N264CA, cancelled Oct 5, 2006
Service difficulty reports · 88
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 = 'N264CA' AND deregistration_id = 'N264CA-2006-10-05' 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 = 'N264CA' AND deregistration_id = 'N264CA-2006-10-05' 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 COMA0210029Lamp · burned outFLIGHT 5047 EMERGENCY LIGHT INOP.REPLACED LIGHT BULB.SDR COMA0210015Bracket · crackedDURING AN E-10 PART A INSPECTION THE FUSELAGE SKIN SUPPORT BRACKET (P/N 120-34416-001) ON THE LEFT SIDE JUST BELOW THE PILOTS WINDSHIELD SIDE POST AT FRAME 9 WAS FOUND TO BE CRACKED.THE CRACKED BRACKET (P/N 120-34416-001) WAS REMOVED FROM THE AIRCRAFT AND A SESDR COMA0210012Control Box · malfunctionedFLIGHT 5070 LANDING GEAR CONTROL COULD NOT BE SELECTED TO THE UP POSITION.REPLACED THE L/G CONTROL HANDLE ASSY.SDR COMA0210010Engine · failedFLIGHT 5059 R/H ENGINE FAILED WITH NO WARNINGS. IFSD REPLACED ENGINE.SDR COMA0210003Battery · dischargedFLIGHT 5044 EMERGENCY FLOOR PATH LIGHTS ARE INOP IN SEVERAL PLACES. REPLACED THE NR 2 EMERGENCY BATTERY.SDR COMA0110156Battery · dischargedFLIGHT #5044. EMERGENCY LIGHTS ARE INOP.REPLACED THE EMERGENCY LIGHTS BATTERY.SDR COMA0110148Roller · wornFLIGHT 5070 FLAP SELECTION BEYOND 25 DEGREES RESULTS IN FLAP DISAGREEMENT WARNING.REPLACED THE R/H OUTBD FLAP ROLLERS. SYSTEM CHECK SATISFACTORY.SDR COMA0110139Indicator · faultyFLIGHT #5053. DURING APPLICATION OF POWER FOR TAKE OFF AT MCO THE #2 NH ANALOG INDICATION FAILED, AIRCRAFT RETURNED TO THE GATE.REPLACED THE NH/NL INDICATOR.SDR COMA0110136Indicator · faultyFLIGHT #5053. DURING APPLICATION OF POWER FOR TAKE OFF AT MCO THE #2 NH ANALOG INDICATION FAILED, AIRCRAFT RETURNED TO THE GATE.REPLACED THE NH/NL INDICATOR.SDR COMA0110042Boot · damagedWING DE-ICE FAIL WARNING. REPAIRED HOLES IN WING LEADING EDGE DE-ICE BOOTS, USING PATCH KIT.SDR COMA0110032Display · malfunctionedATTITUDE DISPLAY AND FLIGHT DIRECTOR FAILURE WARNINGS. REPLACED THE NR 2 AHRS.SDR COMA0110031Reservoir · lowHYDRAULIC RESERVOIR LOW LEVEL CAUTION. SERVICED HYD RESERVOIR, NO DEFECTS FOUND WITH HYDRAULIC SYSTEM.SDR COMA0010377Buttstrap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 132-01Z THE FORWARD RH FLOOR SUPPORT BUTTSTRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010376Buttstrap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z THE FORWARD LH FLOOR SUPPORT BUTTSTRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL MANUAL STANDARD PRACTICES.SDR COMA0010375Buttstrap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z THE FORWARD CENTER FLOOR SUPPORT BUTTSTRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT #1671-1, REV. 1, 1-28-97.SDR COMA0010374Skin · gougedUPON COMPLIANCE OF 2 YEAR CORROSION CHECK TASK 5310-132-CO1E THE FUSELAGE SKIN BELOW THE LAV DUMP VALVE DOUBLER WAS FOUND TO BE GOUGED. THE DAMAGED PART WAS REPAIRED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND EMBRAER REPAIR FAX #SST-3090/00SDR COMA0010402Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-432-04I THE LT NACELLE OUTBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-IR, 7-25-99.SDR COMA0010401Skin · chafedUPON COMPLANCE OF 2C INSPECTION TASK 5410-432-04I THE LT NACELLE INBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1,IR,7-25-99.SDR COMA0010400Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-442-04I THE RT NACELLE INBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1, IR, 7-25-99.SDR COMA0010399Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-442-04I THE RT NACELLE OUTBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1, IR, 7-25-99.SDR COMA0010398Sill · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 151-01Z THE LT FLOOR SUPPORT SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010397Floorbeam · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 132-01Z THE RT FLOOR SUPPORT T-SECTION WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010396Channel · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 811-02Z THE PAX DOOR INNER CHANNEL, FOURTH FROM BOTTOM WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010395Channel · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 811-02Z THE PAX DOOR INNER CHANNEL, SECOND FROM BOTTOM WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010394Shear Tie · crackedUPON COMPLIANCE OF 2C INSPECTION 232-01Z THE FUSELAGE SKIN SUPPORT AT FRAME 13A, STRINGER 14R WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3653-IR, 11-7-00.SDR COMA0010393Skin · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 161-01Z THE CARGO DOOR CUTOUT INNER SKIN WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPAIRED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND EMBRAER REPAIR FAX NR SST-3065/00, 11-3-00.SDR COMA0010392Buttstrap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 161-01Z THE CARGO COMPARTMENT ENTRY THRESHOLD BUTTSTRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3661-3, IR, 6-12-00.SDR COMA0010391Floorbeam · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-122-01I THE RT FLOOR PROP AT FRAME 13 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3647-1, IR, 5-3-00.SDR COMA0010390Floorbeam · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-121-01I THE LT FLOOR PROP AT FRAME 12 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3647-1, IR, 5-3-00.SDR COMA0010389Shear Tie · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 221-01Z THE LT FUSELAGE SKIN SUPPORT BRACKET WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010388Sill · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 164-01Z THE RT FLOOR SUPPORT SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010387Sill · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 162-01Z THE RT FLOOR SUPPORT SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010386Crossbeam · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 152-01Z THE RT FLOOR SUPPORT CROSSBEAM WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010385Crossbeam · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 151-01Z THE LT FLOOR SUPPORT CROSSBEAM WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010384Crossbeam · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 145-01Z THE LT FLOOR SUPPORT CROSSBEAM WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010383Sill · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 141-01Z THE LT FLOOR SUPPORT SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010382Sill · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 132-01Z THE RT FLOOR SUPPORT SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010381Buttstrap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 141-01Z THE LT FLOOR SUPPORT BUTTSTRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL PRACTICES.SDR COMA0010380Buttstrap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z THE CENTER FLOOR SUPPORT BUTTSTRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010379T-Section · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 132-01Z THE RT FLOOR SUPPORT T-SECTION AT FRAME 16 WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL PRACTICES.SDR COMA0010378Floorbeam · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z THE LT FLOOR SUPPORT T-SECTION AT FRAME 16 WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010372Battery · dischargedFWD SECTION OF EMERGENCY FLOOR LIGHTING IS INOP. REPLACED THE NR 1 EMERGENCY BATTERY.SDR COMA0010331Light · inoperativeEMERGENCY LIGHT AT ROW 5 IS INOPERABLE. COULD NOT DUPLICATE. EMERGENCY LIGHT OPS NORMAL.SDR COMA0010327Connector · dirtyAUTOFEATHER WARNING DURING TAKEOFF. CLEANED CONNECTORS CL4 AND CL28, SYSTEM TESTED SATISFACTORY.SDR COMA0010066Receptacle · shortedMECHANIC NOTICED SMOKE COMING FROM THE GPU PLUG WHILE AIRCRAFT WAS PARKED AT THE GATE. REPLACED THE EXTERNAL POWER RECEPTACLE AND MULTIPLE AVIONICS COMPONENTS DUE TO CONTAMINATION FROM FIRE EXTINGUISHER CHEMICALS.SDR COMA0010067Pcu · out of rigRIGHT PROPELLER RPM 102.7 PERCENT. CHECKED PROPELLER TO PCU RIGGING, FOUND NO DEFECTS AND FUNCTION CHECK NORMAL. A/C RETURNED TO SERVICE.SDR COMA0010052Skin · corrodedON A MAINTENANCE SERVICE CHECK, MECHANIC NOTED POPPED RIVET HEAD ON EXTERNAL SKIN, FRAME 21, LOWER LEFT SIDE, AND SEVERAL BULGES IN SKIN. UPON FURTHER INSPECTION, FOUND CORROSION BETWEEN SKIN AND TITANIUM STRAP. CUT OUT CORRODED AREA, FABRICATED AND INSTALLESDR COMA0010053Potentiometer · malfunctionedLANDING GEAR SELECTOR COULD NOT BE SELECTED UP. REPLACED THE NWS FEEDBACK POT.SDR COMA0010047Battery · dischargedFORWARD SECTION OF EMERGENCY FLOOR PATH LIGHTING IS INOPERABLE. REPLACED EMERGENCY BATTERY.SDR COMA0010037Sensor · malfunctionedLANDING GEAR FAILED TO RETRACT, ALL GREEN INDICATORS ON WITH SELECTOR UP. REPLACED RIGHT HAND MLG UPLOCK SENSOR.
Back to N264CA, cancelled Oct 5, 2006