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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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 SHUTDSDR 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.SDR 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. REPLSDR AC2A2009050381739Warning Light · illuminatedFLYING FROM THE HERCULES 120 TO 299B AND THE NR1 M/ECU CAUTION LIGHT ILLUMINATED IN FLIGHT, RETURNED TO DEPARTURE AND SHUTDOWN.SDR 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.SDR 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.SDR 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, BACSDR 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 LSDR 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.SDR AC2A118979Stop · crackedSTOP CRACKED IN RADIUS.SDR 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 LANDESDR 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 INTRACSDR 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.SDR 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.SDR AC2A109138Yoke · crackedFOUND CRACKS IN YOKE /REPLACED YOKE AND SENT CRACKED ONE TO MFG FOR EVALUATION.SDR AC2A108635Stud · crackedFOUND STUDS CRACKED DURING INSPECTION, AT BASE OF THREADED PORTION./ REPLACED STUDS.SDR AC2R099710Battery · failedPART FAILED TEST TWO CHARGE AND CAPACITY CHECKS. REPLACED BATTERY AND BOOSTED GENERATOR OUTPUT TO 28.5.SDR AC2A097170Housing · deterioratedPART HOUSING IS DETERIORATED. ORDERED REPLACEMENT PART.SDR AC2A097166Sun Gear · damagedSUN GEAR WORN BEYOND LIMIT AT 3000 HOUR INSPECTION. METAL TRANSFERRED TO SHAFT. REPLACED SUN GEAR. REQUEST WARRANTY.SDR AC2A097165Shaft · damagedMETAL TRANSFER FROM SUN GEAR. REPLACED SHAFT. REQUEST WARRANTY.SDR AC2A097164Stud · crackedPART IS CRACKED WHERE THREADED AREA ATTACHES TO FLANGE. REPLACED STUD ASSEMBLY.SDR AC2A093329Restraint · debondedRESTRAINT DISBONDED. SHEAR RESTRAINT DISBONDED AT PIN. REPLACED RESTRAINT.SDR AC2A093330Altimeter · malfunctionedALTIMETER MALFUNCTIONED. 60 FT LOW ON CERTIFICATION CHECK. REPLACEDSDR AC2A086763Module · galledHYDRAULIC MODULE FILTER HOUSING THREADS GALLED ON THE RETURN SIDE. REPLACED HYDRAULIC MODULE ASSEMBLY.SDR AC2A086762Line · failedNR 1 HYDRAULIC SYSTEM PRESSURE LINE FAILURE. REMOVED AND REPLACED LINE , PUMP, FILTERS.SDR AC2A086464Turbine · roughCOOLING TURBINE IS ROUGH. COOLING TURBINE FAILED. REPLACED TURBINE WITH SERVICABLE TURBINE.SDR AC2A086267Light · defectivePART IS DEFECTIVE. LANDING LIGHT WILL NOT ILLUMINATE. CHANGING BULB DID NOT SOLVE PROBLEM. LIGHT ASSEMBLY WAS REPLACED.SDR 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.SDR AC2A084874Probe · loosePROBE IS LOOSE. REPLACED PARTSDR AC2A084873Strap · debondedFOUND RUBBER SUPPORT DISBONDED ON MLG DURING INSPECTION. REPLACED STRAP ASSEMBLIES.SDR 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.SDR AC2A084870Sleeve · wornSLEEVE IS WORN THRU LINER. REPLACED WITH NEW PART.SDR AC2A084869Sleeve · delaminatedLINER CAME UNBONDED FROM SLEEVE. REPLACED WITH NEW PART.SDR AC2A084868Bearing · roughTAIL ROTOR BEARING IS ROUGH. REPALCED BEARING.SDR AC2A084867Sleeve · wornSLEEVE IS WORN THROUGH THE LINER. REPLACED WITH NEW PART.SDR AC2A084866Cone Set · groovedTAIL ROTOR CONE SET WAS GROOVED. REPLACED CONE SET.SDR AC2A084865Bearing Race · wornGROOVES WORN INTO BUSHING. REPLACED WITH NEW BUSHING.SDR AC2A084864Bearing · wornTAIL ROTOR BEARINGS ARE WORN. REPLACED WITH NEW BEARINGS.SDR 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.SDR AC2A084862Tube · chafedFUEL TUBE HAS A GROOVE ON THE EXTERNAL SIDE OF THE FLARE. REPLACED WITH NEW TUBE ASSEMBLY.SDR 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.SDR 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.SDR AC2A084148Crosstube · corrodedCROSSTUBE IS CORRODED. CROSSTUBE WAS REPLACEDSDR AC2A082965Contactor · defectiveSTARTER ENGAGES WHEN BATTERY IS TURNED ON. REPLACED CONTACTOR.SDR AC2A092340Gyro · malfunctionedIN CRUISE FLIGHT WITH NR 1 AUTOPILOT ENGAGED THE AIRCRAFT EXPERIENCED AN UNCOMMANDED RIGHT HAND DESCENDING TURN. VERTICAL GYRO REPLACED.SDR AC2A082144Contactor · malfunctionedAFTER BEING ENGAGED, THE START CONTACTOR WOULD ONLY DISENGAGE BY TURNING BATTERY SWITCH OFF. REPLACED PART.SDR AC2A082140Power Supply · malfunctionedPOWER SUPPLY WILL NOT CHARGE BATTERIES. REPLACED POWER SUPPLY.SDR AC2A0000345Connector · inoperativeREMOVED AND REPLACED CONNECTOR.SDR AC2A0000344Connector · brokenCONNECTOR P16, PIN (G) LOCK BROKEN. REPACED CONNECTOR AND IT CORRECTED PROBLEM.
Back to N430CT, cancelled Dec 31, 2022