N867QS
Service difficulty reports not matched to an aircraft · 19
They name N867QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N867QS' AND registry_match IS NULL 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 = 'N867QS' AND registry_match IS NULL 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 DXTA2014042905747Radome · damagedBIRD STRIKE ON RT SIDE OF ACFT AT NOSE. REMOVED AND REPLACED RADOME ASSEMBLY IAW MM 53-50-14. OPS CHECK GOOD.SDR DXTA2012032604429Apu · odorAFTER TAKEOFF, SHORTLY AFTER TURNING THE MAV'S ON AND THE APU COMPLETELY OFF THERE WAS A STRONG ODOR THAT SMELLED LIKE OIL. THERE WAS NO SMOKE. TURNED MAV'S TO LP AND THE ODOR WENT AWAY. R & R APU WITH UNIT REPAIRED UNIT. OPS AND LEAK CHECKED SATISFACTORY.SDR DXTA2012032249270Water Separator · odorAFTER ENGINE START UP, A FAINT ODOR OF OIL FUMES WAS NOTICED IN THE COCKPIT. DURING TAXI, THE ODOR CONTINUED, BUT WAS ATTRIBUTED TO THE PROXIMITY OF OTHER JETS. THE APU WAS RUNNING THROUGHOUT THE STARTUP, TAXI AND TAKEOFF. IMMEDIATELY AFTER T/O, THE OIL ODOR WSDR DXTA2012032204927Warning Light · illuminatedCRUISING AT FL390 "FADEC 2" LIGHT ILLUMINATED ON MWP FOLLOWED IMMEDIATELY BY A ROLL BACK TO FLIGHT IDLE OF NR 2 ENGINE. CREW COMPLETED CHECKLIST ITEMS. EIED 2 DISPLAYED A "F2A WF SOFT FAULT". ENGINE 2 REMAINED AT FLIGHT IDLE FOR ABOUT 20 MINS. DURING DESCENSDR DXTA2012020604863Downlock Switch · malfunctionedDURING APPROACH AFTER SELECTING GEAR DOWN, WITH A NORMAL 3 GREEN INDICATION, THE RT MAIN RED UNSAFE LIGHT BEGAN FLICKERING FAINTLY. REPLACED THE RT MLG DOWNLOCK SWITCH IAW MM CH 32-60-00. OPS CHECKED GOOD.SDR DXTA2011111604792Servo · failedELECTRIC TRIM FAILED IN FLIGHT. NOTHING WAS INDICATED ON ANY OF THE SCREENS THAT THE TRIM WAS NOT WORKING. AUTOPILOT STILL WORKED NORMALLY. DURING APPROACH, WHEN FLAPS WERE SELECTED TO 15 DEGREES OR GREATER, THE ELECTRIC TRIM WOULD START TO WORK NORMAL AGAIN. SDR DXTA2011080104671Hose · leakingRT SIDE BRAKES INOPERATIVE. BRAKE PEDAL GOES TO THE FLOOR WITH LITTLE RESISTANCE AND ONLY 200 LBS OF PRESSURE. WHEN THE BRAKE IS APPLIED INDEPENDENTLY, IT WILL NOT STOP ACFT. LT SIDE BRAKES WORK NORMALLY. TROUBLESHOT, FOUND FLEX HOSE LEAKING. REPLACED FLEXSDR DXTA2011080104676Brake · inoperativeCAPTAINS SIDE RT BRAKE IS INOPERATIVE. BRAKE PEDAL GOES TO THE FLOOR WITH LITTLE RESISTANCE AND ONLY 200 LBS OF PRESSURE. WHEN THE BRAKE IS APPLIED INDEPENDENTLY IT WILL NOT STOP THE AIRPLANE. CO-PILOTS SIDE BRAKES WORK NORMALLY.SDR DXTA2011030304486Brake Sys · weakLEFT PILOTS RIGHT BRAKE PEDAL SOFT AND SPONGY, ONLY PRODUCING 800-900 PSI. SERVICED AND BLED BRAKES, OPS CHECKED GOOD IAW MM 32-40-00.SDR E81RJW304273Transducer · failedINVESTIGATED FLIGHT CREW REPORT OF REPEATED MACH TRIM AND ELEVATOR TRIM FAIL ANNUNCIATOR INDICATIONS DURING DESCENT. DURING TROUBLESHOOTING FOUND ELEVATOR TRIM WOULD STOP IN SAME POSITION EACH TIME DURING OPERATION. NOTED AUTOPILOT TRIM INPUTS WOULD STOP JUST SDR DXTA2010070204136Switch · malfunctionedON DEPARTURE, SQUAT AND STALL IDENT MWS LIGHTS ILLUMINATED AND ACFT DID NOT PRESSURIZE. INSTALLED NEW WEIGHT ON WHEELS SWITCH, LT MLG IAW MM CHAPTER 32-10-12. PERFORMED SATISFACTORY GEAR SWING CYCLES AND OPS CHECK OF SYS.SDR DXTA200802838Eec · malfunctionedWHEN APPLYING TAKEOFF POWER LT ENGINE LAGS BEHIND R BY APPROX 15-20 PERCENT. REMOVED AND REPLACED LT DEEC WITH AN INSPECTED DEEC AND OPERATIONAL CHECKED OK IAW LMM CH 76-10-02 AND 72-00-00.SDR DXTA200702643Squat Switch · malfunctionedAFTER T/O, LANDING GEAR WOULD NOT RETRACT, SQUAT AND STALL IDENT WARNING LIGHTS CAME ON. REPLACED LT & RT MLG WOW SWITCH . ROUTED WIRE TO TERMINAL BLOCKS "JK" AND "KK" AND TERMINATED. PERFORMED OPERATIONAL CHECKS AS REQUIRED WITH NO DEFECTS NOTED. ALL WORK PESDR DXTA200601406Apu · overservicedAFTER TAKEOFF, DURING FIRST 15 MIN'S OF FLIGHT, AND DURING LAST 10 TO 15 MIN'S OF FLIGHT, STRONG ACRIDLY SWEET, BURNED SMELL FILLED CABIN. ALL PAX /CREW SMELLED ODOR, LANDED SAFELY. INSPECTED AND FOUND OIL LEAKING FROM APU ENCLOSURE COMPARTMENT. ACCESSED SDR DXTA200500853Warning Light · illuminatedDURING CLIMB-OUT, A LOUDER THAN NORMAL WIND NOISE WAS HEARD ON THE RIGHT SIDE OF THE COCKPIT. THE CABIN ALTITUDE CLIMBED AS HIGH AS 11500'. THE CABIN ALT LIGHT CAME ON AND THE HORN SOUNDED. KNOB PULLED MASKS DROPPED. ITEM IS UNDER INVESTIGATION.SDR DXTA200500750Pump · inoperativeNR 2 ENGINE FUEL ANNUNCIATOR ILLUMINATED AT 40 KNOTS ON T/O STATIC POWER, ARMED APR AT BRAKE RELEASED, T/O ABORTED. REMOVED INOP FUEL PUMP & INSTALLED AN OVERHAULED UNIT AS REQUIRED, OPS & LEAK CHECK GOOD. ALL WORK PERFORMED IAW HONEYWELL TFE-731-5BR MM CHAPTESDR DXTA200500749Fuel Filter · contaminatedON T/O RT ENGINE FUEL ANNUNICATOR ILLUMINATED. REMOVED RT ENGINE FUEL FILTER ELEMENT, P/N NR 897513-1 AND FILTER HOUSING O-RING P/N NR M25988/1-134 AND INSTALLED NEW FILTER AND O-RING, SAME P/N NRS. RAN ACFT RT ENGINE FOR 25 MINUTES AND NO RT ENGINE FUEL ANNSDR DXTA200500710Bulb · burned out2 EMERGENCY EXIT LIGHTS ABOVE DOOR AND ONE LOCATED AT THE ENTRANCE NOT ILLUMINATED DURING EMERGENCY LIGHT SYSTEM TEST. REPLACED 2 EACH BULBS IAW RAC DWG 149-349514. OP'S CHECKED GOOD.SDR DXTA200500643Warning Light · illuminatedDURING T/O ROLL AT 80 KTS ENG 2 FUEL ANNUNCIATORS ILLUMINATED. T/O ABORTED, ANNUNCIATOR EXTINGUISHED WHEN POWER REDUCED, THEN RE-ILLUMINATED AFTER RUNNING NR 2 ENGINE UP AGAIN TO FULL STATIC POWER AFTER 5-7 SECONDS. COULD NOT DUPLICATE SQK RAN ENGINES AT MAX
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