N345QS, cancelled Jun 27, 2011
Service difficulty reports · 16
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 = 'N345QS' AND deregistration_id = 'N345QS-2011-06-27' 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 = 'N345QS' AND deregistration_id = 'N345QS-2011-06-27' 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 DXTA2010110304287Push-Pull Rod · looseDURING FLT VIBRATION FELT IN ACFT AIRFRAME. VIBRATION INCREASED WITH ACFT AIRSPEED & NOT ENGINE SPEED. VIBRATION WORSE TOWARD REAR OF ACFT. VIBRATION WAS NOT FELT BELOW 190 KTS, BUT INCREASED PROGRESSIVELY AS SPEED INCREASED. CHANGING ACFT ATTITUDE DID NOT CSDR DXTA2010070704144Adc · failedADC NR 1 FAILED IN FLIGHT. REVERTED TO NR 2. RED "X" ON AIRSPEED TAPE AND ALTIMETER TAPE. REVERTED BACK TO NR 1 AFTER LANDING AND RED "X" REMAINED. R & R NR 1 ADC. LEAK CHECK OK IAW MX 34-11-25 TASK 34-11-25-700. PITOT LEAK TO 249.8KTS, STATIC TO 31,350FT OSDR DXTA2009070603720Wire Harness · inoperativeANTI-SKID ANNUNICATOR LIGHT WILL INTERMITTENTLY ILLUMINATE AFTER GEAR RETRACTION. LIGHT ILLUMINATES APROX 30 SECONDS THEN EXTINGUISHES. BRAKES ALSO PULSATE ON LANDING WHEN BRAKES APPLIED FROM BOTH SIDES. REMOVED AND REPLACED LT ANTI SKID TRANSDUCER WIRING HSDR DXTA2008121703406Engine · malfunctionedNORMAL ENGINE START, LT ENGINE SHUTDOWN DURING THE SPEED BRAKE TEST. REMOVED LOWER COWLING ON LT ENGINE AND INVESTIGATED. NO DISCREPANCIES NOTED. STARTED BOTH ENGINES, RT FIRST THEN THE LT SIDE. LT ENGINE STARTED FINE. ATTEMPTED SEVERAL THINGS TO TRY ASDR DXTA2008121803406Engine · shutdownAFTER NORMAL ENGINE START LEFT ENGINE SHUT DOWN DURING THE SPEED BRAKE TEST.SDR DXTA200809213281Unknown · odorON TAKEOFF HAD STRONG ODOR OF HOT WIRE OR RUBBER. (HAD OVERHEAD FAN ON. WHEN TURNED OFF ODOR SEEMED TO LESSEN. VISUALLY INSP'D AIRCRAFT PERFORMED ENG RUNS WITH AIRCRAFT IN TAKEOFF CONFIG IAW NJA 560 NORMAL CHECKLIST NO ODORS NOTED ON GROUND RUN.SDR DXTA200803281Unknown · odorON TAKEOFF HAD STRONG ODOR OF HOT WIRE OR RUBBER.SDR DXTA200702608Wheel · out of balanceAT APPROX 50 KTS ON TAKE OFF ROLL, NOSE WHEEL SHIMMIES AND STAYS AT A STEADY STATE OF OSCILLATION UNTIL STOPPED. REMOVED NOSE SHIMMY DAMPER AND INSTALLED OVERHAULED UNIT. REMOVED NOSE WHEEL AND FOUND BALANCE TO BE OUT. REINSTALLED REPAIRED NOSE WHEEL BALANCESDR DXTA200601637Acm · failedBURNING ODOR DETECTED BY BOTH CREW MEMBERS DURING SECOND ENGINE START. NO SMOKE PRESENT. REMOVED AND REPLACED FAULTY ACM IAW C560 MM 21-51-00. OPS AND LEAK CHECK GOOD.SDR DXTA200601493Connector · unsecureLEFT AC INVERTER FAILED AND CB POPPED, RESET ONCE POPPED AGAIN WHEN ADDED T/O PWR. ABORTED T/O. SECURED NR 1 CONNECTOR, FOUND NR 1 CONNECTOR LOOSE & SECURED CONNECTOR. SYSTEM TESTED IAW CE 560 MM CHAP 24-20-04. SWAPPED INVERTERS FOR FURTHER TROUBLESHOOTINGSDR DXTA200601313Transducer · inoperativeANTI-SKID ANNUNCIATOR ILLUMINATED ON TAKEOFF ROLL. AIRSPEED WAS BELOW 70 KIAS. TROUBLESHOT SYSTEM. REMOVED AND REPLACED NR 2 TRANSDUCER AND SKIN CONTROL UNIT. OPS CHECK GOOD IAW CE 560 MM CH 32-42-00 AND 32-42-07.SDR DXTA200601265Reservoir · emptyBRAKE FLUID RESERVOIR EMPTY AFTER LANDING WHEN PARKING, BRAKES FELT MUSHY THEN NO BRAKE PEDAL PRESSURE. STOPPED AIRPLANE AND NEVER USED EMERGENCY HANDLE OR ANYTHING OF NITROGEN BOTTLE. POST FLIGHT, NO BRAKE FLUID, SOME OILY FILM ON LEFT WING FLAP. INSPECTEDSDR DXTA200500708Brake · leakingSPONGY BRAKES ON LANDING. FOUND BRAKE FLUID LEAKING FROM BRAKE ASSEMBLY AIRCRAFT RIGHT SIDE, REMOVED AND INSTALLED BRAKE ASSY, PERFORMED BRAKE BLEED NO DEFECTS NOTED IAW CE560 M/M 32-42-00.SDR DXTA200500654Odor · detectedUPON TAKEOFF ROLL RANCID BURNING OIL SMELL WAS EMITTING FROM GASPERS & VENTS.SDR DXTA200300002Hydromech Unit · leakingPOWER BRAKE LITE AND ANTI SKID INOP LITE ON IN FLIGHT.SDR 20000426SH033Counterweight · corrodedTHE LEFT AILERON PN 6524113-809, SN 258, HAD WEIGHTS (BALANCE) LOOSE IN THE INBOARD END CAP AND WERE BOUNCING AROUND LOOSE. THE LAST BALANCE WEIGHT CAME OFF OR PULLED THROUGH THE SMALL WASHER AND NUT THAT HOLD THE WEIGHT ON. THERE WAS SOME CORROSION, BUT NOT
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