# Service difficulty reports: N584QS A list on [N584QS](https://openairdocs.org/aircraft/N584QS.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR DXTA2026071408796](https://openairdocs.org/sdr/DXTA2026071408796.md): Elec Connector · disconnected · Jul 12, 2026 · N584QS · Cessna 680A · Light System Wiring > LOWER LAV EXIT LIGHT DOES NOT ILLUMINATE. FOUND LOWER LAV EXIT LIGHT CONNECTOR NOT HOOKED UP. REATTACHED CONNECTOR. OPS CHECK GOOD. DONE IN ACCORDANCE WITH CESSNA 680A MM 33-50-01. - [SDR DXTA2026050707950](https://openairdocs.org/sdr/DXTA2026050707950.md): Anti-Ice Valve · faulted · May 5, 2026 · N584QS · Cessna 680A · Engine Anti-Icing System > DURING DESCENT WE SELECTED ALL A/I SYSTEMS ON FOR ICING CONDITIONS. ALL SYSTEMS OPERATED NORMALLY. UPON EXITING ICING CONDITIONS AT FL270, SELECTED ALL A/I SYSTEMS OFF. ABOUT 3 MINUTES AFTER SELECTING ALL A/I OFF, WE RECEIVED A/I ENGINE HOT R. ACCOMPLISHED - [SDR DXTA2025120105875](https://openairdocs.org/sdr/DXTA2025120105875.md): Squat Switch · out of rig · Nov 27, 2025 · N584QS · Cessna 680A · Landing Gear Position and Warning > UNABLE TO RETRACT LANDING GEAR AFTER TAKE OFF. GEAR HANDLE WOULD NOT MOVE. 3 GREEN INDICATED, WOW MISCOMPARE AMBER CAS DISPLAYED AFTER PASSING THROUGH APPROXIMATELY 1000 FT AND REMAINED DISPLAYED UNTIL PARKING THE AIRCRAFT. TROUBLESHOT NLG SQUAT SWITCH. FOUN - [SDR DXTA2025120105842](https://openairdocs.org/sdr/DXTA2025120105842.md): Squat Switch · faulted · Nov 25, 2025 · N584QS · Cessna 680A · Landing Gear Position and Warning > AFTER OUR TAKEOFF ROLL, WHEN AT THE INDICATION OF POSITIVE RATE OF CLIMB, THE GEAR HANDLE WAS MOVED TO THE GEAR UP POSITION. THOUGH THE HANDLE WAS EASILY MOVED TO THE UP POSITION THE LEFT MAIN, RIGHT MAIN AND NOSE GEAR DID NOT RETRACT. AT APPROXIMATELY 400 F - [SDR 2025FA0000509](https://openairdocs.org/sdr/2025FA0000509.md): Frame · cracked · Jul 21, 2025 · N584QS · Cessna 680A · Fuselage Miscellaneous Structure > A CRACK WAS FOUND ON THE LUG FOR DOOR STRUT ARM ON THE 7411351-8 SURROUND FRAME. ACCOMPLISHED FR-680A-139-15365 REV - DATED: 25-JUN-2025 - FIELD REPAIR - CRACK, FUSELAGE, AFT DOOR SURROUND FRAME, DOOR STRUT DRIVE ARM ATTACH. - [SDR DXTA2025052203559](https://openairdocs.org/sdr/DXTA2025052203559.md): Window · cracked · May 19, 2025 · N584QS · Cessna 680A · Flight Compartment Windows > FIRST OFFICER SIDE COCKPIT WINDOW CRACKED IN FLIGHT. CORRECTIVE ACTION: REMOVED CRACKED RH SIDE WINDOW P/N 9914809-2 S/N 21088H6054 AND INSTALLED CUSTOMER SUPPLIED NEW SIDE WINDOW P/N 9914809-2 S/N 24211H6471 IAW CE680A AMM 56-10-05. - [SDR DXTA2025050203311](https://openairdocs.org/sdr/DXTA2025050203311.md): Warning Message · illuminated · May 1, 2025 · N584QS · Cessna 680A · Fuel Controlling System > RECEIVED AMBER ENG CONTRL FAULT R IN CLIMB OUT. RAN QRH CHECKLIST. MESSAGE REMAINED FOR ENTIRETY OF FLIGHT. ARRIVED ON SITE AND GAINED ACCESS TO AIRCRAFT, PERFORMED ARES DOWNLOAD AND SENT TO TEXTRON FOR REVIEW. FOUND CAS MESSAGE TO BE RELATED TO THRUST REVER - [SDR DXTA2023082894090](https://openairdocs.org/sdr/DXTA2023082894090.md): Unknown · unknown · Aug 27, 2023 · N584QS · Cessna 680A · Doors > WHEN ATTEMPTING TO CLOSE THE MCD ON THE RAMP, THE DOOR WOULD GO UP, BUT THE HANDLE WILL NOT TURN TO ENGAGE PINS TO LOCK THE DOOR IN UP POSITION. THIS HAPPENS WHEN TRYING TO CLOSE FROM THE INSIDE OR OUTSIDE //SIGNOFF// INSPECTED DOOR LATCHING MECHANISM AND FOUN - [SDR DXTA2023062689280](https://openairdocs.org/sdr/DXTA2023062689280.md): Unknown · unknown · Jun 26, 2023 · N584QS · Cessna 680A · Emergency Lighting > CABIN EMERG LIGHT: THE NUMBER 3 SEAT LED AISLE LIGHTS DO NOT ILLUMINATE WHEN USING EMERGENCY POWER ONLY. REMOVED BATTERY PACKS. PERFORMED EMERGENCY LIGHTING BATTERY PACK POST-MAINTENANCE CHECK. POST MAINTENANCE CHECK GOOD, NO DISCREPANCIES NOTED. WORK DONE - [SDR 2023F00111](https://openairdocs.org/sdr/2023F00111.md): Skin · damaged · Apr 17, 2023 · N584QS · Cessna 680A · Fuselage Main, Plate/Skin > OBLONG HOLE IN RH NOSE SKIN REF ENGINEERING MEMO DQ37272M1. - [SDR 2023F00110](https://openairdocs.org/sdr/2023F00110.md): Skin · damaged · Apr 17, 2023 · N584QS · Cessna 680A · Fuselage Main, Plate/Skin > OBLONG HOLE IN RH NOSE SKIN REF ENGINEERING MEMO DQ37272M1. - [SDR 2023F00109](https://openairdocs.org/sdr/2023F00109.md): Skin · damaged · Apr 17, 2023 · N584QS · Cessna 680A · Fuselage Main, Plate/Skin > OBLONG HOLE IN RH NOSE SKIN REF ENGINEERING MEMO DQ37272M1. - [SDR 2023F00112](https://openairdocs.org/sdr/2023F00112.md): Fitting · corroded · Apr 17, 2023 · N584QS · Cessna 680A · Fuselage, Landing Gear Attach Fittings > NLG- ACTUATOR FITTING REPLEACEMENT REF (SR-680A-ATA53-33739) - [SDR DXTA2022072566590](https://openairdocs.org/sdr/DXTA2022072566590.md): Trunnion · defective · Jul 23, 2022 · N584QS · Cessna 680A · Fuselage, Landing Gear Attach Fittings > WHILE IN CRUISE AT FL380 THE NLG STARTED SLAMMING AROUND IN THE NLG BAY. NORMAL EXTENSION, EMERGENCY EXTENSION, & ALTERNATE EMERGENCY EXTENSION ALL FAILED TO PRODUCED A NLG GREEN INDICATION. LANDED WITH NLG IN WHEEL WELL. TROUBLESHOT NLG TO FIND THE ROOT CAU - [SDR DXTA2022071866160](https://openairdocs.org/sdr/DXTA2022071866160.md): Switch · out of rig · Jul 16, 2022 · N584QS · Cessna 680A · Landing Gear Retraction/Extension System > NLG ACTUATOR: DURING FLIGHT CLIMBING THROUGH 41600, WE STARTED HEARING AND FEELING A VERY LOUD AND CONTINUOUS BANGING UNDERNEATH OUR FEET. NO CASS MESSAGES WERE PRESENT OR ANY OTHER ABNORMAL INDICATION. BECAUSE THE BANGING SEAMED TO BE INTENSIFYING AND WOULD N - [SDR DXTA2022061964260](https://openairdocs.org/sdr/DXTA2022061964260.md): Harness · defective · Jun 19, 2022 · N584QS · Cessna 680A · Nose/Tail Landing Gear > NLG STRUT: WHILE CRUISING AT FL410, WE HEARD A LOUD THUMPING NOISE COMING FROM THE NOSE FOLLOWED BY "GEAR DISAGREE N" CAS MESSAGE. THE GEAR INDICATIONS SHOWED YELLOW HASH FOR THE NOSE AND WHITE UP FOR THE MAINS. DESCENDING THROUGH FL180, THE NOISE AND CAS ME - [SDR DXTA2022040859920](https://openairdocs.org/sdr/DXTA2022040859920.md): None · defective · Apr 7, 2022 · N584QS · Gulstm 680 · Emergency Lighting > CABIN EMERG LIGHT: THE FOLLOWING EMERGENCY LIGHTS ARE INOP. EXIT SIGN OVER SEAT 7, PATH LIGHT IN LAV AND ALSO THE READING LIGHT IN LAV. THESE LIGHTS ARE INOP WITH EMER LIGHT SWITCH IN ARM AND SHIPS BATTERIES OFF. // SIGNOFF //:REMOVED AND REPLACED THE #4 EMER - [SDR DXTA2022032358870](https://openairdocs.org/sdr/DXTA2022032358870.md): None · defective · Mar 22, 2022 · N584QS · Cessna 680A · Emergency Lighting > EMERGENCY LIGHTING: ALL EMERGENCY LIGHTS FUNCTION NORMALLY AND BRIGHTLY WITH THE EMER LTS SWITCH IN THE ON POSITION AND ALL OF THEM EXTINGUISH WHEN THE SWITCH IS MOVED TO THE ARM POSITION PRIOR TO TURNING ON THE BATTERIES. THEY SHOULD STAY ON UNTIL BATTERIES - [SDR DXTA2022020856410](https://openairdocs.org/sdr/DXTA2022020856410.md): Solenoid · defective · Feb 8, 2022 · N584QS · Cessna 680A · Passenger/Crew Doors > MAIN DOOR HANDLE: THE RED BUTTON ON THE MAIN CABIN DOOR HANDLE WILL NOT RELEASE THE HANDLE.///SIGN-OFF///REMOVED AND REPLACED FAULTY DOOR LATCH SOLENOID. PERFORMED CABIN DOOR CHECK REF CE680 MM 31-59-00 WITH NO DEFECTS. - [SDR DXTA2018070201144](https://openairdocs.org/sdr/DXTA2018070201144.md): Wheel · vibration · Jul 2, 2018 · N584QS · Cessna 680A · Wheel/Ski/Float > MLG VIBRATION AFTER RETRACTION, AIRCRAFT SHUDDERED VIOLENTLY CLIMBING THROUGH 7000'. VIBRATION FELT LIKE IT CAME FROM BELOW PILOT'S FEET. NO ABNORMAL GEAR INDICATIONS WERE NOTED. GEAR WAS NOT BLOWN DOWN. REMOVED AND REPLACED BOTH NLG WHEEL ASSYS (OFF) - LT 694 ## 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 = 'N584QS' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N584QS/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.