# Service difficulty reports: N586QS A list on [N586QS](https://openairdocs.org/aircraft/N586QS.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR DXTA2026061608458](https://openairdocs.org/sdr/DXTA2026061608458.md): Brake Assy · faulted · Jun 15, 2026 · N586QS · Cessna 680A · Landing Gear Brake System > AFTER TAXIING IN TO A STOP ON THE RAMP POST LANDING THE MAIN BRAKES WILL EXTENSIVELY VIBRATE FROM A SLOW SPEED UNTIL COMING TO A COMPLETE STOP. CHECKED ALL BRAKE PINS AND EVERYTHING LOOKED GOOD. CHECKED THE BRAKES THEMSELVES AND DIDN'T SEE ANY UNUSUAL WEAR. - [SDR 2026FA0000252](https://openairdocs.org/sdr/2026FA0000252.md): Spar Cap · corroded · Apr 6, 2026 · N586QS · Cessna 680A · Wing Spar > RH WHEEL WELL AFT LOWER SPAR CAP CORROSION. - [SDR DXTA2025112605839](https://openairdocs.org/sdr/DXTA2025112605839.md): Battery Pack · failed · Nov 25, 2025 · N586QS · Cessna 680A · Emergency Lighting > ARM LIGHT TEST FAIL MULTIPLE TIMES, TRIED UNSUCCESSFUL RECHARGE PROCEDURE. REPLACED BATTERY PACKS. OPS CHECK GOOD. IAW CESSNA CE-680A AMM 33-50-06 - [SDR DXTA2025032502777](https://openairdocs.org/sdr/DXTA2025032502777.md): Engine · malfunctioned · Mar 21, 2025 · N586QS · Cessna 680A · Fire Detection > CLIMBING OUT OF KHPN ABOUT TO LEVEL AT 5000 FT WE RECIEVED A RIGHT RED ENGINE FIRE WARNING. BEFORE I COULD RUN THE CHECKLIST THE LIGHT AND WARNING EXTINGUISHED. I BELIEVE IT WAS FROM THE THEOTTLE RETARDING AT LEVEL OFF. NOTICED THE ITT ON THE RIGHT ENGINE WO - [SDR DXTA2025011501959](https://openairdocs.org/sdr/DXTA2025011501959.md): Steering Unit · defective · Jan 13, 2025 · N586QS · Cessna 680A · Landing Gear Steering System > UPON LANDING WHILE ATTEMPTING TO EXIT THE RUNWAY LEFT AND RIGHT TILLER STEERING APPEARED TO BE INOP. REPLACED NWS UNIT. OPS CHECK/LEAK CHECK GOOD. IAW CE-680A AMM 32-50-50 - [SDR DXTA2024120201318](https://openairdocs.org/sdr/DXTA2024120201318.md): Light · defective · Nov 27, 2024 · N586QS · Cessna 680A · Emergency Lighting > ON POST FLIGHT WALK NOTICED THE SMALLER EMER LIGHT ON THE RIGHT SIDE OVER WING LIGHT IS VERY DIM AND FLICKERING. CORRECTIVE ACTION; REMOVED OVER WING EMER LIGHT INSTALLED NEW OVER WING EMER LIGHT OPS CHECK GOOD. NO DEFECTS NOTED. REF. CE 680A AMM 33-50-20. - [SDR DXTA2023092596250](https://openairdocs.org/sdr/DXTA2023092596250.md): Unknown · unknown · Sep 23, 2023 · N586QS · Cessna 680A · Passenger/Crew Doors > MAIN DOOR: MAIN CABIN DOES NOT OPEN NORMALLY. REQUIRES PUSH TO OPEN. //SIGNOFF// COULD NOT DUPUCATE DISCREPANCY. DOOR OPENS AND CLOSES AS INTENDED. CHECKED RIG OF DOOR PER CE-680A MM 52-10-00 FOUND DOOR RUBBING SUGHTLY ON AFT RUB BLOCK REMOVED SHIMS FROM RUB B - [SDR DXTA2023092696190](https://openairdocs.org/sdr/DXTA2023092696190.md): Unknown · unknown · Sep 22, 2023 · N586QS · Cessna 680A · Passenger/Crew Doors > MAIN DOOR: MAIN CABIN DOOR DIFFICULT TO OPEN. // SIGNOFF// INSPECTED MAIN CABIN DOOR FOR ANY DAMAGE AND NO DEFECTS NOTED, PERFORMED SERVERAL SATISFACORY OPS CHECKS OF MAIN CABIN DOOR, NO DIFFICULTY NOTED OPENING AND CLOSING FROM INSIDE AND OUTSIDE I/A/W CE·680 - [SDR DXTA2023072791810](https://openairdocs.org/sdr/DXTA2023072791810.md): Unknown · unknown · Jul 27, 2023 · N586QS · Cessna 680A · Air Distribution System > AT FL400, LOUDRUSH OF AIR NOISE SIMILAR TO THE NOISE MADE WHEN DOING PRESSURIZATION SYSTEM CHECKS CAME ON CONTINUOUSLY. NOISE CONTINUES NON STOP WHILE ON GROUND, AND A BURNING ODOR NEAR LAVATORY & REAR CABIN. RAN APU & ENGINES WITH BLEED ON, NO DEFECTS OR - [SDR DXTA2022103173060](https://openairdocs.org/sdr/DXTA2022103173060.md): Unknown · unknown · Oct 31, 2022 · N586QS · Cessna 680A · Standard Practices/Structures > A VIBRATION OF UNDETERMINED LOCATION. COULD BE FELT THROUGH OUT THE ENTIRE AIRCRAFT. SEEMS TO LESSEN WITH SPEED BUT NEVER GOES AWAY. VIBRATION OCCURRED CLIMBING OUT OF 3000 WITH THE FLAPS & GEAR UP. REMAINED THROUGHOUT THE ENTIRE FLIGHT UNTIL LANDING. BUT IT - [SDR DXTA2022021156570](https://openairdocs.org/sdr/DXTA2022021156570.md): Not Reported · not reported · Feb 10, 2022 · N586QS · Cessna 680A · Emergency Lighting > FLOOR EMERG EXIT LIGHT: THE TOE KICK LIGHTING UNDER THE LAV SEAT IS INOPERATIVE. THE LIGHTS DO NOT OPERATE WITH EMERGENCY BATTERY POWER OR WITH MAIN SHIPS POWER.///SIGN-OFF///FOUND TOE KICK LIGHTING CONNECTOR DISCONNECTED. RECONNECTED TOE KICK CONNECTOR. OPS - [SDR 2021F00248](https://openairdocs.org/sdr/2021F00248.md): Skin · corroded · Aug 11, 2021 · N586QS · Cessna 680A · Wing, Plate/Skin > REPAIR TO LH WING LOWER SKIN CORROSION. TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ30944M1 REV. A DATED: 8/11/2021, LEFT WING EXTENSION DAMAGE (CORROSION). - [SDR 2021F00244](https://openairdocs.org/sdr/2021F00244.md): Skin · chafed · Aug 11, 2021 · N586QS · Cessna 680A · Fuselage Main, Plate/Skin > LWR SKIN CHAFE FROM ANTI - ICE CROSSFLOW VALVE. ACCOMPLISHED TEXTRON AVIATION STANDARD REPAIR SR-680A-ATA53-22175 DATED 07/15/2019, STANDARD REPAIR - 680A ALL S/N LWR SKIN CHAFE FROM ANTI - ICE CROSS-FLOW VALVE. WITH FAA FORM 8100-9 DATED 07/19/2019. COMPLETE - [SDR 2021F00242](https://openairdocs.org/sdr/2021F00242.md): Skin · corroded · Aug 11, 2021 · N586QS · Cessna 680A · Wing, Plate/Skin > REPAIR TO LH WING LOWER SKIN CORROSION. TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ30944M1 DATED 8/4/2021, LEFT WING EXTENSION DAMAGE (CORROSION). - [SDR DXTA2021061643760](https://openairdocs.org/sdr/DXTA2021061643760.md): Acm · contaminated · Jun 15, 2021 · N586QS · Cessna 680A · Cabin Cooling System > ODORS IN COCKPIT / CABIN: CLEAR ACM INTAKE AND INTAKE DUCTS OF CICADAS. CLEAN CICADA DEBRIS FROM APU INTAKE DUCT AND ASSOCIATED AREAS. ALL INSECT DEBRIS HAS BEEN REMOVED AND RESTORED AIRCRAFT TO ORIGINAL CONDITION CLEAR ACM INTAKE AND INTAKE DUCTS OF CICADAS. - [SDR DXTA2020121404466](https://openairdocs.org/sdr/DXTA2020121404466.md): Unknown · odor · Dec 14, 2020 · N586QS · Cessna 680A · Air Distribution System > DURING CLIMB OUT NOTICED AN UNIDENTIFIED ODOR IN THE COCKPIT. THERE WAS NO SIGN OF SMOKE. ANTI ICE WAS OFF AND CLIMB POWER WAS SET. ALL ELECTRICAL INDICATIONS WERE NORMAL AND AIR CONDITIONING SUPPLY TEMPERATURES WERE NORMAL. SIGNOFF. PERFORMED ENGINE RUN - [SDR 2020F00327](https://openairdocs.org/sdr/2020F00327.md): Doubler · cracked · Jul 9, 2020 · N586QS · Cessna 680A · Fuselage Miscellaneous Structure > CRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW), FRAME, WEB, AND DOUBLERS, FS 75. ACCOMPLISHED FIELD REPAIR SR-680A-ATA53-25890 REV- DATED JUNE 1, 2020 AND 8100-9 DATED 6/1/2020; STANDARD REPAIR - CRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW), FRAME, WEB, ## 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 = 'N586QS' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N586QS/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.