# Service difficulty reports: N368QS, cancelled Jul 26, 2025

A list on [N368QS, cancelled Jul 26, 2025](https://openairdocs.org/deregistered/N368QS-2025-07-26.md).

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

- [SDR DXTA2025032402799](https://openairdocs.org/sdr/DXTA2025032402799.md): Cable · out of adjust · Mar 23, 2025 · N368QS · Cessna 680SOV · Passenger/Crew Doors
  > MAIN DOOR: WHEN OPENING MAIN CABIN DOOR IT LOWERS AT AN ABNORMALLY RAPID RATE. WHEN CLOSING THE DOOR, DOOR FEELS ABNORMALLY HEAVY WHEN PULLING IT ONTO THE PRECATCH. INTERNAL TENSION SEEMS NOT TO BE PROPERLY ADJUSTED. CORRECTIVE ACTION; ADJUSTED MED CABLE TENSI
- [SDR DXTA2024120501384](https://openairdocs.org/sdr/DXTA2024120501384.md): Processor · defective · Dec 3, 2024 · N368QS · Cessna 680SOV · Autopilot System
  > ON CLIMB OUT THE AUTO PILOT A AND B FAILED, WE RECEIVED A CYAN CASS MESSAGE. NOTICED THE AIRCRAFT WAS TRIMMED TO THE LEFT ON AILERON. WHEN TRYING TO TRIM TO THE RIGHT THE LEFT AILERON TRIM WOULDN¿T MOVE. AFTER SEVERAL ATTEMPTS WE WERE ABLE TO GET IT RECENTE
- [SDR 2024FA0000815](https://openairdocs.org/sdr/2024FA0000815.md): Skin · corroded · Nov 4, 2024 · N368QS · Cessna 680CE · Fuselage Main, Plate/Skin
  > REPAIRED THE CORRODED AREAS OF THE FUSELAGE SKIN LOCATED UNDER AND ADJACENT TO THE AFT CHIN FAIRING (WING-TO FUSELAGE FAIRING) BY BLENDING CORRODED AREAS, PERFORMING NDT AND REPORTING FOR REPAIR DISPOSITION, FABRICATING AND INSTALLING REPAIR DOUBLERS IN ACCORD
- [SDR 2024FA0000784](https://openairdocs.org/sdr/2024FA0000784.md): Closeout Panel · corroded · Oct 22, 2024 · N368QS · Cessna 680CE · Passenger/Crew Doors
  > MECHANICALLY REMOVED 11 AREAS OF CORROSION WITH AN ADDITIONAL 4 AREAS LOCATED ON MED INNER/LOWER CLOSE-OUT PANEL OUTER SURFACE, PERFORMED NDT, AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED AND PRIMED BLENDED AREAS PER NETJETS ENGINEERING TECHNICAL SERV
- [SDR DXTA2023070390280](https://openairdocs.org/sdr/DXTA2023070390280.md): Unknown · unknown · Jul 3, 2023 · N368QS · Cessna 680CE · Fuselage Structure (General)
  > VIBRATION IN AIRFRAME OR ENGINE. TAKE OFF WAS NORMAL COMING THROUGH 5000FT I STARTED TO NOTICE WHAT SEEMED LIKE LIGHT CHOP. CONTINUED CLIMB UP TO 15000FT LEVELED OFF AND IMEDIATLY NOTICED VIBRATION. THERE WAS NO CAS MESSAGE. WE RAN THE ENGINE VIBRATION CHECK
- [SDR DXTA2023060788130](https://openairdocs.org/sdr/DXTA2023060788130.md): Coalescer Bag · dirty · Jun 7, 2023 · N368QS · Cessna 680CE · Air Conditioning System
  > ON DESCENT OUT OF 25000 BOTH CREW COULD SMELL AN ACIDIC ODOR IN COCKPIT & SLIGHT HAZE IN CABIN. RAN THE CHECKLISTS. LANDED AT DESTINATION. INSPECTED APU INLET FOR CONTAMINATION. FOUND OIL DRIPPING FROM APU COMPRESSOR DRAIN LINE. APU WAS PLACED ON MB. PRIOR
- [SDR DXTA2023060688010](https://openairdocs.org/sdr/DXTA2023060688010.md): Unknown · unknown · Jun 6, 2023 · N368QS · Cessna 680SOV · Air Conditioning System
  > SMOKE IN COCKPIT / CABIN: AFTER STARTING APU AND TURNING ON BLEED AIR THE APU DID NOT HAVE THE NORMAL SOUND TO IT I LOOKED OUTSIDE AND THE PERSONNEL WAS LOOKING AT THE BACK OF THE PLANE AND SHORTLY AFTER THE COCKPIT AND CABIN FILLED WITH SMOKE AND THE APU AUTO
- [SDR DXTA2023051085740](https://openairdocs.org/sdr/DXTA2023051085740.md): Unknown · unknown · May 9, 2023 · N368QS · Cessna 680CE · Emergency Lighting
  > CABIN EMERG LIGHT: DURING POSTFLIGHT, FOUND MULTIPLE EMERGENCY LIGHTS INOPERATIVE IN THE AFT SECTION OF THE AIRCRAFT. REMOVED AND REPLACED #2 AND #4 EMERGENCY BATTERY PACK IAW CE-680A M/M 33-50-10. OPS CHECK GOOD.
- [SDR DXTA2022072966940](https://openairdocs.org/sdr/DXTA2022072966940.md): Battery · defective · Jul 29, 2022 · N368QS · Cessna 680A · Emergency Lighting
  > CABIN EMERG LIGHT: EMERGENCY LIGHTS FAIL TEST WITH SWITCH IN ARM AND MAIN BATTERIES OFF. THEY DO NOT ILLUMINATE. RAN APU FOR 20 MINS WITH SAME RESULT. // SIGNOFF // REMOVED BATTERY CHARGER SYSTEM PN:CBS28·1 SN:2698M INSTALLED CUSTOMER SUPPLIED BATTERY CHARGER
- [SDR DXTA2021052442470](https://openairdocs.org/sdr/DXTA2021052442470.md): Blade · missing · May 22, 2021 · N368QS · Cessna 680CE · Engine (Turbine/Turboprop)
  > ENGINE VIBRATION R RED CAS: WHILE CLIMBING TO FL340 IN VMC, AT ABOUT FL320 WE HEARD A LOUD BANG AND SHORTLY AFTER WE HAD THE ENGINE VIBRATION R CASS MESSAGE, WE ACCOMPLISHED THE ENGINE VIBRATION R QRH. REDUCED POWER ON AFFECTED SIDE 2 TIMES AND THE CASS MESSAG
- [SDR JGVR20201215001](https://openairdocs.org/sdr/JGVR20201215001.md): Spar · damaged · Dec 15, 2020 · N368QS · Cessna 680CE · Vertical Stabilizer, Spar/Rib
  > BLENDED CORRODED AREA ON THE VERTICAL STABILIZER AFT SPAR, LT SPAR STIFFENER. PERFORMED NDT AND REPORTED RESULTS FOR REPAIR DISPOSITION. REPLACED BLENDED STIFFER WITH NEW TEXTRON P/N 6931012-36.
- [SDR JGVR2020124001](https://openairdocs.org/sdr/JGVR2020124001.md): Spar · corroded · Dec 14, 2020 · N368QS · Cessna 680CE · Wing Spar
  > REMOVED EXISTING HI-LOC FASTENERS AND BLENDED CORRODED AREA OF THE LT AFT WING SPAR LOWER CLIP LOCATED IN THE LT MAIN LANDING GEAR WHEEL WELL. PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, PRIMED REPAIR AREA, INSTALLED EXISTING FASTENE
- [SDR JGVR20191220001](https://openairdocs.org/sdr/JGVR20191220001.md): Skin · corroded · Dec 20, 2019 · N368QS · Cessna 680CE · Fuselage Main, Plate/Skin
  > MECHANICALLY BLENDED THREE CORRODED AREAS OF THE EXTERIOR FUSELAGE SKIN, JUST BELOW THE EMERGENCY EXIT OPENING, PERFORMED ULTRASONIC AND EDDY CURRENT INSPECTIONS AND REPORTED RESULTS TO TEXTRON FOR REPAIR DISPOSITION. TREATED, PRIMED AND TOP COATED REPAIR AREA
- [SDR JGVR20191219001](https://openairdocs.org/sdr/JGVR20191219001.md): Door Frame · corroded · Dec 19, 2019 · N368QS · Cessna 680CE · Fuselage Main, Structure
  > FOUND CORROSION OUT OF LIMITS ON THE EMERGENCY EXIT DOOR LOCATED UNDERNEATH THE CONTOUR RINGS, REPLACED THE EMERGENCY EXIT DOOR WITH NEW TEXTRON PART.
- [SDR DXTA2019FA0000015](https://openairdocs.org/sdr/DXTA2019FA0000015.md): Skin · gouged · Jan 20, 2019 · N368QS · Cessna 680CE · Fuselage Main, Plate/Skin
  > LT NOSE SKIN DAMAGE (GOUGES), REF ENGINEERING LETTER DQ17110M1, DATED JAN 17, 2019
- [SDR DXTA2018010100518](https://openairdocs.org/sdr/DXTA2018010100518.md): Switch · faulty · Jan 31, 2018 · N368QS · Cessna 680CE · Door Warning System
  > CLIMBING THROUGH 12,000 FEET, NOSE DOOR OPEN L CAS MESSAGE ILLUMINATED. AFTER COMPLETING CHECKLIST AND RETURNING TO LAND, BOTH CREW MEMBERS VERIFIED NOSE DOOR LATCHES WERE SECURE. SUPPLEMENTAL INFORMATION: REPLACED AND RIGGED LEFT NOSE DOOR LATCH SWITCHES SN0
- [SDR JGVR20170630002](https://openairdocs.org/sdr/JGVR20170630002.md): Skin · corroded · Jun 30, 2017 · N368QS · Cessna 680SOV · Rudder, Plate/Skin
  > THE RUDDER HAS 3 AREAS OF SURFACE CORROSION LOCATED ON THE LT SIDE BOTTOM EDGE OF SKIN, AFT CORNER. REMOVED THE CORROSION IAW MM 51-10-01. PERFORMED AN EDDY CURRENT CHECK OF THE BLENDED AREAS ON RUDDER OUTER SKIN. NO CRACK OR CORROSION INDICATIONS FOUND. REPA
- [SDR JGVR20170630001](https://openairdocs.org/sdr/JGVR20170630001.md): Skin · corroded · Jun 30, 2017 · N368QS · Cessna 680SOV · Passenger/Crew Doors
  > MAIN ENTRANCE DOOR OUTER SKIN HAS AN AREA OF CORROSION ON THE LOWER AFT CORNER INSIDE SURFACE. REMOVED CORROSION IAW MM 51-10-01. PERFORMED AN EDDY CURRENT CHECK OF BLENDED AREA, NO CRACK OR CORROSION INDICATIONS FOUND. REPAIRED CORROSION BLEND IAW DQ8619.
- [SDR DXTA2015081106055](https://openairdocs.org/sdr/DXTA2015081106055.md): Brake · chattering · Aug 10, 2015 · N368QS · Cessna 680CE · Brake
  > BRAKES CHATTERED EXCESSIVELY & WHOLE PLANE SHOOK VERY BAD DURING LANDING ROLL OUT. PLANE DID NOT STOP AS IT SHOULD & BRAKES FELT SPONGY. R & R NR 1 & 2 BRAKE ASSEMBLIES, WORK DONE IAW MM 32-42-10.
- [SDR DXTA2014092605896](https://openairdocs.org/sdr/DXTA2014092605896.md): Oil System · overserviced · Sep 25, 2014 · N368QS · Cessna 680CE · APU Oil System
  > STARTED APU IMMEDIATELY HAD SMOKE COMING OUT OF THE WEMACS. FOUND APU OIL OVER SERVICED. REMOVED EXCESS OIL & BORESCOPED INLET OF APU WITH NO EVIDENCE OF OIL. RAN APU WITHOUT ANY SMOKE OR ODOR DETECTED AT THIS TIME. CHECKED OIL LEVEL AFTER SHUTDOWN IAW MM
- [SDR DXTA2014090505873](https://openairdocs.org/sdr/DXTA2014090505873.md): Brake Sys · contaminated · Sep 4, 2014 · N368QS · Cessna 680CE · Landing Gear Brake System
  > ON LANDING APPLIED MAX BRAKING, DECELERATION WAS EQUIVALENT TO MIN BRAKING WITH NO ANTI-SKID CYCLING. BLED ALL 4 BRAKES, INSPECTED BRAKES IAW MM 12-12-02. SERVICED HYD, TAXI CHECKED GOOD.
- [SDR DXTA2013101405543](https://openairdocs.org/sdr/DXTA2013101405543.md): Line · cracked · Oct 20, 2013 · N368QS · Cessna 680CE · Landing Gear Retraction/Extension System
  > AFTER ROTATION, HYD LOW PRESSURE CASS MESSAGE ILLUMINATED. LOWERED LANDING GEAR AND RECEIVED A HYD LEVEL LOW LIGHT. NOSE COMPARTMENT WAS COVERED IN HYD FLUID. FOUND NOSE WHEEL CENTERING HYDRAULIC LINE CRACKED AND LEAKING. REPLACED HYD LINES ON THE NOSE
- [SDR DXTA2013072305454](https://openairdocs.org/sdr/DXTA2013072305454.md): Strut · low pressure · Jul 22, 2013 · N368QS · Cessna 680CE · Landing Gear Retraction/Extension System
  > LANDING GEAR WILL NOT RETRACT AFTER TAKEOFF. GEAR HANDLE WOULD NOT MOVE. RECEIVED A WOW MISCOMPARE. RAN APPROPRIATE CHECKLIST. FOUND NOSE STRUT NOT FULLY EXTENDING. ACCOMPLISHED NOSE STRUT SERVICING IAW MM 12-14-00. OPS & LEAK CHECKED GOOD.
- [SDR DXTA2013062105421](https://openairdocs.org/sdr/DXTA2013062105421.md): Anti-Skid Sys · failed · Jun 20, 2013 · N368QS · Cessna 680CE · Landing Gear System Wiring
  > ON LANDING ROLLOUT, SLOWING TO 65 KTS, AMBER ANTI-SKID FAIL CAS ILLUMINATED FOR 5-10 SECONDS & WENT OUT. DURING TAXI, ANTI-SKID FAIL CAS MESSAGE CYCLED ON/OFF FOUR TIMES. POWERED ACFT DOWN & CAS MESSAGE DID NOT COME ON. AFTER TAKEOFF, AT GEAR RETRACTION, A
- [SDR DXTA2013041105353](https://openairdocs.org/sdr/DXTA2013041105353.md): Oil System · leaking · Apr 10, 2013 · N368QS · Cessna 680CE · APU Oil System
  > AFTER 2ND POST FLIGHT OF THE DAY DISCOVERED OIL LEAKING FROM APU EXHAUST FWD ALONG BOTTOM OF FUSELAGE. APU WAS STARTED ON GROUND AND COCKPIT FILLED WITH SMOKE FROM WEMACS. CABIN ALSO FILLED WITH SMOKE, DID NOT NOTICE FROM WHERE. APU WAS SHUTDOWN. ENGINES WER
- [SDR DXTA2012090605117](https://openairdocs.org/sdr/DXTA2012090605117.md): Door Frame · corroded · Sep 4, 2012 · N368QS · Cessna 680CE · Fuselage Main, Structure
  > CABIN DOOR FORWARD FRAME CORRODED AT SHEAR TIE FITTING. REMOVED SURFACE CORROSION IAW SRM 51-20-01. INSTALLED DOOR FRAME IAW SRM 51-40-03.
- [SDR DXTA2012082905108](https://openairdocs.org/sdr/DXTA2012082905108.md): Door Frame · corroded · Aug 23, 2012 · N368QS · Cessna 680CE · Fuselage Main, Structure
  > MAIN ENTRY DOOR FRAME CORRODED. FOUND DURING INSPECTION.
- [SDR DXTA2011071204657](https://openairdocs.org/sdr/DXTA2011071204657.md): Starter Gen · failed · Jul 12, 2011 · N368QS · Cessna 680CE · Starter-Generator
  > DURING CRUISE AT FL400, A VIBRATION & AUDIBLE NOISE NOTED APPROX 2 HRS INTO FLT. AN ENGINE CONTROL FAULT MESSAGE DISPLAYED ON CAS. CHECKLIST FOLLOWED AND CAS MESSAGE EXTINGUISHED. SEVERAL MINUTES LATER, A DC GEN CAS MESSAGE DISPLAYED & CHECKLIST COMPLETED. UN
- [SDR DXTA2011042504558](https://openairdocs.org/sdr/DXTA2011042504558.md): Circuit Board · inoperative · Apr 24, 2011 · N368QS · Cessna 680CE · Stabilizer Control System
  > PRIMARY STAB TRIM FAIL AND/OR RUN-AWAY ON TAKEOFF. AIRPLANE WOULD NOT MAINTAIN AIRSPEED WITH YOKE TO THE FULL FWD STOP. SECONDARY TRIM WAS OPERATIONAL. UNABLE TO DUPLICATE. TALKED TO TEAM SOVEREIGN ABOUT THE PROBLEM. THEY RECOMMENDED REPLACING THE TRIM CONT
- [SDR DXTA2010102904283](https://openairdocs.org/sdr/DXTA2010102904283.md): Engine · malfunctioned · Oct 23, 2010 · N368QS · Cessna 680CE · Engine (Turbine/Turboprop)
  > DECENDING THROUGH FL 320, FELT A SHUTTER ICAS HAD A CYAN ENG SHUTDOWN LT DISPLAYED FOR A FEW SECONDS ACOMPANIED BY A DECREASING LT ITT. LT ENG THEN RETURNED ITSELF TO NORMAL OPS. PRESSED EVENT MARKER AT TIME OF INCIDENT. IT APPEARS THAT 60 TO 80 PERCENT OF TH
- [SDR DXTA200702428](https://openairdocs.org/sdr/DXTA200702428.md): Engine · power loss · Aug 24, 2007 · N368QS · Cessna 680CE · Engine (Turbine/Turboprop)
  > AFTER TAKEOFF, LEVELED OFF AT 2000 FT WHEN REDUCING POWER ON BOTH ENGINES TO 70 PERCENT N1 BOTH ENGINES SURGED +/- 5 TO 10 PERCENT. BOTH ENGINES STABILIZED AFTER APPROXIMATELY 60 TO 90 SECONDS. DOWNLOADED EDU'S IAW MM CH 77-40-01. RAN ENGINES REPRODUCED SQU
- [SDR DXTA200702165](https://openairdocs.org/sdr/DXTA200702165.md): Switch · out of adjust · May 1, 2007 · N368QS · Cessna 680CE · Landing Gear Position and Warning
  > FRONT NOSE DOOR L AMBER CAUTION MESSAGE ILLUMINATED AFTER TAKE OFF AND ACCELERATING MESSAGE ILLUMINATED. LIGHT EXTINGUISHED WHEN LANDING GEAR EXTENDED. ADJUSTED LEFT NOSE ACCESS DOOR SWITCH PER CE 680 M/M 52-70-00. OPS CKS GOOD.
- [SDR DXTA200601763](https://openairdocs.org/sdr/DXTA200601763.md): Actuator · inoperative · Nov 29, 2006 · N368QS · Cessna 680CE · Autopilot System
  > AUTOPILOT FAIL - B CYAN CAS MESSAGE ILLUMINATES AFTER AVIONICS POWER UP. REMOVED AND INSTALLED NEW ACTUATOR I/O MODULE ASSEMBLY CARD. PERFORMED YAW DAMPNER SYSTEM TEST GOOD IAW MM. 34-23-10.
- [SDR DXTA200601693](https://openairdocs.org/sdr/DXTA200601693.md): Electrical Box · shorted · Oct 27, 2006 · N368QS · Cessna 680CE · Flight Control System Wiring
  > (FLAPS FAIL) AMBER CAS MESSAGE POSTED ATTEMPTING FLAPS 7: FLAPS WERE RESET AND FAILED AGAIN AT FLAPS 7. FLAPS WERE RESET AND FAILED AT FLAPS 15: FLAPS WERE RESET AND DID NOT FAIL AFTER FLAPS 35 WERE INDICATED. CHECKED BITE ON FLAP CONTROLLER, BITE 5 TRIPPED
- [SDR DXTA20061691](https://openairdocs.org/sdr/DXTA20061691.md): Electrical Box · inoperative · Oct 27, 2006 · N368QS · Cessna 680CE · Leading Edge Slat Control System
  > "FLAPS FAIL" AMBER CAS MESSAGE POSTED ATTEMPTING FLAPS 7: FLAPS WERE RESET AND FAILED AGAIN AT FLAPS 7. FLAPS WERE RESET AND FAILED AT FLAPS 15: FLAPS WERE RESET AND DID NOT FAIL AFTER FLAPS 35 WERE INDICATED. CHECKED BITE ON FLAP CONTROLLER, BITE 5 TRIPPE

## 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 = 'N368QS' AND deregistration_id = 'N368QS-2025-07-26'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N368QS-2025-07-26/reports

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