N572QS
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 = 'N572QS' 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 = 'N572QS' 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 DXTA2026101510167Pcb · defectiveDURING INITIAL CLIMBOUT CHECK DOORS AND CABIN DOOR OPEN CAS ILLUMINATED. SAME MESSAGES APPEARED DURING PREFLIGHT AND WERE CLEARED BY THE RESET PROCEDURE ACCOMPLISHED UNDER THE DIRECTION OF MAINTENANCE CONTROL. CORRECTIVE ACTION: REPLACED CED MONITOR PCB ASSEMBSDR DXTR2026090302Blades · crackedBLADE S/N PMOXM75 SUCTION SIDE CRACK .155 INCH. PRESSURE SIDE CRACK .407 INCH (OPEN) THROUGH COOLING HOLE WITH CRACK PRESENT ON TOP OF COOLING HOLE R&R ENGINE.SDR DXTR2026090301Rib · crackedFOUND CRACK ON THE PYLON RIB RT AFT FIREWALL REMOVED THE CRACKED RIB IAW SRM 51-40-05. MATCH DRILLED HOLES IN NEW RIB IAW SRM 51-40-05. COMPLETED MATCH DRILL OF NEW RIB AND INSTALLED IAW SRM 51-40-05.SDR DXTR2026090300192Rib · crackedFOUND CRACK IN PYLON RIB RIGHT AFT FIREWALL. REMOVED CRACKED RIB IAW SRM 51-40-05. MATCH DRILLED HOLES IN NEW RIB IAW SRM 51-40-05. COMPLETED MATCH DRILL OF NEW RIB AND INSTALLED TO RIGHT PYLON IAW SRM 51-40-05.SDR DXTR2026090201Compressor Blade · crackedFAULT: DURING 100 HR 2ND STAGE HPT BORESCOPE RE-INSPECT OF ENGINE, FOUND PREVIOUS CRACK ON SUCTION SIDE OF BLADE HAS MIGRATED BEYOND LIMITS. RESOLUTION: REMOVED ENGINE UNSERVICEABLE & RETURNED TO PWC FOR REPAIR.SDR DXTA2026060108258Filter · odorUPON DEPARTURE AFTER FLAP RETRACTION AT ABOUT 1000' NOTICED A STRONG BURNING SMELL IN COCKPIT AREA. DID NOT SEE SMOKE, LOOKED BACK IN CABIN AREA AND ALSO DID NOT SEE SMOKE, DID NOT GET ANY CAS MESSAGES NOR AUDIO WARNINGS , JUST A STRONG BURNING ODOR THAT STAYESDR 2026FA0000317Structure · corrodedACCOMPLISHED REMOVAL OF CORROSION TO AFFECTED AREAS OF VERTICAL STABILIZER. INSPECTED THE REMAINING MATERIAL USING ULTRASONIC TESTING AND EDDY CURRENT FOR CRACKS. NO CRACKS NOTED. ACCOMPLISHED DOUBLER REPAIR TO ONE NOTED LOCATION AND RESTORED FINISH TO ALL SURSDR 2026FA0000289Stringer · 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 DXTA2024060611975Light · inoperativeEMERGENCY LIGHT INOP UNDER LAV TOE KICK PANEL. GAINED ACCESS TO LAV RH VANITY EXIT INDICATOR TO CHECK FOR VOLTAGE AND PROPER INSTALLATION OF EXIT LIGHT ASSY. IAW AMM 33-50-00. ACCOMPLISHED OPS CHECK OPS CHECK GOOD.SDR DXTA2023062689390Unknown · unknownCABIN EMERG LIGHT: FORWARD EMERGENCY LIGHTS WILL NOT EXTINGUISH. VISUALLY INSPECTED #1 AND #2 BATTERY COMPARTMENT, NO DEFECT NOTED. VISUALLY INSPECTED ALL THE BREAKERS OF THE JBOX FROM THE CARGO BAY AREA NO DEFECT NOTED. REMOVED PANEL #244BR FROM THE COCKPIT SDR DXTA2022060263140None · noneFUSELAGE STRUCTURE: A VIBRATION ON THE FLOOR, UNDER OUT FEET AND ON THE GLARESHIELD IN COCKPIT WAS OBSERVED IN OUR CLIMBOUT @15000' AND ONCE LEVEL AT 17000' IT CONTINUED AS SPEED INCREASED TO @270KTS. WE SLOWED TO @250 AND IT SEEMED TO GET A LITTLE BETTER BUSDR DXTA2022050961420G Switch · failedCABIN EMERG LIGHT: LAV EMER LIGHT AND LAV "EXIT" EMER LIGHT WILL NOT EXTINGUISH. /// CORRECTIVE ACTION /// VERIFY DISCREPANCY FOUND EMERGENCY LIGHT ON LAV ON. RESET LAV EMERGENCY LIGHT BATTERY G-SWITCH AND RUN THE AIRCRAFT FOR 2 HOURS TO TOP CHARGE EMERGENCY LSDR 2021F00298Web · crackedTHE NOSE LANDING GEAR WHEEL WELL IS CRACKED ON LH AND RH SIDES AT APPROXIMATELY FS 75. CRACK DAMAGE IS TYPICALLY SEEN ON THE TOP WEB PN: 7413133-10, LH DOUBLER PN: 7413133-15, RH DOUBLER PN: 7413133-16, AND FRAME PN: 7413133-59. REPAIR ACCOMPLISHED IAW TEXTRONSDR 2021FA0000314Brace · gougedR/H MLG ACTUATOR SIDE BRACE FITTING (PN: 6922928-4) IS GOUGED FROM CONTACT WITH THE ACTUATOR. GOUGE IS ON THE INTERNAL SURFACE THAT DOES NOT HAVE A PROTECTIVE WEAR PLATE INSTALLED. IT WAS REPAIRED PER TEXTRON AVIATION ENGINEERING MEMO DQ32221M1 DATED NOV 3, 20SDR 2021F00297Brace · gougedL/H MLG ACTUATOR SIDE BRACE FITTING (PN: 6922928-3) IS GOUGED FROM CONTACT WITH THE ACTUATOR. GOUGE IS ON THE INTERNAL SURFACE THAT DOES NOT HAVE A PROTECTIVE WEAR PLATE INSTALLED. IT WAS REPAIRED PER TEXTRON AVIATION ENGINEERING MEMO DQ32221M1 DATED NOV 3, 20SDR 2021F00176Cover · corrodedRH ENGINE AGB REAR COVER HAS MULTIPLE AREAS OF CORROSION.SDR 2021F00175Cover · corrodedLH ENGINE AGB REAR COVER HAS MULTIPLE AREAS OF CORROSION.
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