N248CA, cancelled Jan 12, 2007
Service difficulty reports · 56
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 = 'N248CA' AND deregistration_id = 'N248CA-2007-01-12' 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 = 'N248CA' AND deregistration_id = 'N248CA-2007-01-12' 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 COMA0010370Channel · crackedWHILE PERFORMING A SCHEDULED INSPECTION, IT WAS DISCOVERED THAT THE PAX DOOR CHANNEL NR 4 IS CRACKED (P/N 120-1658-001). REMOVED THE OLD CHANNEL AND INSTALLED A SERVICEABLE CHANNEL.SDR COMA0010369Channel · crackedTHE PAX DOOR VERTICAL CHANNEL (P/N 120-21057-003) BETWEEN NR 4 AND NR 5 STRINGERS IS CRACKED. REMOVED THE OLD CHANNEL AND INSTALLED A SERVICEABLE CHANNEL.SDR COMA0010368Channel · crackedTHE PAX DOOR NR 2 STRINGER FROM THE TOP END FWD SIDE IS CRACKED (P/N 120-21158-001). REMOVED THE OLD NR 2 STRINGER CHANNEL AND INSTALLED A SERVICEABLE STRINGER.SDR COMA0010367Channel · crackedTHE PAX DOOR VERTICAL CHANNEL (P/N 12024577-003) BETWEEN NR 5 AND NR 6 STRINGER IS CRACKED. REMOVED THE OLD CHANNEL AND INSTALLED A SERVICEABLE CHANNEL.SDR COMA0010330Battery · dischargedFORWARD CABIN EMERGENCY LIGHTS WILL NOT REMAIN ILLUMINATED. REPLACED BATTERY.SDR COMA0010126Pump · leakingGREEN HYDRAULIC SYSTEM LOW PRESSURE AND LOW QUANTITY. REPLACED THE LEFT HAND ENGINE HYDRAULIC PUMP.SDR COMA0010058Sign · brokenEXIT SIGN AT ROW 5 IS BROKEN. REPLACED EXIT SIGN.SDR COMA0010050Warning Light · false indicationLOW OIL PRESSURE WARNING LIGHT ON MAP CAME ON. REPLACED THE MAP.SDR COMA9910189Battery · dischargedEMERGENCY LIGHTS FWD OF ROW 4 WERE INOPERATIVE. REPLACED EMERGENCY LIGHTS BATTERY.SDR COMA9910155Circuit Breaker · trippedDURING TAKEOFF FROM MCO, THE AURAL TRIM WARNING ACTIVATED. FOUND THE AURAL WARNING CIRCUIT BREAKER TRIPPPED, RESET THE AURAL TRIM WARNING CIRCUIT BREAKER.SDR COMA9910108Bulb · failedOVERHEAD EMERGENCY LIGHT AT ROW 8 IS INOPERATIVE. REPLACED LIGHT BULB.SDR COMA9910065Bellcrank · crackedUPON REINSTALLATION OF THE PILOT'S DIRECT VISION WINDOW AFTER REPLACEMENT OF THE SEAL, FOUND AFT LOWER BELL CRANK TO BE CRACKED .25 INCH THROUGH WEB BY ROLLER. REMOVED AND REPLACED LOWER BELL CRANK AND RIGGED IAW EMB-120 MM CH 52-22-01.SDR COMA9810276Battery · dischargedTWO EMERGENCY LIGHTS ARE INOPERABLE FORWARD CABIN SECTION. REPLACED EMERGENCY LIGHT BATTERY.SDR COMA9810249Box Control · malfunctionLANDING GEAR WILL NOT RETRACT. REPLACED LANDING GEAR CONTROL BOX.SDR COMA9810214Buttstrap · corrodedDURING 2C INSPECTION, TASK 151-012 REVEALED LEFT NR 5 BUTTSTRAP TO BE CORRODED. REMOVED BUTTSTRAP AND INSTALLED SERVICEABLE BUTTSTRAP USING EMB 120 STANDARD PRACTICES.SDR COMA9810213Buttplate · corrodedDURING 2C INSPECTION, TASK 5310-131-01I REVEALED CENTER BUTTPLATE TO HAVE SPOTS OF CORROSION THAT WERE BEYOND LIMITS. REMOVED CENTER BUTTPLATE AND INSTALLED SERVICEABLE BUTTPLATE USING EMB 120 SRM STANDARD PRACTICES.SDR COMA9810212Buttstrap · corrodedDURING 2C INSPECTION, TASK 5310-131-01I REVEALED LEFT FORWARD BUTTSTRAP TO BE CORRODED. REMOVED BUTTSTRAP AND INSTALLED SERVICEABLE BUTTSTRAP USING EMB 120 SRM STANDARD PRACTICES.SDR COMA9810211Buttstrap · corrodedDURING 2C INSEPCTION, TASK 151-012 REVEALED RIGHT NR 5 BUTTSTRAP TO BE CORRODED. REMOVED BUTTSTRAP AND INSTALLED SERVICEABLE BUTTSTRAP USING EMB 120 STANDARD PRACTICES.SDR COMA9810210Crossbeam · corrodedDURING 2C INSPECTION, TASK 5310-131-01I REVEALED RIGHT CENTER CROSSBEAM AT FRAME 16 TO BE CORRODED. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES.SDR COMA9810209Crossbeam · corrodedDURING 2C INSPECTION, TASK 5310-131-01I REVEALED LT CROSSBEAM AT FRAME 14 TO BE CORRODED. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES.SDR COMA9810208Crossbeam · corrodedDURING 2C INSPECTION, TASK 5310-131-01I REVEALED LT CENTER CROSSBEAM TO BE CORRODED AT FRAME 16. REMOVED AND REPLACED CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES.SDR COMA9810207Crossbeam · corrodedDURING 2C INSPECTION, TASK 5310-131-01I REVEALED RIGHT CROSSBEAM AT FRAME 16 TO BE CORRODED. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES.SDR COMA9810206Crossbeam · corrodedDURING 2C INSPECTION, TASK5310-131-01I REVEALED LT CENTER CROSSBEAM TO BE CORRODED. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES.SDR COMA9810205Crossbeam · corrodedDURING 2C INSPECTION, TASK5310-131-01I REVEALED RT CROSSBEAM AT FRAME 20 TO BE CORRODED. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB 120SRM STANDARD PRACTICES.SDR COMA9810204Crossbeam · corrodedDURING 2C INSPECTION, TASK5320-141-03I REVEALED LT CENTER CROSSBEAM AT FRAME 23 TO BE HEAVILY CORRODED. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES.SDR COMA9810203Sill · corrodedDURING 2C INSPECTION, TASK 163-012 REVEALED LEFT CARGO SILL TO BE CORRODED. REMOVED SILL AND INSTALLED SERVICEABLE USING EMB 120 SRM STANDARD PRACTICES.SDR COMA9810202Sill · corrodedDURING 2C INSPECTION, TASK 5310-131-01I REVEALED LEFT NR 1 SILL TO BE CORRODED. REMOVED SILL AND INSTALLED SERVICEABLE SILL USING EMB 120 SRM STANDARD PRACTICES.SDR COMA9810201Sill · corrodedDURING 2C INSPECTION, TASK 5310-131-01I REVEALED RIGHT NR 1 SILL TO BE CORRODED. REMOVED SILL AND INSTALLED SERVICEABLE SILL USING EMB 120 SRM STANDARD PRACTICES.SDR COMA9810200Buttstrap · corrodedDURING 2C INSPECTION, TASK 151-012 REVEALED LEFT NR 5 BUTTSTRAP TO BE CORRODED. REMOVED BUTTSTRAP AND INSTALLED SERVICEABLE PART USING EMB 120 STANDARD PRACTICES.SDR COMA9810199Buttstrap · corrodedDURING 2C INSPECTION, TASK 5310-131-01I REVEALED CENTER NR 1 BUTTSTRAP TO BE CORRODED. REMOVED BUTTSTRAP AND INSTALLED SERVICEABLE BUTTSTRAP USING EMB 120 SRM STANDARD PRACTICES.SDR COMA9810198Buttstrap · corrodedDURING 2C INSPECTION, TASK 145-012 REVEALED LEFT NR 2 BUTTSTRAP TO BE CORRODED. REMOVED AND REPLACED BUTTSTRAP WITH SERVICEABLE ONE USING EMB 120 STANDARD PRATICES.SDR COMA9810197Buttstrap · corrodedDURING 2C INSPECTION, TASK 151-012 REVEALED RIGHT NR 5 BUTTSTRAP TO BE CORRODED. REMOVED BUTTSTRAP AND INSTALLED SERVICEABLE ONE USING EMB 120 SRM STANDARD PRACTICES.SDR COMA9810196Buttstrap · corrodedDURING 2C INSPECTION, TASK 151-012 REVEALED RIGHT NR 4 BUTTSTRAP TO BE CORRODED. REMOVED BUTTSTRAP AND INSTALLED SERVICEABLE PART USING EMB 120SRM STANDARD PRACTICES.SDR COMA9810195Buttstrap · corrodedDURING 2C INSPECTION, TASK 145-012 REVEALED RIGHT NR 3 BUTTSTRAP TO BE CORRODED. REMOVED BUTTSTRAP AND INSTALLED A SERVICEABLE BUTTSTRAP USING EMB 120 SRM STANDARD PRACTICES.SDR COMA9810173Indicator · malfunctionPRESSURIZATION SYSTEM DOES NOT WORK. REPLACED THE CABIN PRESSURE TRIPLE INDICATOR.SDR COMA9810157Current Sensor · failedCREW REPORTED F/O 'S AOA HEAT INOP. AVIONICS REPLACED THE RIGHT CURRENT SENSOR ASSEMBLY. UPON INSPECTION/TEARDOWN IN THE AVIONICS SHOP, THE CURRENT SENSOR FOR THE RIGHT AOA VANE HEAT WAS FOUND TO BE DAMGED BY SEVERE OVERHEATING. THE CURRENT SENSOR WAS REPLASDR COMA9810152Battery · dischargedEMERGENCY EXIT LIGHTS INOP AT ROW 4 AND 5. REPLACED EMERGENCY BATTERY.SDR COMA9810025Seal · tornAIRCRAFT WOULD NOT PRESURIZE AFTER TAKEOFF. REPLACED CARGO DOOR SEAL.SDR COMA9710479Battery · dischargedFORWARD CABIN EMERGENCY LIGHT INOP. REPLACED EMERGENCY LIGHT BATTERY.SDR COMA9710418Warning Unit · malfunctionTAKEOFF, TRIM AURAL WARNING SOUNDED, TRIM WAS CONFIRMED TO BE IN TAKEOFF RANGE. REPLACED THE AURAL WARNING UNIT.SDR COMA9710408Control Module · malfunctionWITH THE LANDING GEAR IN UP POSITION, THE B-SYSTEM DISAGREE LIGHTS ILLUMINATED. CYCLED GEAR CONTROL AND INDICATIONS NORMAL. REPLACED THE LANDING GEAR CONTROL MODULE.SDR COMA9710322Engine · failedLEFT ENGINE CHIP DETECTOR WARNING ON. REPLACED LEFT ENGINE.SDR COMA9710266Fuse · blownRT EXTERNAL OVERWING EMERGENCY LIGHT IS INOP. REPLACED THE NR 2 EMERGENCY BATTERY FUSE.SDR COMA9710239Cowl Door · separatedLT ENGINE NACELLE AFT INBOARD COWLING DOOR SEPARATED AIRCRAFT AFTER TAKEOFF. REPLACED COWLING DOOR AND ASSOCIATED INTERMEDIATE COWLING ASSY DUE TO ADDITIONAL DAMAGE.SDR COMA9710233Battery · dischargedFIVE LIGHTS IN THE EMERGENCY FLOOR PATH LIGHTING ARE INOP. REPLACED THE NR 2 BATTERY PACK.SDR COMA9710229Battery · discharged4 WHITE AND 1 RED FLOOR EMERGENCY LIGHTS FAILED DURING TAXI-OUT. REPLACED NR 2 BATTERY PACK AT SEAT 4C LOCATION.SDR COMA9710087Accessory Gb · oil leakRT ENGINE OIL PRESSURE DROPPED TO 50 PERCENT DURING FLIGHT. ENGINE WAS FOUND TO BE 6 QUARTS LOW OIL LEVEL. REPLACED THE AGB BREATHER SEAL AND GEAR SHAFT.SDR COMA9610297Valve · defectiveAFTER TAKEOFF, THERE WAS A 1,500 LB FUEL IMBALANCE. AIRCRAFT RETURNED TO FIELD. REPLACED DEFECTIVE RIGHT WING FUEL PILOT VALVE.SDR COMA9610286Transfer Tube · not seatedRT ENGINE LEAKING FUEL AND SMOKING AFTER SHUT DOWN. SECURED LOOSE FUEL TRANSFER TUBES ON THE NR 14 FUEL NOZZLE.SDR COMA9610285Tube · leakingRT ENGINE LEAKING FUEL AND SMOKING AFTER SHUT DOWN. REPLACED LEAKING FUEL NOZZLE TRANSFER TUBE.
Back to N248CA, cancelled Jan 12, 2007