N571QS
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 = 'N571QS' 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 = 'N571QS' 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 DXTA2026092209809Lamp · inoperativeEMERGENCY EXIT SIGN UNDER LAV SEAT IS NOT ILLUMINATE. RECONNECTED LAV LAMP CONNECTOR. OPS CHECK GOOD. IAW MM 33-50-00.SDR DXTA2026091109638Flap System · malfunctionedDURING DECENT, FLAPS FAIL CAS MESSAGE DISPLAYED. THE FLAPS AND THE FLAP HANDLE WERE IN THE UP POSITION AND NO FLAP POSITION WAS SELECTED. FLAPS FAIL QRH COMPLETED. TECHS POWERED UP AND SENT THE ARES DATE. WE ALSO DID NOT RECEIVE ANY FLAP FAIL CAS. TECHS CYCLSDR DXTA2026080409072Door · out of alignmentMAIN CABIN DOOR WILL NOT OPEN UNLESS FORCE IS APPLIED TO DOOR HANDLE TO ASSIST THE DOOR DOWN. ALIGNMENT APPEARS TO BE OFF. RIGGED DOOR HINGE. OPS CHECK GOOD. IAW CE680A MM 52-10-00SDR 2026FA0000168Skin · debondedDISBONDS ON THE UPPER WINGS BETWEEN THE OUTBOARD END OF STRINGERS AND THE COMMON SKIN DOUBLERS. THE SKIN AND COMMON DOUBLERS MAY ALSO EXHIBIT A GRADUAL DEVIATION FROM CONTOUR IN THESE REGIONS. THE EXTENT OF THE DEFECT IS LOCATED USING ULTRASONIC INSPECTION ANDSDR DXTA2025082504682Stop Fitting · out of adjustMAIN CABIN DOOR LATCH REQUIRES MORE FORCE THAN NORMAL CLOSING. "CORRECTIVE ACTION" PERFORMED THE MAIN CABIN DOOR HEALTH CHECK/DATA COLLECTION CHECK LIST REFERENCING CESSNA MODEL 680A MAINTENANCE MANUAL CH 52-10-04 NOTING THAT THE INNER HANDLE DID NOT CONTACT TSDR DXTA2025042503215Door · malfunctionedTHE MAIN CABIN DOOR ONLY CLOSED HALF WAY BEFORE STOPPING AND COMING BACK DOWN. THE 2ND TRY IT WENT UP 3/4 OF THE WAY BEFORE STOPPING. WE USED THE OVERIDE SWITCH WITH THE NORMAL LUFT SWITCH AND THE DOOR CLOSED.SDR DXTA2025042203126Strut · inoperativeMAIN CABIN DOOR GAS STRUT INOP. DOOR FALLS WITHOUT ANY RESISTANCE. LIFT MOTOR INOP CORRECTIVE ACTION: WE HAD TO REMOVED INTERIOR TO GAIN ACCESS. REMOVED INOP MAIN DOOR GEAR MOTOR P/N GM50A-3 S/N 0101 AND INSTALLED REPAIRED GEAR MOTOR P/N GM50A-3 S/N 0122 IAW ASDR DXTA2025040702989Battery · no testDURING PREFLIGHT TEST, EMERGENCY LIGHT UNDER SEATS 3,5 AND 8 FAILED. PERFORMED EMERGENCY LIGHTS FAIL PREFLIGHT CHECKLIST. AFTER FIRST CHARGE ATTEMPT, SEATS 5 AND 8 CAME ON. AFTER SECOND CHARGE PERIOD, SEATS THREE LIGHT WAS STILL INOP. CORRECTIVE ACTION: MCC ELSDR DXTA2025040102852Light · malfunctionedCABIN EMERG LIGHT: SEAT 3 EMER LIGHT IS INOP AS WELL AS SEAT 3 AND SEAT 9 KICK PLATE EMER LIGHT INOP CORRECTIVE ACTION: PERFORMED A SATISFACTORY OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM WITH NO DEFECTS. WORK PERFORMED IN REF WITH CE-680A AMM 33-50-00.SDR DXTA2023102098360Module · faultedLEFT MLG LANDING GEAR RETRACTION: UNABLE TO RETRACT LANDING GEAR ON TAKE OFF UPON TAKE OFF THE LANDING GEAR HANDLE WAS LOCKED IN THE DOWN POSITION AND COULD NOT BE MOVED TO THE UP POSITION. NO CAS MESSAGES WERE DISPLAYED OR ANY OTHER INDICATIONS OF A PROBLEM SDR DXTA2023101397880Unknown · unknownLEFT MLG LANDING GEAR RETRACTION: AFTER TAKE OFF UNABLE TO RAISE GEAR (HANDLE WONT MOVE). AFTER 1-2 MINUTES, GEAR HANDLE MOVES AND RETRACTS NORMALLY. NO ISSUES WITH EXTENSION. COMPLIED WITH GVI OF NLG AND MLG ASSEMBLIES WITH NO DEFECTS. OF WOW SWITCHES WITH NSDR DXTA2023091595460Unknown · unknownMAIN DOOR: MAIN DOOR CLOSED, WHEN PULLING HANDLE DOWN THE HANDLE WILL NOT GO SMOOTHLY ALL THE WAY DOWN. IT STOPS HALF WAY AND WITH MORE PRESSURE IT THAN CAN BE PUSHED ALL THE WAY DOWN TO OPEN SAFELY. CLEANED AND LUBRICATED DOOR SHOOT BOLTS AND HANDLE HINGE PSDR DXTA2023052286710Unknown · unknownODORS IN COCKPIT / CABIN: ON THE DECENT, WE SELECTED THE ENGINE/STAB AND WING ANTI-ICE ON. MOMENTS LATER THE ODOR OF BURNING TOAST COULD BE NOTICED. IT WAS NOTICEABLE FROM THE OVER HEAD VENTS AS WELL. UPON TURNING OFF THE WING AND ENGINE/STAB ANTI-ICE THE ODORSDR DXTA2023051786410Unknown · unknownAFTER TAKEOFF, A STRONG ODOR OF BURNING. INSPECTED CABIN, & SMELL FOUND THROUGHOUT ACFT. AFTER CLEARING. PRESSURIZED W/CHERRY PICKER, BURNING ODOR RETURNED STRONGER. DIVERTED, & FIRE DEPART COULD NOT FIND SOURCE, AFTER F/D CLEARED ACFT, TURNED APU ON, & SESDR DXTA2022032358850None · brokenMAIN DOOR: MAIN CABIN DOOR IS SIGNIFICANTLY HARDER TO CLOSE THAN NORMAL. WHEN RAISING THE DOOR, THE LAST COUPLE OF INCHES THE DOOR BINDS AND BANGS TO A STUTTERED CLOSE. WHEN LOWERING THE DOOR, THE DOOR DOES NOT RELEASE INTO THE CONTROLLED FREEFALL UNTIL YOU HASDR 2022FA0000073Piccolo Tube · undersizeHORIZONTAL STABILIZER RH LEADING EDGE AFT BLEED AIR COUPLING LEAKING AT VERTICAL HOSE CONNECTIONSDR 2021F00306Web · crackedNOSE WHEEL WELL STRUCTURE IS CRACKING AT FS 75. DAMAGE IS OCCURING IN NOSE LANDING GEAR WHEEL WELL (NWW), FRAME WEB, AND DOUBLERS. ACCOMPLISHED TEXTRON AVIATION STANDARD REPAIR SR-680A-ATA53-25890 DATED: 6/1/2020, CRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NW
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