N247CA, cancelled Aug 13, 2025
Service difficulty reports · 60
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 = 'N247CA' AND deregistration_id = 'N247CA-2025-08-13' 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 = 'N247CA' AND deregistration_id = 'N247CA-2025-08-13' 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 COMA0010314Channel · crackedUPON COMPLIANCE OF 1C-CHECK TASK 52-14, THE PASSENGER DOOR INNER CHANNEL WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IN ACCORDANCE WITH EMB-120 STUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010313Bulkhead · crackedUPON COMPLIANCE OF 1C-CHECK TASK 433-01Z, THE LEFT NACELLE FRAME 14 EXHAUST PAN SUPPORT BULKHEAD WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IN ACCORDANCE WITH EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 33712-1, IR-7-2SDR COMA0010312Skin · gougedUPON COMPLIANCE OF 1C-CHECK TASK 100-01Z, THE FUSELGE FWD LOWER RT SKIN JUST BELOW LAV DUMP VALVE DOUBLER WAS FOUND TO BE GOUGED. THE DAMAGED PART WAS REPAIRED IN ACCORDANCE WITH EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND EMBRAER REPAIR NR SST-18SDR COMA0010311Skin · dentedUPON COMPLIANCE OF 1C-CHECK TASK 5310-122-01E, THE FUSELAGE RT FWD LOWER SKIN WAS FOUND TO BE DENTED. THE DAMAGED PART WAS REPAIRED IN ACCORDANCE WITH EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND EMB120 SRM 53-00-01, FIGURE 201.SDR COMA0010310Shear Tie · crackedWHILE PERFORMING OTHER MAINTENANCE, THE FUSELAGE LEFT HAND SKIN SUPPORT AT FRAME 9, WAS FOUND TO BE CRACKED. THE SKIN SUPPORT WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT NR 660-1, IR, 2-16-93.SDR COMA0010309Skin · gougedUPON COMPLIANCE OF 1C-CHECK TASK 813-01Z THE CARGO DOOR SKIN WAS FOUND TO BE GOUGED. THE DAMAGED PART WAS REPAIRED IN ACCORDANCE WITH EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND EMB-120 SRM 52-30-01, FIGURE 201.SDR COMA0010308Angle · crackedUPON COMPLIANCE OF 1C-CHECK TASK 194-01Z THE RIGHT WING UPPER SKIN ATTACH ANGLE FOR FAIRING 194 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IN ACCORDANCE WITH EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 1226-21, IR,SDR COMA0010307Angle · crackedUPON COMPLIANCE OF 1C-CHECK TASK 193-01Z, THE LEFT WING UPPER SKIN ATTACH ANGLE FOR FAIRING 193 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IN ACORDANCE WITH EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 1226-21, IR, SDR COMA0010306Skin · damagedUPON COMPLIANCE OF 1C-CHECK TASK 5720-622-02E, THE RIGHT WING LOWER SKIN RIVET HOLE AT RIB 6, STRINGER 10 WAS FOUND TO BE IMPROPERLY COUNTERSUNK. THE DAMAGED SKIN WAS REPAIRED IN ACCORDANCE WITH EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESISDR COMA0010305Strap · corrodedWHILE PERFORMING OTHER MAINTENANCE, THE FUSELAGE FORWARD CENTER CABIN FLOOR BEAM BUTT-STRAP WAS FOUND TO BE CORRODED. THE BUTT-STRAP WAS REPLACED IN ACCORDANCE WITH THE EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010202Battery · dischargedEMERGENCY FLOOR PATH LIGHTING IS INOPERABLE. REPLACED EMERGENCY LIGHT BATTERY.SDR COMA0060258Boot · leakingWING DE-ICE FAIL WARNING. REPLACED THE RIGHT WING INBOARD DE-ICE BOOT.SDR COMA0010028Battery · dischargedCABIN EMERGENCY LIGHT SYSTEM WAS PARTIALLY INOP. REPLACED EMERGENCY BATTERY.SDR COMA0010026Battery · discharged5 EXIT LIGHTS ON FLOOR AND 1 ON OVERHEAD ARE INOPERABLE. REPLACED THE NR 1 AND NR 2 EMERGENCY BATTERIES.SDR COMA9910198Sign · inoperativeEMERGENCY EXIT SIGN AT ROW 8 IS INOPERABLE. REPAIRED DAMAGED WIRES AT EXIT SIGN.SDR COMA9910190Controller · malfunctionedRT PROPELLER RPM WAS 99.2 TO 99.6 AFTER TAKEOFF. GROUND RUNS SHOWED PROPELLER RPM TO BE IN LIMITATIONS.SDR COMA9910184Rccb · failedRIGHT HAND PROPELLER DEICE FAIL WARNING. REPLACED RCCB (CB0226).SDR COMA9910169Light · inopFWD EMERGENCY FLOOR LIGHT WAS INOP. REPLACED LIGHT ASSY.SDR COMA9910149Warning · activatedSERVICE DOOR WARNING DURING TAKEOFF. DOOR WARNING SYSTEM PREVIOUSLY DEFERRED PER MEL.SDR COMA9910150Warning · activatedSERVICE DOOR WARNING DURING TAKEOFF. DEFERRED DOOR WARNING SYSTEM PER MEL.SDR COMA9910084Sensor · failedLEFT MLG DOWN INDICATOR ON WITH GEAR RETRACTED. LANDING GEAR WOULD NOT EXTEND WHEN SELECTED. FREE FALL SYSTEM USED TO EXTEND GEAR. REPLACED DOWN LOCK PROXIMITY SENSOR. (M)SDR COMA9910034Deice · inopRIGHT HAND PROPELLER DEICE IS INOPERABLE. REPLACED THE NR 3 BLADE ON RIGHT HAND PROPELLER.SDR COMA9910026Frame · crackedLEFT NACELLE, FRAME WEB NR 10 CRACKED AT INBOARD RADIUS OF THE FLANGE. REPAIRED BY SPLICING IN A NEW FLANGE PER AERODESIGN REPORT NR 1076-2 AND EMB120 SRM 51-40-02.SDR COMA9910025Battery Pack · dischargedFORWARD SECTION OF CABIN EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED BATTERY PACK FOR THE FORWARD EMERGENCY LIGHTING.SDR COMA9910005Contactor · failedEXTERNAL POWER CONTACTOR BURNT/OVERHEATED AT TERMINAL ENDS. REPLACED CONTACTOR AND POSITIVE CABLE.SDR COMA9810277Fastener · brokenSERVICE DOOR WARNING DURING TAKEOFF. REPLACED BROKEN CAM LOCK FASTENER ON SINGLE POINT FUEL SERVICE DOOR.SDR COMA9810274Sensor · malfunctionedAFTER LANDING GEAR RETRACTED, RIGHT HAND MLG DOWN INDICATOR REMAINED ON. REPLACED DEFECTIVE DOWNLOCK PROXIMITY SENSOR.SDR COMA9810270Latch · not securedSERVICE DOOR WARNING DURING CLIMBOUT. AIRCRAFT RETURNED TO THE FIELD. CLOSED DOOR AND SECURED LATCH.SDR COMA9810238Pin · not removedNOSE LANDING GEAR WOULD NOT RETRACT. REMOVED NLG PIN. GEAR SWINGS GOOD.SDR COMA9810235Crossbeam · corrodedDURING 2C INSPECTION, TASK 5310-131-01I REVEALED LEFT CENTER CROSSBEAM TO BE CORRODED AT FRAME 16. REMOVED AND REPLACED CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES.SDR COMA9810233Sill · corrodedDURING 2C INSPECTION, TASK 5310-131-01I REVEALED LEFT NR 1 STILL TO BE CORRODED. REMOVED SILL AND INSTALLED SERVICEABLE SILL USING EMB 120 SRM STANDARD PRACTICES.SDR COMA9810232Sill · 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 COMA9810231Buttstrap · corrodedDURING 2C INSPECTION TASK 151-01Z REVEALED LEFT NR 5 BUTTSTRAP TO BE CORRODED. REMOVED BUTTSTRAP AND INSTALLED SERVICEABLE BUTTSTRAP USING EMB 120 STANDARD PRACTICES.SDR COMA9810230Buttstrap · 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 COMA9810229Wire Harness · out of positionDURING 2C INSPECTION, TASK 5720-622-01I, REVEALED THE WIRE HARNESS FOR THE RIGHT WING FORWARD FUEL BOOST PUMP TO BE CHAFFING ON THE METAL BRAIDED FUEL LINE. PUMP WIRE INSULATION WAS NOT DAMAGED ONLY WIRE HARNESS PROTECTIVE COVERING. REMOVED PUMP AND HARNESS SDR COMA9810236Buttplate · corrodedDURING 2C INSPECTION TASK 5310-131-O1I REVEALED CENTER BUTTPLATE TO HAVE SPOTS OF CORROSION THAT WERE BEYOND LIMITS. REMOVED CENTER BUTTPLATE AND INSTALLED SERVICEABLE BUTTPLATE USING EMB120 SRM STANDARD PRACTICES AND AERODESIGN REPORT NR 1671-1.SDR COMA9810172Wheel · crackedDURING TEARDOWN VISUAL INSPECTION FOR TIRE CHANGE, THE INNER HALF OF THE MAIN WHEEL ASSY WAS FOUND TO HAVE A CRACK APPROXIMATELY 2 INCHES IN LENGTH RUNNING INWARD IN THE WEB AREA, STARTING FROM UNDER THE BEARING CUP. THE WHEEL WAS REMOVED FROM SERVICE AT THISSDR COMA9810123Battery · dischargedSOME OF THE CABIN EMERGENCY LIGHTS ARE INOPERABLE. REPLACED EMERGENCY BATTERY.SDR COMA9710506Wire · brokenSOME OF THE CABIN FLOOR PATH EMERGENCY LIGHTS ARE INOP. REPAIRED BROKEN WIRE.SDR COMA9710316Fuel Door · not latchedSERVICE DOOR WARNING CAME ON AFTER TAKEOFF. SINGLE POINT FUEL SERVICE DOOR NOT LATCHED. SECURED DOOR AND AIRCRAFT RETURNED TO SERVICE.SDR COMA9710089Roller · dirtyFLAP DISAGREEMENT AFTER FLAPS SELECTED TO 0 DEGREES. REPLACED FLAP ROLLERS ON LEFT AND RIGHT OUTBOARD FLAPS.SDR COMA9710013Relay · failedEMERGENCY LIGHTING NOT ARMED WARNING ON MAP, CIRCUIT BREAKER TRIPPED. COULD NOT DUPLCIATE DISCREPANCY. REPLACED RELAY K201 FOR TROUBLESHOOTING.SDR COMA9610401Tubing · chafedHYDRAULIC FLUID LEAKING FROM LT ENGINE NACELLE. REPLACED DAMAGED SECTION OF GREEN SYSTEM HYDRAULIC PRESSURE TUBING BETWEEN NACELLE 13 AND 14.SDR COMA9610334Potentiometer · malfunctionCLUNKING SOUND AND UNCOMMANDED MOVEMENT FROM NOSE WHEEL STEERING SYSTEM. REPLACED THE NWS FEEDBACK POTENTIOMETER.SDR COMA9610288Switch · out of adjustCARGO DOOR WARNING SOUNDED DURING TAKEOFF. ADJUSTED CARGO DOOR MICROSWITCH. AIRCRAFT CONTINUED SERVICE.SDR COMA9610223Controller · failedTRANSPONDER NR 1 AND NR 2 REPORTED INOPERATIVE BY AIR TRAFFIC CONTROL. REPLACED CTL-92.SDR COMA9610225Fuel Nozzle · leakingFUEL LEAKING FROM RT ENGINE NACELLE. REPLACED THE RT ENGINE FUEL NOZZLES.SDR COMA9610166Sensor · defectiveWHEN LANDING GEAR SELECTED DOWN, GEAR DID NOT EXTEND. INDICATION WAS 5 RED INTRANSIT AND ONE GREEN DOWNLOCK. EMERGENCY SYSTEM USED TO EXTEND GEAR. REPLACED DEFECTIVE DOWNLOCK PROXIMITY SENSOR ON LEFT MLG.SDR COMA9610154Latch · brokenRIGHT MLG OUTBOARD GEAR DOOR WILL NOT CLOSE. REPLACED BROKEN DOOR LATCH ASSY.SDR COMA9610145Prop Contl Unit · malfunctionLEFT PROPELLER TAKES 30 SECONDS TO TRANSITION FROM FEATHER TO BETA RANGE. REPLACED THE PROPELLER CONTROL UNIT.
Back to N247CA, cancelled Aug 13, 2025