N5447C
Service difficulty reports · 19
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 = 'N5447C' 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.
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 = 'N5447C' AND registry_match = 'registration' 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 AC2R47C05212011Fitting · brokenON WALK AROUND PRIOR TO TAKING OFF, THE HERC 201 (MP42) PILOT NOTICED THE RT MLG COWLING HANGING, UPON FUTHER INSPECTION REALIZED THE FWD HINGE HAD CRACKED. REPLACED GEAR DOOR WITH SERVICEABLE UNIT.SDR AC2A20101218001Warning Light · illuminatedMAIN TRANSMISSION CHIP LIGHT ILLUMINATED INBOUND TO VENICE. NO SECONDARY INDICATIONS NOTED.SDR AC2R20101214001Gearbox · making metal(AC2R) APPROX 2 MILES FROM LANDING, THE MAIN GEARBOX CHIP LIGHT ILLUMINATED. PERFORMED THE MAIN GEARBOX CAUTION LIGHT ILLUMINATED EMERGENCY PROCEDURE AND LANDED. MX FOUND 1 FLAKE ON PLUG, PERFORMED A SERVICEABILITY CHECK AND RETURNED ACFT TO SERVICE. RECHECKSDR AC2A685KWarning Light · illuminatedNR 2 ENGINE CHIP LIGHT ILLUMINATED INBD TO BASE. FOLLOWED EMERGENCY PROCEDURES CHECKLIST, PLACED NR 2 ENGINE LEVER TO IDLE AND LANDED AS SOON AS PRACTICAL. ENGINE LEVER PLACED TO FLIGHT FOR LANDING AND RETURNED TO IDLE AFTER LANDING.SDR AC2A119194Bolt · corrodedNEW BOLTS HAVE A PIT IN THE SHANK OFF THE BOLT.SDR AC2A113672Coupling · crackedCOUPLING WAS FOUND CRACKED ON 110 HR, AIRFRAME INSPECTION.SDR AC2A110338Flex Coupling · crackedDISCOVERED CRACKED COUPLING DURING 50 HOUR INSPECTION. INSTALLED NEW COUPLING.SDR AC2A087919Latch · brokenRT FWD ENGINE COWL LATCH FAILED IN FLIGHT. UPON LANDING IT WAS DISCOVERED THAT THE COWLING HAD LIFTED 2 INCHES ON RIGHT HAND SIDE. THE LATCH HOOK ON THE FWD. LATCH WAS COMPLETELY MISSING AND THE AFT LATCH WAS CLOSED BUT NOT HOOKED TO THE AIRFRAME FITTING. FWD.SDR AC2A081172Seal · leakingENGINE STARTED LEAKING OIL AFTER OIL FLOW CHECK. REPLACED SEALSDR AC2A0000064Control Cable · damagedAFTER LANDING ON SS169C, MOVED ENGINE THROTTLES TO GROUND IDLE WHILE LOADING AND UNLOADING PASSENGERS. WHEN THROTTLES MOVED BACK TO FLY, NR 2 THROTTLE MADE A NOTICEABLE CLICK AT THE FULL OPEN POSITION AND TRAVEL FURTHER FORWARD IN THE QUADRANT. PULLED THROTTSDR AC2A0000056Meter · corrodedPART IS ERODED AT THE METER SET CAUSING STREAKING AND VOIDS IN THE SPRAY PATTERN. REPLACED THE METER SET. (X)SDR AC2A0000045Pinion Gear · spalledENGINE REMOVED FOR METAL IN OIL. UPON DISASSEMBLY OF GEARBOX, HELICAL POWER TRAIN PINION GEAR PN 6893672 WAS FOUND TO HAVE SPALLING ON GEAR TEETH. HELICAL TORQUEMETER GEAR ALSO HAD SPALLING ON GEAR TEETH. BOTH PARTS WERE REJECTED DUE TO SPALLING. PINION GESDR AC2A0000044Scroll · damagedENGINE WOULD NOT PASS LIMITING CHECK AS OUTLINED IN SIKORSKY S76 FLIGHT MANUAL. ENG ALSO REPORTED FOR LOW POWER. ENG REMOVED. UPON DISASSEMBLY OF TURBINE, 1ST STAGE TURBINE NOZZLE AND 1ST STAGE TURBINE WHEEL WERE FOUND DAMAGED FROM FOREIGN OBJECT PASSING THSDR AC2A0000063Fire Detector · malfunctionedAIRCRAFT DEPARTED ICY ON 135 SERVICE FLIGHT AND APPROX 10 MILES SOUTH OF ICY, NR 2 ENGINE FIRE LIGHT ILLUMINATED AND FIRE WARNING HORN SOUNDED. CANCELLED TONE AND IN ABSENCE OF ANY SECONDARY INDICATIONS, RETURNED TO HELIPORT AND MADE A NORMAL APPROACH. MECHASDR AC2A0000041Turbine Wheel · damagedACFT''''''''S NR 2 ENG HAD A CHIP LIGHT AFTER LANDING. CHIP PLUGS REMOVED, ENG FOUND MAKING METAL. METAL CLEARED FROM PLUGS, ENG RUN. CHIP LIGHT AGAIN CAME ON. PLUGS CLEANED, ENG RE-STARTED. BEFORE ENG REACHED IDLE RPM, CHIP LIGHT CAME ON. MECH REPORTED SDR 99ZZZX4439Potentiometer · failedFEEDBACK POT PREMATURE FAILURE. SUBMITTER STATED SHOULD LAST UNTIL OVERHAUL TIME OF 3,000 HOURS. CAUSED ACTUATOR TO KICK IN-FLIGHT. COMPONENT PN 7690002802106.SDR 97ZZZX2859Switch · shortedFLOAT INFLATED PREMATURELY. FOUND SWITCH ROTATING IN CYCLIC, LOOSE INSTALLATION, WIRE FRAYED. NO SHIELDING OVER SOLDER JOINT, CAUSING SHORT. UNSOLDERED CONNECTION, INSTALLED SHIELDING OVER WIRES, RESOLDERED, AND INSTALLED SWITCH SECURELY TO PREVENT TURNING.SDR 97ZZZX2856Explosive Link · failedEXPLOSIVE LINK DID NOT ACTIVATE WHEN FLOATS WERE DEPLOYED. HARNESS TEST OK. REPLACED LINK.SDR 97ZZZX97Nozzle Shield · damagedTHE NR 2 ENGINE FIRST STAGE TURBINE NOZZLE SHIELD WAS FOUND TO HAVE AN .8750 INCH BY 1.75 INCH SECTION MISSING AT THE 6 O'CLOCK POSITION. THIS DEFECT WAS FOUND DURING A ROUTINE INSPECTION. IT WAS SEEN THROUGH THE FUEL NOZZLE MOUNTING HOLE. AFTER REMOVAL OF
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