Pilatus PC-12/47E
Service difficulty reports · 211
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = 'PC1247E' 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 aircraft_model_key = 'PC1247E' 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 CA130107001Heater · failed(CAN) DURING CRUISE, ANNUNCIATOR PANEL ILLUMINATED A CAUTION MESSAGE INDICATING AN AOA FAIL. MAINTENANCE TROUBLESHOOTING DETERMINED THAT THE VANE AND TIP HEATING ELEMENTS WERE NOT FUNCTIONING. REPLACED UNIT.SDR CA121219001Actuator · leaking(CAN) DURING WALKAROUND ACFT NOTICED HYDRAULIC FLUID ON FLOOR UNDER LT MLG. INVESTIGATION REVEALED FLUID WAS LEAKING FROM AROUND SHAFT OF MLG ACTUATOR. REPLACED ACTUATOR WITH SERVICEABLE UNIT. HYDRAULIC SYSTEM SERVICED IAW AMM. ACTUATOR PN IS 70839.SDR CA121213002Adiru · failed(CAN) HEADING INDICATION ON LT PRIMARY FLIGHT DISPLAY DRIFTING 7-8 DEGREES INTERMITTENTLY IN CRUISE FLIGHT AND ALSO NOTED ON THE GROUND. HEADING REPORTED TO DRIFT SLOWLY AND RETURN TO NORMAL A SHORT TIME LATER. ELECTRONIC STANDBY, MAGNETIC STANDBY AND RT PRISDR CA121221011Relay · damaged(CAN) DURING MAINTENANCE, IT WAS NOTED THE BEACON LAMP CAME ON WITH THE BEACON SWITCH IN THE OFF POSITION WHEN THE ACFT WAS POWERED. TROUBLESHOOT SYS AND REPLACED THE RELAY LISTED ABOVE. ALL TESTED SERVICEABLE.SDR CA121119010Power Supply · failed(CAN) AIRCRAFT WAS IN CLIMB, GOING THRU 8000 FT CAS ALARM WENT OFF. THE PILOTS PFD AND THE UPPER MFD WERE BLACK WITH RED X`S IN THEM. PILOT NOTED THAT THE 20 AMP BREAKER FOR MAU CHANNEL 1 HAD POPPED. THE PILOT RESET THE BREAKER AND EVERYTHING RETURNED TO NOSDR CA121122003Pump · leaking(CAN) SMALL AMOUNT OF HYDRAULIC FLUID LEAKING FROM THE REAR FLANGE OF THE PUMP. REPLACEMENT PUMP INSTALLED.SDR CA120502004Brushes · burned(CAN) DURING ROUTINE INSPECTION, THE VCCS MOTOR WAS FOUND TO HAVE BURNED BRUSHES AND THE MAIN POWER C/B FOR THE UNIT WAS POPPED.SDR CA120412006Drive Unit · failed(CAN) FLAPS WOULD NOT RETRACT FROM TAKEOFF POSITION ON TAKEOFF. ACFT RETURNED TO AIRPORT. PILOTS ATTEMPTED GROUND RESET. NO RESET, FLAP WOULD NOT RETRACT. MAINTENANCE STAFF ATTEMPTED A FLAP RESET WITH MAINTENANCE BOX. NO RESET. TROUBLESHOOTING FOUND THAT 2SDR CA120306008J-Box · loose(CAN) ON FEB 17, AT 1131.6 HRS, A DEFECT WAS RECORDED FOR BATTERY ASSIST NOT FUNCTIONING, SECONDARY START, WHICH WAS RECTIFIED BY REPLACEMENT OF THE LHPJB. ON FEB 25 AT 1142.8 HRS A DEFECT WAS RECORDED: GEN 1 BUS CAS MESSAGE, UNABLE TO CLEAR. WHILE CONDUCTINGSDR CA120215009Servo · defective(CAN) CREW REPORTS THAT THE YAW DAMPER FAILS AFTER IT STARTS TO CORRECT TRIM. SUBSIQUENTLY THE. AUTOPILOT FAILS.SDR CA120124001Elbow · cracked(CAN) FUEL LEAK NOTED FROM LT WING IB GEAR BAY AREA. FURTHER INVESTIGATION FOUND THE FCU SPILL RETURN LINE IN THE LH WING ON THE AFT SIDE OF THE WING SPAR WAS FOUND LOOSE. THE FUEL LINE WAS TIGHTENED. WING PANEL 51AB WAS REMOVED AND FUEL WAS ALSO FOUND LEAKING
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