# Service difficulty reports: N585QS

A list on [N585QS](https://openairdocs.org/aircraft/N585QS.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR DXTR2026092701](https://openairdocs.org/sdr/DXTR2026092701.md): Compressor Blade · cracked · Sep 27, 2026 · N585QS · Cessna 680A · Turbine Engine Compressor Section
  > RIGHT ENGINE, SECOND STAGE TURBINE BLADES FAILED BORESCOPE INSP, DUE TO CRACKS OUT OF LIMITS IAW EMM 72-00-00. R & R THE ENGINE IAW AMM 72-00-05, OPS CHKD GOOD.
- [SDR DXTA2025102205381](https://openairdocs.org/sdr/DXTA2025102205381.md): Anti-Skid Valve · faulty · Oct 20, 2025 · N585QS · Cessna 680A · Brake Anti-Skid Section
  > TAXIING OUT OF RAMP FELT BRAKES SLIP MOMENTARILY. ON RETURN TO RAMP, APPLIED BRAKES LIBERALLY AT TAXI SPEED AND GOT DISTINCT SLIPPAGE AGAIN WITH ASSOCIATED RIGHT YAW. BELIEVE THE LEFT BRAKE TO BE SLIPPING. DO NOT SEE ANY FLUID OR INDICATIONS OUT OF THE ORDI
- [SDR DXTA2025052803645](https://openairdocs.org/sdr/DXTA2025052803645.md): Brake · smoke · May 26, 2025 · N585QS · Cessna 680A · Landing Gear Brake System
  > LEFT MLG BRAKE: AFTER BLOCKING IN NOTICED SMOKE COMING FROM LEFT MAIN GEAR. THE LANDING AND TAXI WERE NORMAL WITH NORMAL BRAKING. NO LEAKS ARE VISIBLE. CORRECTIVE ACTION: PERFORMED VISUAL INSPECTION OF LEFT MLG BREAK ASSEMBLIES FOR CONDITION AND SECURITY. FO
- [SDR DXTA2024102800938](https://openairdocs.org/sdr/DXTA2024102800938.md): Battery · defective · Oct 24, 2024 · N585QS · Cessna 680A · Battery/Charger System
  > BATTERY OTEMP L RED CAS: SHORTLY AFTER TAKE OFF FROM TEB, BATT OTEMP L ILLUMINATED. CREW PERFORMED IMMEDIATE ACTION ITEM, RAN QRC AND QRH. BATTERY TEMP DECREASED AFTER L BATT WAS SELECTED OFF. FLIGHT RETURNED TO TEB. CORRECTIVE ACTION; REPLACED L/H NICAD BATTE
- [SDR DXTA2024102800939](https://openairdocs.org/sdr/DXTA2024102800939.md): None · no discrepancy · Oct 24, 2024 · N585QS · Cessna 680A · Standard Practices/Structures
  > OVERWEIGHT LANDING: DURING EMERGENCY RETURN TO TEB DUE TO BATT OTEMP L, WE LANDED OVER WEIGHT. WEIGHT AT LANDING WAS APPROXIMATELY 28,400 POUNDS. CORRECTIVE ACTION; PERFORMED HARD OR OVER WEIGHT LANDING INSPECTION AS PER CE680A CH, 05-50-00. FOUND NO ABNORMALI
- [SDR DXTA2024010810527](https://openairdocs.org/sdr/DXTA2024010810527.md): Unknown · unknown · Jan 5, 2024 · N585QS · Cessna 680A · Passenger/Crew Doors
  > MAIN DOOR: MAIN CABIN DOOR WILL NONLOCK CLOSED. PINS WILL NOT ENGAGE. PERFORMED CASIN DOOR LOCK FUNCTIONAL CHECK RESULTS SATISFACTORY IAW CESSNA 680A AMM 52-10-00. PERFORMEDCABIN DOOR INSPECTION CHECK PAYING PARTICULAR ATTENTION OF BAYONETS AND STRIKER PLATE
- [SDR DXTA2023120410226](https://openairdocs.org/sdr/DXTA2023120410226.md): Pump · faulty · Dec 3, 2023 · N585QS · Cessna 680A · Hydraulic Pump (Electric/Engine), Main
  > HYD VOLUME LOW AMBER CAS: AT FL410 ASKING NO DEMAND ON HYRAULIC SYSTEM WE GOT A HY VOLUME LOW AMBER CAS. DECLARED AN EMERGENCY AND DIVERTED TO IAD AIRPORT. USING THE CHECKLIST WE USED THE EMERGENCY GEAR EXTENSION FUNCTION AND BROUGHT THE AIRCRAFT TO A STOP ON
- [SDR DXTA2023101097570](https://openairdocs.org/sdr/DXTA2023101097570.md): Unknown · unknown · Oct 9, 2023 · N585QS · Cessna 680A · Emergency Lighting
  > AFT OVERHEAD READING LIGHT IN LAV IS INOP. THIS IS PART OF THE EMERGENCY LIGHT SYSTEM. VERIFIED DISCREPANCY. FOUND LIGHT UNPLUGGED. RECONNECTED LIGHT. OPS CHECKED GOOD IAW CE-680A AMM CHAPTER 33-50-00.
- [SDR DXTA2023030682100](https://openairdocs.org/sdr/DXTA2023030682100.md): Probe · defective · Mar 5, 2023 · N585QS · Cessna 680A · Fuel Indicating System
  > LEFT FUEL QUANTITY INDICATION: DURING DESCENT WE GOT FUEL IMBALANCE CAUTION. LEFT SIDE SHOWED 400 LBS LOW AND CONTINUED TO DROP. RAN CHECKLIST FOR IMBALANCE AND USED CROSSFEED OFF RIGHT SIDE. FUEL INDICATION CONTINUED TO DROP ON LEFT. ASSUMED FUEL LEAK AND LAN
- [SDR DXTA2022062764410](https://openairdocs.org/sdr/DXTA2022062764410.md): None · broken · Jun 21, 2022 · N585QS · Cessna 680A · Passenger/Crew Doors
  > PASSENGER / CREW DOORS: DOOR SUPPORT ARM. TELESCOPING ARM ON AFT OF DOOR. // SIGNOFF// REMOVED BROKEN SUPPORT STRUT ASSY P/N:7411332-26 INSTALLED CUSTOMER SUPPLIED NEW STRUT ASSY P/N:7411332-26 WORK DONE IN REF TO CE-680A AMM 52-10-00. OPS CHECK SATISFAC
- [SDR DXTA2021122754160](https://openairdocs.org/sdr/DXTA2021122754160.md): Thrust Washer · defective · Dec 25, 2021 · N585QS · Cessna 680A · Nose/Tail Landing Gear
  > NLG: DURING LANDING AT APPROXIMATELY 65 KNOTS, SEVERE NOSE WHEEL SHIMMY OCCURRED. UPON FURTHER SLOWING TO TAXI SPEED, NOSE WHEEL STEERING USING THE CONTROL WHEEL WAS ALSO INTERMITTENTLY LOST. THERE IS NO APPARENT HYDRAULIC LEAKAGE IN THE NOSE WHEEL AREA. // SI
- [SDR 2022F00117](https://openairdocs.org/sdr/2022F00117.md): Axle · nicked · Dec 4, 2021 · N585QS · Cessna 680A · Main Landing Gear
  > RIGHT MAIN LANDING GEAR AXLE HAS NICK THROUGH PLATING ON THE OUTBOARD SIDE, VERIFIED WITH COPPER SULFATE, INBOARD OF WASHER RETAINING GROOVE. NICK DETERMINED TO BE MINOR IN SCOPE. ACCOMPLISHED TEXTRON AVIATION ENGINEERING REPAIR MEMO DQ32732 DATED DECEMBER 4,
- [SDR 2021FA0000355](https://openairdocs.org/sdr/2021FA0000355.md): Brace · gouged · Dec 4, 2021 · N585QS · Cessna 680A · Fuselage Main, Structure
  > THE RIGHT-HAND MAIN LANDING GEAR SIDE BRACE ACTUATOR WAS GOUGED FROM CONTACTING THE ACTUATOR DURING GEAR OPERATION. REPAIR DEEMED MINOR IN SCOPE BY TEXTRON AVIATION ENGINEERING. REPAIR ACCOMPLISHED PER TEXTRON AVIATION ENGINEERING REPAIR MEMO DQ32693M1 DATED D
- [SDR 2022F00116](https://openairdocs.org/sdr/2022F00116.md): Brace · gouged · Dec 4, 2021 · N585QS · Cessna 680A · Main Landing Gear
  > THE LEFT-HAND MAIN LANDING GEAR SIDE BRACE ACTUATOR WAS GOUGED FROM CONTACTING THE ACTUATOR DURING GEAR OPERATION. REPAIR DEEMED MINOR IN SCOPE BY TEXTRON AVIATION ENGINEERING. REPAIR ACCOMPLISHED PER TEXTRON AVIATION ENGINEERING REPAIR MEMO DQ32693M1 DATED DE
- [SDR 2022F00115](https://openairdocs.org/sdr/2022F00115.md): Brace · gouged · Dec 4, 2021 · N585QS · Cessna 680A · Wing, Landing Gear Attach Fittings
  > THE LEFT-HAND MAIN LANDING GEAR SIDE BRACE ACTUATOR WAS GOUGED FROM CONTACTING THE ACTUATOR DURING GEAR OPERATION. REPAIR DEEMED MINOR IN SCOPE BY TEXTRON AVIATION ENGINEERING. REPAIR ACCOMPLISHED PER TEXTRON AVIATION ENGINEERING REPAIR MEMO DQ32693M1 DATED DE
- [SDR 2021FA0000231](https://openairdocs.org/sdr/2021FA0000231.md): Skin · corroded · Aug 10, 2021 · N585QS · Cessna 680A · Horizontal Stabilizer, Plate/Skin
  > HORIZONTAL STAB LH LOWER SKIN HAS MULTIPLE AREAS OF CORROSION ON THE TRAILING EDGE OF SKIN. REFERENCE TEXTRON AVIATION ENGINEERING MEMO DQ30952M1 DATED AUGUST 9TH 2021.
- [SDR DXTA2021071545270](https://openairdocs.org/sdr/DXTA2021071545270.md): Battery · inoperative · Jul 13, 2021 · N585QS · Cessna 680A · Emergency Lighting
  > CABIN EMERG LIGHT: OVERHEAD EMERGENCY LIGHT OVER SEAT 7 AND UNDER SEATS 5 AND 8 ARE INOPERATIVE. OVER WING EMERGENCY LIGHT IS ALSO INOPERATIVE. // SIGNOFF // GAINED ACCESS AND REMOVED EMERGENCY BATTERY #3 P/N CBS28-1 S/N 2171M AND INSTALLED CUSTOMER SUPPLIED
- [SDR DXTA2021070644720](https://openairdocs.org/sdr/DXTA2021070644720.md): Squat Switch · malfunctioned · Jul 5, 2021 · N585QS · Cessna 680A · Landing Gear Position and Warning
  > GEAR POSITION & WARNING: AFTER TAKE OFF WHILE THE LANDING GEAR WAS BEING RETRACTED A VERY LOUD VIBRATION OCCURRED. THE LANDING GEAR HANDLE WAS IN THE UP POSITION UNTIL THE ABNORMAL CHECKLIST CALLED FOR THE LANDING GEAR DOWN. ONCE AT A SAFE ALTITUDE THE GEAR I
- [SDR DXTA2021062844330](https://openairdocs.org/sdr/DXTA2021062844330.md): Switch · malfunctioned · Jun 26, 2021 · N585QS · Cessna 680A · Emergency Lighting
  > EMERGENCY LIGHTING: AFTER AIRCRAFT WAS POWERED DOWN, ALL EMERGENCY LIGHT SWITCHES OFF AND BATTERIES DISCONNECTED THE EMERGENCY LIGHT ABOVE THE MAIN CABIN DOOR AND BELOW SEAT 10 IS STILL ILLUMINATED. RESET #1 5G SWITCH AND LIGHTS EXTINGUISHED. OPS CHECKED EMER
- [SDR DXTA2019010301861](https://openairdocs.org/sdr/DXTA2019010301861.md): Unknown · odor · Jan 2, 2019 · N585QS · Cessna 680A · Air Distribution System
  > COCKPIT ODOR - DESCENDING THROUGH FL190 WE BEGAN TO SMELL AN EXHAUST ODOR THAT WAS STRONG ENOUGH SO MY SIC WHO WAS FLYING PUT ON HER MASK. I DID NOT WEAR A MASK AND DEVELOPED A SLIGHT HEADACHE FROM THE ODOR. DESCENDING THROUGH 10,000 FT THE SMELL SEEMED TO DI

## 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 = 'N585QS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N585QS/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.
