# Service difficulty reports: N572QS A list on [N572QS](https://openairdocs.org/aircraft/N572QS.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR DXTA2026102610333](https://openairdocs.org/sdr/DXTA2026102610333.md): Door · malfunctioned · Oct 23, 2026 · N572QS · Cessna 680A · Passenger/Crew Doors > MAIN ENTRANCE DOOR IS EXTREMELY DIFFICULT TO CLOSE FROM INTERIOR, TAKES BOTH HANDS AND GREAT EFFORT TO CLOSE. - [SDR DXTA2026101510167](https://openairdocs.org/sdr/DXTA2026101510167.md): Pcb · defective · Oct 13, 2026 · N572QS · Cessna 680A · Door Warning System > DURING 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 ASSEMB - [SDR DXTR2026090302](https://openairdocs.org/sdr/DXTR2026090302.md): Blades · cracked · Sep 3, 2026 · N572QS · Cessna 680A · Turbine Section > BLADE 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 DXTR2026090301](https://openairdocs.org/sdr/DXTR2026090301.md): Rib · cracked · Sep 3, 2026 · N572QS · Cessna 680A · Nacelle/Pylon, Frame/Spar/Rib > FOUND 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 DXTR2026090300192](https://openairdocs.org/sdr/DXTR2026090300192.md): Rib · cracked · Sep 3, 2026 · N572QS · Cessna 680A · Nacelle/Pylon, Frame/Spar/Rib > FOUND 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 DXTR2026090201](https://openairdocs.org/sdr/DXTR2026090201.md): Compressor Blade · cracked · Sep 2, 2026 · N572QS · Cessna 680A · Turbine Engine Compressor Section > FAULT: 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 DXTA2026060108258](https://openairdocs.org/sdr/DXTA2026060108258.md): Filter · odor · May 28, 2026 · N572QS · Cessna 680A · Air Distribution System > UPON 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 STAYE - [SDR 2026FA0000317](https://openairdocs.org/sdr/2026FA0000317.md): Structure · corroded · May 4, 2026 · N572QS · Cessna 680A · Vertical Stabilizer > ACCOMPLISHED 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 SUR - [SDR 2026FA0000289](https://openairdocs.org/sdr/2026FA0000289.md): Stringer · debonded · Apr 23, 2026 · N572QS · Cessna 680A · Wing, Longeron/Stringer > DISBONDS 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 AND - [SDR DXTA2024060611975](https://openairdocs.org/sdr/DXTA2024060611975.md): Light · inoperative · Jun 6, 2024 · N572QS · Cessna 680A · Emergency Lighting > EMERGENCY 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 DXTA2023062689390](https://openairdocs.org/sdr/DXTA2023062689390.md): Unknown · unknown · Jun 26, 2023 · N572QS · Cessna 680A · Emergency Lighting > CABIN 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 DXTA2022060263140](https://openairdocs.org/sdr/DXTA2022060263140.md): None · none · Jun 2, 2022 · N572QS · Cessna 680A · Fuselage Main, Structure > FUSELAGE 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 BU - [SDR DXTA2022050961420](https://openairdocs.org/sdr/DXTA2022050961420.md): G Switch · failed · May 6, 2022 · N572QS · Cessna 680A · Emergency Lighting > CABIN 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 L - [SDR 2021F00298](https://openairdocs.org/sdr/2021F00298.md): Web · cracked · Nov 5, 2021 · N572QS · Cessna 680A · Fuselage Main, Bulkhead > THE 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 TEXTRON - [SDR 2021FA0000314](https://openairdocs.org/sdr/2021FA0000314.md): Brace · gouged · Nov 5, 2021 · N572QS · Cessna 680A · Main Landing Gear Attach Section > R/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, 20 - [SDR 2021F00297](https://openairdocs.org/sdr/2021F00297.md): Brace · gouged · Nov 5, 2021 · N572QS · Cessna 680A · Main Landing Gear Attach Section > L/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, 20 - [SDR 2021F00176](https://openairdocs.org/sdr/2021F00176.md): Cover · corroded · Jun 25, 2021 · N572QS · Cessna 680A · Accessory Gearboxes > RH ENGINE AGB REAR COVER HAS MULTIPLE AREAS OF CORROSION. - [SDR 2021F00175](https://openairdocs.org/sdr/2021F00175.md): Cover · corroded · Jun 25, 2021 · N572QS · Cessna 680A · Accessory Gearboxes > LH ENGINE AGB REAR COVER HAS MULTIPLE AREAS OF CORROSION. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/aircraft/N572QS/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.