N326QS, cancelled Sep 18, 2013
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 = 'N326QS' AND deregistration_id = 'N326QS-2013-09-18' 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 = 'N326QS' AND deregistration_id = 'N326QS-2013-09-18' 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 DXTA2012030904911Squat Switch · out of adjustAFTER TAKEOFF, GEAR WOULD NOT RETRACT. UNABLE TO MOVE GEAR HANDLE. FOUND LT MAIN SQUAT SWITCH ON OUTER LIMITS OF ADJUSTMENT AND OUT OF RIG. ADJUSTED SQUAT SWITCH IAW MM 32-61-00, OPS CHECKED NORMAL.SDR DXTA2011050204569Pitot Tube · obstructedON TAKEOFF ROLL, ABORTED TAKEOFF FOR NO AIRSPEED INDICATION ON PILOTS PFD. REMOVED PILOT'S PITOT TUBE. REMOVED SAND FROM PITOT TUBE PURGED PITOT LINE FROM PILOT'S MADC TO PITOT TUBE. NO DEBRIS NOTED. RESECURED PITOT LINES AND TUBE. SECURED ACCESS. PITOT HSDR DXTA2009022003516Brake Sys · failedPOWER BRAKE FAILED WHILE TAXIING FOR TAKEOFF.SDR DXTA2009021903516Pressure Switch · stickingFOUND THE 900-1300 PSI SWITCH STICKING. REMOVED SWITCH PN 1206P27, SN 3568 AND INSTALLED SWITCH PN 1206P27, SN 3751. PERFORMED COMPLETE BRAKE SYS BLEED. PERFORMED 2-0 MILE TAXI CHECK AND ACCEL/STOP FROM 45KTS. BRAKES AND INDICATION ALL NORMAL. WORK DONE ISDR DXTA200808113223Brake Assy · malfunctionedAFTER LANDING, AT ABOUT 20 KNOTS THE BRAKES LOST ABOUT HALF THEIR CONTROL PRESSURE AND BRAKING EFFECTIVENESS IS QUESTIONABLE. LAST FOR ABOUT 1 SECOND AND BRAKES RETURN TO NORMAL. INSPECTED BRAKE SYS AND BLEED BRAKE SYS NO DEFECTS FOUND OPS CK GOOD IAW TC-560-3SDR DXTA20080811Brake Sys · contaminatedAFTER LANDING, AT ABOUT 20 KNOTS THE BRAKES LOOSE ABOUT HALF THEIR CONTROL PRESSURE AND BRAKING EFFECTIVENESS IS QUESTIONABLE. LAST FOR ABOUT 1 SECOND AND BRAKES RETURN TO NORMAL. INSPECTED BRAKE SYS AND BLEED BRAKE SYS NO DEFECTS FOUND. OPS CK GOOD IAW TC-56SDR DXTA200803223Brake · weakAFTER LANDING, AT ABOUT 20 KNOTS, THE BRAKES LOST ABOUT HALF THE CONTROL PRESSURE AND BRAKING EFFECTIVENESS. (S)SDR DXTA200803206Brake Assy · malfunctionedEXCESSIVE AMOUNT OF BRAKE PEDAL APPLICATION IS NEEDED TO STOP AIRPLANE. INSP BRAKE SYSTEM FOR LEAKS. NO LEAK DETECTED AT THIS TIME. PERFORMED BRAKE BLEEDING PROCEDURES PER MM 32-42-00 AND MEMO M344-08-10. TAXIED ACFT ABOVE 15 KTS FOR BRAKE OP'S CHECKS. SYSSDR DXTA200702460Starter Gen · trippedDURING TAKEOFF POWER APPLICATION, LT GENERATOR TRIPPED OFF LINE (LOW SPEED ABORT). VISUALLY INSPECTED LH GENERATOR WIRING. ALL CONNECTIONS TIGHT. RAN BOTH ENGINES WITH GENERATOR SELECTED ON. CYCLED RT GEN OFF AND VERIFIED LT TOOK LOAD ON AMP METER. GENERSDR DXTA200601743Brake Assy · weakSOFT BRAKE PEDALS ON BOTH SIDES. BLEED THE BRAKE SYSTEM AND INSTALLED NEW PACKINGS ON BLEED FITTING NAS1612-4. OPS OK. WORK DONE IAW CH 32-42-00 OF MM. LEAK CHECK GOOD. NO LEAKS NOTED.SDR DXTA200601587Wheel · damagedRT MAIN TIRE BLEW ON LANDING ROLLOUT. EVIDENCE OF WHEEL LOCK FROM TIRE DAMAGE. REMOVED WHEEL ASSY P/N 3-1490-1, S/N 3844 AND INSTALLED WHEEL ASSY P/N 3-1490-1, S/N 2334 WHILE PLANE WAS STUCK ON RUNWAY. PILOTS REPORTED BRAKES REMAINED ENGAGED WHILE RELEASINGSDR DXTA200601296Brake · malfunctionedUPON LANDING APPLIED BRAKES AT APPROX, 90-100 KTS, BOTH BRAKE PEDALS ON CAPTAIN SIDE FELT HARD AND NO EFFECTIVE BRAKE ACTION FOR 3 SEC, THEN BRAKES FELT NORMAL AND BRAKE ACTION RESUMED. REMOVED AND INSPECTED BOTH LEFT AND RIGHT WHEEL SPEED TRANSDUCERS INSPECTSDR DXTA200500929Engine · inoperativeDURING ENGINE START, THE RIGHT ENGINE HAD NORMAL START, LEFT ENGINE STARTED, ENGINE ACCELERATED THRU 52 PERCENT AND WOULD NOT SHUT OFF WITH THRUST LEVER IN CUT OFF. HAD TO SHUT ENGINE DOWN USING FIREWALL SHUTOFF. MAX N1 103.5%, N2 OVERSPEED, DID NOT NOTICE ASDR DXTA200500563Brake · malfunctionedBRAKES WORKED NORMALLY AFTER LANDING, AS AIRCRAFT DECELERATED THROUGH APPROXIMATELY 20 KTS, THE BRAKES FAILED. BRAKE PRESSURE RECOVERED WHEN BRAKE PEDALS WERE PUMPED. REMOVED AND REPLACED LEFT AND RIGHT WHEEL ANTI-SKID TRANSDUCERS AFTER TROUBLESHOOTING SYSTESDR DXTA200300162Control Lever · looseRIGHT HAND THRUST REVERSER LEVER VERY LOOSE, DEPLOYED BY ITSELF DURING TAXI. INSPECTED ENGINE CONTROL AND THRUST REVERSER LEVER SPRING PLUNGER LOOSE, TIGHTEN RT THRUST REVERSER LEVER SPRING PLUNGER IAW CE560 MAINTENANCE MANUAL CHAPTER 78-31-00, OPS CHECK GOODSDR 99ZZZX4489Wheel · mismanufacturedWHEEL WAS DISASSEMBLED FOR TIRE REPLACEMENT. DURING INSPECTION, FOUND THAT NO HOLES HAD BEEN DRILLED INTO WHEEL HALF INSIDE DIAMETER FOR THERMAL RELIEF. THERMAL RELIEF PLUGS, AND BORES WERE INSTALLED NORMALLY. FIRST TIRE REPLACEMENT SINCE NEW.
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