Dec 31, 2022