N564QS
Service difficulty reports · 17
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 = 'N564QS' AND registry_match = 'registration' 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 = 'N564QS' AND registry_match = 'registration' 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 DXTA2026031707274Link · crackedWHILE ACCOMPLISHING SL680A-32-11 - LANDING GEAR - MAIN LANDING GEAR TRAILING LINK ENHANCED INSPECTION; SN: 27486606 LH, FOUND EVIDENCE OF CRACKS INSIDE THE LH TRAILING LINK WHICH COULD CONDEMN THE PART ACCORDING TO THE TOLERANCES CALLED OUT PER THE SERVICE LETSDR 2026FA0000125Angle · corrodedNOSE TUNNEL CORROSION.SDR 2026FA0000124Fastener · interferenceHI-LOC CLEARANCE AND INTERFERENCE.SDR DXTA2025070304089Starter Gen · vibrationCONSISTENT RESONANCE VIBRATION IN YOKE FLIGHT CONTROLS WITH AUTO PILOT ON AND OFF IN FAIRLY STABLE AIR. NOTICEABLE IN MULTIPLE SPEEDS AND PITCH ANGLES. CORRECTIVE ACTION: VISUALLY EXAMINED ALL TRIM TABS AND CONTROL SURFACES AND GEAR DOORS (WELGHT ON WHEELS) FSDR DXTA2025030502565Battery Pack · defectiveEXIT LIGHT ON EXTERIOR LAV WALL, EXIT LIGHT ON LAV KICK PANEL AND FLOOR LIGHT UNDER KICK PANEL DID NOT ILLUMINATE DURING CHECK. EMERGENCY LIGHTS BATTERY PACKS CHARGED FOR 1 HOUR PER AFM AND STILL FAILED CHECK. LIGHTS WILL ILLUMINATE ON SHIPS POWER. CORRECTIVE SDR DXTA2025021702333Battery Pack · no testEMERGENCY LIGHTING: #1 EMERGENCY BATTERY PACK DOESN'T HOLD A CHARGE OVERNIGHT.SDR DXTA2025012702093Downlock Switch · defectiveLEFT MLG LANDING GEAR RETRACTION: AFTER TAKE OFF WHEN WE RETRACTED THE LANDING GEAR WE GOT A LH MAIN GEAR DISAGREE CAS MSG WITH A X IN THE LH MAIN GEAR BOX. WE ALSO GOT AN ASSOCIATED SSD FAIL CAS MSG CORRECTIVE ACTION: REPLACED DOWN LOCK SWITCH. OPS CHECK GOODSDR DXTA2024061312026Trim System · faultedDURING CLIMB OUT AFTER TAKEOFF, WITH 1.2 NOSE DOWN STAB TRIM, EXPERIENCED SIGNIFICANT NOSE UP CONTROL PRESSURE. REQUIRING PILOT NOSE DOWN YOKE PRESSURE. LEVELED OFF AT 10,000 FT & SLOWED ACFT UNTIL NO PITCH CONTROL PRESSURES FELT. PRIMARY TRIM UNRESPONSIVSDR DXTA2023080792340Unknown · unknownLEFT MLG LANDING GEAR RETRACTION: AFTER TAKEOFF, THE LANDING GEAR HANDLE COULD NOT BE MOVED TO THE UP POSITION WHICH DID NOT ALLOW ALL 3 GEAR TO BE RETRACTED. AMBER WOW MISCOMPARE CAS MESSAGE DISPLAYED. RETURNED TO DEPARTURE AIRPORT. PERFORMED MLG OPS CHECK ISDR DXTA2023063089860Unknown · unknownEMERGENCY EXIT SIGN ON DIVIDING WALL BEHIND SEAT NUMBER 7 IS INOPERATIVE DURING EMER LTS CHECK. POWERED UP AC AND VERIFIED THAT THE EXIT SIDN IN THE LH AFT BULKHEAD DID NOT WORK PROPERLY REMOVED DEFECTIVE EXIT SIGN FROM THE LH AFT BULKHEAD PT#9919054-1 SN 17SDR DXTA2022052362420Limit Switch · intermittentCABIN EMERG LIGHT: DURING PREFLIGHT THE EMERGENCY LIGHTS SWITCH WAS SELECTED TO THE ARM POSITION: THE RELEVANT LIGHTS ILLUMINATED FOR A FEW SECONDS AND THEN WENT OFF. AFTER RUNNING THE APU FOR 1 HOUR THE TEST WAS REPEATED RESORTING IN THE SAME OUTCOME // SIGNOSDR DXTA2022031058300Pump · defectiveOIL PRESSURE LOW L RED CAS: DURING CRUISE NOTICED THE LEFT ENGINE OIL PRESSURE FLUCTUATING BETWEEN 45 AND 50 PSI. THEN WENT BELOW 36 PSI SO WE DISENGAGE THE AUTO THROTTLE AND SET THE N2 BELOW 88%. ON OUR DESCENT TO LAND WE HAD THE OIL PRESSURE LOW LEFT RED CASDR DXTA2021121653610Ring · missingPASSENGER / CREW DOORS: MAIN DOOR MOTOR ARM DISCONNECTED FROM THE DOOR. // SIGNOFF// MAIN DOOR MOTOR ARM RING WAS MISSING WHICH ALLOWED THE ARM TO DISCONNECT. OREDERED NEW WASHER PIN AND RING AND REPLACED THEM WITH CUSTOMER SUPPLIED PARTS. ALL WORK DONE IAW CSDR 2021F00273Fitting · chafedREPAIR OF LEFT AND RIGHT MAIN LANDING GEAR SIDE BRACE ACTUATOR INBOARD FITTING(S) CHAFE DAMAGE PER TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ31258M1 DATED: 08/27/2021.SDR 2021F00078Tail Cone · gougedFORWARD (LEFT) TAILCONE SKIN DAMAGE (GOUGE/BAR MARK). REF ENGINEERING MEMO DQ29509M1SDR DXTA2020021303450Handle · defectiveFLAPS FAIL AMBER CAS ILLUMINATED - ON APPROACH FLAPS WERE SELECTED TO 2. FLAPS DID NOT MOVE AND HAD A FLAPS FAIL EICAS MESSAGE. DID THE FLAPS FAIL APPROACH CHECKLIST. FLAPS FAIL MESSAGE STAYED ILLUMINATED. COMPLETED FLAP FAIL APPROACH AND LANDING CHECKLISTSDR 2019FA0000390Step · damagedCABIN DOOR TOP STEP THREADED HOLE DAMAGE. REFERENCE TEXTRON AVIATION ENGINEERING MEMO REF: DQ24022M1 DATED DEC. 4, 2019.
Back to N564QS