N341CA
Service difficulty reports not matched to an aircraft · 20
They name N341CA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N341CA' AND registry_match IS NULL 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 = 'N341CA' AND registry_match IS NULL 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 COMA9630103Gcu · out of adjustLEFT DC GENERATOR FAILED AND WOULD NOT RESET. ADJUSTED THE LT GENERATOR CONTROL UNIT.SDR COMA9630091Erosion Guard · separatedONE BLADE ON RT PROPELLER, LEADING EDGE EROSION GUARD IS SEPARATING. REBONDED EROSION GUARD.SDR COMA9630080Wire · chafedLEFT AC GENERATOR FAILED IN FLIGHT. REPAIRED WIRE NR XA510, XA509, XA508 AT WING FLAP INTERCONNECT AREA. WIRING WAS CHAFED AND BURNED.SDR COMA9630058Gcu · defectiveLEFT ENGINE WILL NOT START (NO ROTATION) USING CROSS GENERATOR PROCEDURE. REPLACED THE LT GENERATOR CONTROL UNIT. PART TOTAL CYCLES, 6,629.SDR COMA9630056Inlet · burnedRT ENGINE INLET HEAT FAILED. REPLACED THE LOWER INLET ASSY. PART TOTAL CYCLES, 12,972.SDR COMA9630038Anti Ice Valve · defectiveRT ENGINE INDICATED NO TORQUE DROP WHEN ANTI-ICE SELECTED ON. REPLACED THE ANTI-ICE VALVE. PART TOTAL CYCLES, 7,921.SDR COMA9531216Duct Assy · failedRT ENGINE INTAKE HEAT FAIL INDICATION AND A WHITE FLASHING GLOW VISIBLE INSIDE INTAKE. REPLACED UPPER INLET ASSY.SDR COMA9531205Controls · lack of lubeAILERONS ARE BINDING. INSPECTED AILERON SYSTEM AND NO FAULTS FOUND. LUBRICATED AILERON CENTERING CAMS AND ACFT RETURNED TO SERVICE.SDR COMA9531196Switch · defectivePITCH TRIM FUNCTION FROM COPILOTS POSITION IS INTERMITTENT. REPLACED THE COPILOTS PITCH TRIM SWITCH.SDR COMA9531155Propeller Hub · crackedDURING ULTRASONIC INSP OF HUB REAR FACE, A FLAW WAS INDICATED AT THE BOLT HOLE ADJACENT TO BLADE PORT NR 3. PROPELLER WAS DISSEMBLED, HUB (S/N CW1044) AND REMOVED FROM SERVICE.SDR COM31130Connector · defectiveRIGHT TAIL PIPE HOT LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF. ENGINE WAS SHUT DOWN AND LIGHT EVENTUALLY WENT OUT. FLIGHT RETURNED TO CVG. REPLACED WIRING CONNECTOR 162VP.SDR COM31129Hub · crackedDURING OVERHAUL INSPECTION MULTIPLE CRACK INDICATIONS WERE FOUND DURING ULTRASONIC INSPECTION (IAW SB 61-58 APPENDIX C, SCAN B) HUB S/N 110502 WAS DISASSEMBLED AND REMOVED FROM SERVICE.SDR COM31123Detector · false warnCARGO SMOKE WARNING ACTIVATED DURING TAKEOFF. REPLACED THE CARGO SMOKE DETECTOR.SDR COM31088Hot Warning · illuminatedRT TAIL PIPE HOT WARNING LIGHT CAME ON AFTER TAKEOFF. COULD NOT DUPLICATE PROBLEM. INSPECTED SYSTEM AND FOUND NO DEFECTS.SDR COM1083Prop Blade · damagedRT PROPELLER, BLADE LEADING EDGE ERROSION GUARD IS LOOSE. REPLACED PROPELLER ASSY.SDR COM31074Bolt · brokenDURING C-CHECK INSPECTION, FOUND LEFT ELEVATOR MOST INBD COUNTER WEIGHT BOLT BROKEN. REPLACED BROKEN COUNTER WEIGHT BOLT.SDR COM31068Lamp · failedRT MLG DID NOT INDICATE DOWN AND LOCKED. CYCLED LANDING GEAR AND ALL INDICATIONS NORMAL. FOUND INDICATOR LAMPS IN CONTROL HANDLE TO BE AT FAULT. REPLACED LAMPS.SDR COM31062Inner Race · spunMECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO THE WORN LIMITS. DURING VISUAL INSPECTION FOUND INNER RACE HAD SPUN. SUBASSY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS FOR REPAIR.SDR COM31026Quadrant · malfunctionedFRICTION LOCK ON CONTROLS QUADRANT IS NOT WORKING. REPLACED QUADRANT.SDR COM31008Connector · dirtyRT TAIL PIPE HOT WARNING ACTIVATED DURING CLIMB. CLEANED WIRING CONNECTION FOR TAIL PIPE HEAT SENSORS AND AIRCRAFT RETURNED TO SERVICE.
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