N831SK, cancelled Nov 3, 2006
Service difficulty reports · 21
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 = 'N831SK' AND deregistration_id = 'N831SK-2006-11-03' 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 = 'N831SK' AND deregistration_id = 'N831SK-2006-11-03' 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 S2YA05052Windshield · crackedDURING FLIGHT, THE CREW REPORTED THE CAPTAINS WINDSHIELD HAD CRACKED IN SEVERAL PLACES. THE FLIGHT CONTINUED WITH NO OTHER DISCREPANCIES. MAINTENANCE REPLACED THE LT WINDSHIELD. WITH NO FURTHER DEFECTS RETURNED THE AC TO SERVICE. (K)SDR S2YA05032Engine · lowDURING FLIGHT, CREW REPORT THE RT OIL PRESSURE WAS FLUCTUATING BETWEEN 70 AND 80 PSI AND OCCASIONALY DROPPING TO 50 TO 60 PSI AND THEY WERE GETTING A RED WARNING LIGHT. THE CREW PERFORMED AN AIR-TURN-BACK. OUTSTATION MECHANIC INSPECTED ENGINE CHEC THE CHIP DSDR S2YA05005Solenoid · inoperativeBEFORE FLIGHT, THE CREW REPORTED RT PROP WOULD NOT SPOOL UP, THEY RETURNED TO THE GATE FOR MECHANIC. MECHANIC REPLACED THE RT PROP GOVERNOR FOR TROUBLESHOOTING BUT THE PROBLEM REMAINED. MECHANIC REPLACED THE RT LOW PITCH SOLENOID AND OPERATIONAL CHECKS WERE SDR S2YA05009Valve · inoperativeSHORTLY AFTER TAKEOFF OF FLIGHT, THE CREW WAS UNABLE TO RETRACT THE GEAR. THE CREW PERFORMED AN AIR-TURN-BACK. MECHANIC INSPECTED THE SYSTEM AND REPLACED THE MLG HANDLE/SWITCH BUT OPS CHECKS WERE STILL BAD. MECHANIC REPLACED THE GROUND SERVICE VALVE AND PERSDR S2YA03011Downlock Switch · failedDURING APPROACH OF FLIGHT 1019, THE CREW DID NOT ACHIEVE A DOWN AND LOCKED INDICATION FOR THE RT MAIN GEAR. THE CREW MANUALLY EXTENDED THE GEAR. THE CREW STILL DID NOT GET THREE GREEN BUT THE IN-TRANSIT LIGHT EXTINGUISHED. THE CREW DID NOT DECLARE AN EMERGESDR S2YA03006Squat Switch · dirtyAFTER TAKEOFF OF FLIGHT 1007, THE GEAR INTRANSIT LIGHT ILLUMINATED WITH THE GEAR HANDLE UP AFTER, THE GEAR SHOULD HAVE RETRACTED. THE CREW MADE AN AIR TURNBACK. MECHANIC INSPECTED THE AIRCRAFT AND REPLACED THE RIGHT UPLOCK SWITCH. MECHANIC OPS CHECK THE SYSSDR S2YA00023Block · wornFLT 1354 - MKE-TVC - SHORTLY AFTER TAKEOFF, THE LEFT ENGINE TORQUE STARTED FLUCTUATED 100-200 LB. THE CREW MADE AN AIR-TURN-BACK AND AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE ENGINE AND REPLACED THE BETA BLOCK. MAINTENANCE OPS CHECKED THE A/C AND RETSDR S2YA98025Skin · bird strikeMKE/CWA - FLT 1071 - JUST AFTER TAKEOFF, AIRCRAFT STRUCK A BIRD JUST ABOVE THE FIRST OFFICER'S WINDSHIELD. THE CREW DECIDED TO RETURN TO MKE SO THE AIRCRAFT COULD BE INSPECTED FOR DAMAGE. AFTER MAKING AN UNEVENTFUL LANDING, MAINTENANCE INSPECTED AIRCRAFT ANDSDR S2YA98014Indicator · failedFLT 1124 - MKE-GRR - JUST AFTER TAKEOFF, THE FLIGHT CREW NOTICED THE PILOTS ALTIMETER WAS FLAGGED, ALTITUDE PRESELECT WAS ONLY SHOWING DASHES, AND THE TCAS WAS SHOWING A FAIL MESSAGE. THE CREW DECIDED TO RETURN TO MKE, ALTHOUGH DURING DESCENT EVERYTHING STARTSDR S2YA970023Squat Switch · out of adjustMKE/FNT - FLT 1905 - AFTER TAKEOFF, THE FLIGHT CREW ATTEMPTED TO RETRACT THE LANDING GEAR, BUT THE DOWNLOCK RELAY DID NOT RELEASE THE LANDING GEAR SAFETY HOOK. THE CREW IMMEDIATELY TURNED BACK TO MKE AND MADE AN UNEVENTFUL LANDING. MAINTENANCE FOUND THE RT LASDR S2YA97016Starter/Gen · malfunctionedGRR/MKE - FLT 1120 - AFTER ROTATION, CREW NOTICED THE LT DC GENERATOR FELL OFF-LINE WITH THE LT DC GEN ANNUNCIATOR ILLUMINATING. THE CREW ATTEMPTED TO RESET THE LT GENERATOR IN-FLIGHT, BUT WERE UNABLE TO. THE CREW MADE AN UNEVENTFUL LANDING AT GRR WITHOUT DESDR 97ZZZX1797Pressure Switch · inoperativeDURING THE MONTH OF JANUARY, SIX FUEL PRESSURE SWITCHES, P/N 100-389018-21 WERE REPLACED. THE TBR FOR THE SWITCHES WAS: 3,933.2 HRS FROM N NR 148SK; 1,418.2 HRS FROM N NR 831SK; 1,479.7 HRS FROM N NR 87SK; 2,525.6 HRS FROM N NR 881SK; 1,715.7 HRS FROM N NR 8SDR S2YA97011Switches · dirtyBNA/MKE - FLT 1266 - CREW NOTICED CABIN DOOR ANNUNCIATOR ILLUMINATE DURING CRUISE. CREW DIVERTED TO NEAREST AIRPORT, EVV EVANSVILLE, IND. AFTER A SAFE LANDING AT EVV, FLIGHT CREW FOUND WHEN THEY WIGGLED THE DOOR HANDLE THE ANNUNCIATOR WOULD FLICKER. AFTER SSDR 97ZZZX1793Vertical Gyro · failedDURING THE MONTH OF JANUARY, SEVEN 332D-11T VERTICAL GYROS (P/N 622-4565-001) FAILED. THE TIMES FOR THE VG'S WERE: 1,639.3 HRS ON N NR 145SK; 5,375.1 HRS ON N NR 79SK; 6,125.4 ON N NR 801SK; 2,328.9 HRS ON N NR 831SK; 3,063.1 HRS ON N NR 881SK; 6,820.9 HRSSDR S2YA960044Comp Contl Head · inoperativeDURING THE MONTH OF NOVEMBER, THERE WERE FOUR CTL-22 COMPENSATION CONTROL HEADS, P/N 622-6520-008, THAT WERE REMOVED DUE TO PART OR ALL OF BACKLIGHTING BEING INOPERATIVE. THE PARTS TIME SINCE OVERHAUL WERE 5,447.8 FROM N NR 831SK NR 1 SIDE; 6,578.5 HRS FROM NSDR 97ZZZX1807Nav Contl Head · inoperativeDURING THE MONTH OF NOVEMBER, THERE WERE SEVEN CTL-32 NAV CONTROL HEADS, P/N 622-6521-016, THAT WERE REMOVED DUE TO PART OR ALL OF BACKLIGHTING BEING INOPERATIVE. THE PARTS TIME SINCE OVERHAUL WERE 6,794.4 HRS FROM N NR 79SK NR 1 SIDE; 6,794.4 HRS FROM N NR 7SDR 97ZZZX1802Comp Contl Head · inoperativeDURING THE MONTH OF NOVEMBER, THERE WERE FOUR CTL-22 COMPENSATION CONTROL HEADS, P/N 622-6520-008, THAT WERE REMOVED DUE TO PART OR ALL OF BACKLIGHTING BEING INOPERATIVE. THE PARTS TIME SINCE OVERHAUL WERE 5,447.8 FROM N NR 831SK NR 1 SIDE; 6,578.5 HRS FROM NSDR 97ZZZX1787Comp Contl Unit · inoperativeDURING THE MONTH OF NOVEMBER, THERE WERE SEVEN CCU-65 COMPENSATION CONTROL UNITS, P/N 622-6135-014, REMOVED DUE TO PART OR ALL OF BACKLIGHTING BEING INOPERATIVE. THE PARTS TIME SINCE OVERHAUL WERE 6,805.5 HRS FROM N NR 118SK; 6,526.6 HRS FROM N NR 831SK; 6,SDR S2YA960024Tire · flat spottedAFTER THE FLIGHT CREW DEPARTED MKE ON FLT NR 1053, THE CREW NOTED SEVERE VIBRATION FROM THE NOSE, RETURNED TO MKE. MAINTENANCE CHANGED THE NOSE WHEEL ASSY, AND IT WAS DETERMINED THAT A TIRE FLAT SPOT OUT OF BALANCE CONDITION CAUSED THE VIBRATION. (M)SDR S2YA960006Prop Governor · failedGRR - FLT 1123 - THE FLIGHT CREW EXPERIENCED TORQUE FLUCTATIONS OF THE RIGHT ENGINE IN-FLIGHT, TURNED BACK TO GRR. THROUGH TROUBLESHOOTING, MAINTENANCE FOUND THE PRIMARY GOVERNOR FAILED AND REPLACED IT. DURING A RUN-UP CHECK, THE RIGHT AUTOFEATHER WAS TESTEDSDR 95ZZZX2479Rib · crackedDURING AN INSPECTION, MAINTENANCE FOUND LT WING CENTER SECTION MID-RIB AT WS 83.00 TO HAVE A CRACK 1.1250 INCH LONG. THE CRACK WAS ALONG THE TOP BEND RADIUS AT THE RIB CENTER STIFFENER ATTACH POINT. THE FORWARD REINFORCEMENT PN 114-120033-15 WAS ALSO CRACKED
Back to N831SK, cancelled Nov 3, 2006