# Service difficulty reports: N385QS, cancelled Jun 1, 2026

A list on [N385QS, cancelled Jun 1, 2026](https://openairdocs.org/deregistered/N385QS-2026-06-01.md).

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

- [SDR DXTA2026010906472](https://openairdocs.org/sdr/DXTA2026010906472.md): Pressure Valve · faulted · Jan 7, 2026 · N385QS · Cessna 680SOV · Pneumatic Indicating System
  > SHORTLY AFTER TAKEOFF POWER APPLIED, HP VALVE FAIL LT AMBER CAS LIGHT ILLUMINATED. COMPLETED APPROPRIATE QRH. INSPECTED GD001 GROUND. NO DISCREPANCIES. RANG WIRING FROM VALVE TO PYLON,. NO DISCREPANCIES. R & R HP VALVE. OPS CHKD GOOD, BUT LEAK CHECKS NOT
- [SDR JGVR20251119002](https://openairdocs.org/sdr/JGVR20251119002.md): Skin · corroded · Nov 19, 2025 · N385QS · Cessna 680CE · Fuselage Main, Plate/Skin
  > REPAIRED THE CORRODED AREA ON THE RT SKIN/PANEL OF THE NOSE LANDING GEAR TUNNEL BY BLENDING CORRODED AREA, PERFORMING NDT, REPORTING FOR REPAIR DISPOSITION, FABRICATING AND INSTALLING REPAIR DOUBLER IN ACCORDANCE WITH ENGINEERING REPAIR ORDER.
- [SDR JGVR20251119001](https://openairdocs.org/sdr/JGVR20251119001.md): Skin · corroded · Nov 19, 2025 · N385QS · Cessna 680CE · Fuselage Main, Plate/Skin
  > REPAIRED CORRODED AREAS OF THE LOWER AFT TAILCONE SKINS, LOCATED UNDER AND ADJACENT TO THE AFT CHIN FAIRING JOINT, BY BLENDING AREAS, PERFORMING NDT, REPORTING FOR REPAIR DISPOSITION, FABRICATING AND INSTALLING REPAIR DOUBLERS PER ENGINEERING REPAIR ORDER.
- [SDR JGVR20251118001](https://openairdocs.org/sdr/JGVR20251118001.md): Skin · corroded · Nov 18, 2025 · N385QS · Cessna 680CE · Emergency Exits
  > BLENDED CORRODED AREA ON THE OUTER SKIN OF THE EMERGENCY EXIT DOOR IN THE LOWER AFT CORNER, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED AREA PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.
- [SDR JGVR20251017003](https://openairdocs.org/sdr/JGVR20251017003.md): Spar · corroded · Oct 17, 2025 · N385QS · Cessna 680CE · Wing Spar
  > BLENDED AREA OF CORROSION LOCATED ON THE LT AFT WING SPAR LOWER WEB AT THE EMERGENCY BRAKE CARRY THROUGH FITTING HOLES, LOCATED IN THE LT MAIN LANDING GEAR WHEEL WELL, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED BLENDED ARE
- [SDR JGVR20251017002](https://openairdocs.org/sdr/JGVR20251017002.md): Spar Cap · corroded · Oct 17, 2025 · N385QS · Cessna 680CE · Wing Spar
  > BLENDED AREA OF CORROSION LOCATED INSIDE LH MAIN GEAR WELL BAY ON THE AFT LOWER SPAR CAP, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED BLENDED AREA PER NETJETS REQUEST FOR TECHNICAL DISPOSITION REPORT.
- [SDR JGVR20251017001](https://openairdocs.org/sdr/JGVR20251017001.md): Spar · corroded · Oct 17, 2025 · N385QS · Cessna 680CE · Wing Spar
  > BLENDED AREA OF CORROSION LOCATED INSIDE RIGHT MAIN GEAR WELL BAY 720DR ON THE LOWER AFT SPAR CAP, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED BLENDED AREA PER TECHNICAL DISPOSITION REPORT.
- [SDR DXTA2025031002606](https://openairdocs.org/sdr/DXTA2025031002606.md): Acm · malfunctioned · Mar 6, 2025 · N385QS · Cessna 680SOV · Cabin Cooling System
  > TEMPERATURE CONTROL: DIVERTED DUE TO AMBER EMERGENCY PRESSURIZATION AND ACM O'TEMP CLIMBING THROUGH APROX 37,000 FT THE RIGHT ENGINE ITT BEGAN TO CLIMB RAPIDLY. PULLED BACK RIGHT THROTTLE APROX 2 FULL KNOB WIDTHS TO AVOID OVERTEMP. EVENT BUTTON WAS PUSHED.
- [SDR 2023F00224](https://openairdocs.org/sdr/2023F00224.md): Angle · corroded · Jul 13, 2023 · N385QS · Cessna 680CE · Wing Structure
  > CORROSION, LH WING, AFT SPAR, WS 28. ACCOMPLISHED TEXTRON AVIATION FIELD REPAIR FR-680-0115-12138 REV-, DATED JULY 11, 2023 AND FAA FORM 8100-9 DATED 7/11/2023; FIELD REPAIR - CORROSION, LH WING, AFT SPAR, WS 28.
- [SDR 2021FA0000252](https://openairdocs.org/sdr/2021FA0000252.md): Panel · damaged · Sep 2, 2021 · N385QS · Cessna 680A · Horizontal Stabilizer Miscellaneous Structure
  > LH HORIZONTAL WIPER PANEL LOWER AFT SECTION MOUNTING HOLES ARE OVERSIZED AND ELONGATED. REFERENCE TEXTRON AVIATION ENGINEERING MEMO DQ31281M1 REV A DATED 31/AUG/2021.
- [SDR DXTA2021080246190](https://openairdocs.org/sdr/DXTA2021080246190.md): Line · failed · Aug 1, 2021 · N385QS · Cessna 680CE · Hydraulic System, Main
  > HYDRAULIC LINE: HYDRAULIC PRESSURE LOW L-R AMBER CAS BOTH EMERGENCY GEAR BLOWDOWN AND EMERGENCY BRAKING APPLIED. PERFORMED MULTIPLE GEAR SWINGS WITH THE HYDRAULIC MULE. DURING INITIAL SWINGS FOUND THE CYCLE TO TAKE MORE THAN 125 WITH 3100 PSI IN THE SYSTEM.
- [SDR DXTA2021061643770](https://openairdocs.org/sdr/DXTA2021061643770.md): Door · binding · Jun 15, 2021 · N385QS · Cessna 680CE · Passenger/Crew Doors
  > MAIN DOOR: COULD NOT OPEN MAIN CABIN DOOR USING RED RELEASE BUTTON OR SECONDARY RELEASE. WITH ASSISTANCE OF GROUND PERSONNEL WE WERE OPEN DOOR. "CORRECTIVE ACTION" PERFORMED CABIN DOOR INSPECTION/CHECK PER CE-680MM 52-10-00. AS FOLLOWS. REMOVED CENTER ACCESS P
- [SDR 2021F00023](https://openairdocs.org/sdr/2021F00023.md): Skin · damaged · Feb 9, 2021 · N385QS · Cessna 680CE · Wing, Plate/Skin
  > OVERSIZED HOLE CENTER WING UPPER SKIN WS 36.5 AT THE REAR SPAR. ACCOMPLISHED A FIELD REPAIR FR680-0115-8859 REV - DATED 0/4/2021; FIELD REPAIR - HOLE OVERSIZE, CENTER WING, UPPER SKIN, WS 36.5 AT THE REAR SPAR.
- [SDR 2021F00022](https://openairdocs.org/sdr/2021F00022.md): Skin · corroded · Feb 9, 2021 · N385QS · Cessna 680CE · Wing, Plate/Skin
  > CORROSION, WING UPPER SKINS, WS37. ACCOMPLISHED TEXTRON AVIATION STANDARD REPAIR SR-680-ATA57-27245 REV - DATED 10/08/2020; STANDARD REPAIR - CORROSION, WING, UPPER SKINS, WS 37.AFFECTED PART (S); SKIN P/NS 6921370-1, 6921372-9, 6922377-39, 6922680-23, 6922680
- [SDR 2021F00021](https://openairdocs.org/sdr/2021F00021.md): Skin · damaged · Feb 9, 2021 · N385QS · Cessna 680CE · Wing, Plate/Skin
  > OVER SIZED HOLE, UPPER CENTER WING SKIN WS 36.5 AT THE MAIN SPAR. ACCOMPLISHED TEXTRON AVIATION FIELD REPAIR FR-680-0115-8872 REV - DATED 02/08/2021; FIELD REPAIR - HOLE OVERSIZE, CENTER WING, UPPER SKIN, WS 36.5 AT THE MAIN SPAR.
- [SDR 2021F00019](https://openairdocs.org/sdr/2021F00019.md): Panel · corroded · Feb 8, 2021 · N385QS · Cessna 680SOV · Horizontal Stabilizer, Plate/Skin
  > REPAIR TO HORIZONTAL TRAILING EDGE PANELS. TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ28656M2 DATED FEB. 7, 2021.
- [SDR 2021F00018](https://openairdocs.org/sdr/2021F00018.md): Piccolo Tube · damaged · Feb 8, 2021 · N385QS · Cessna 680SOV · Airfoil Anti/De-ice System
  > REPAIR TO ANTI-ICE PICCOLO TUBE FLANGE. TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ28735 DATED JANUARY 30, 2021.
- [SDR 2021FA0000035](https://openairdocs.org/sdr/2021FA0000035.md): Fairing · delaminated · Feb 6, 2021 · N385QS · Cessna 680CE · Aerodynamic Fairings
  > LEFT HAND WING TO FUSELAGE MID FAIRING DAMAGED. REPAIRED L/H WING TO FUSELAGE MID FAIRING P/N 6922706-17 I.A.W TEXTRON AVIATION ENGINEERING DQ28747, REF. S-750-ATA51-01RD REV A.
- [SDR 2021FA0000034](https://openairdocs.org/sdr/2021FA0000034.md): Frame · cracked · Feb 5, 2021 · N385QS · Cessna 680CE · Fuselage Main, Frame
  > NLG WHEEL WELL OVERHEAD STRUCTURE FRAME IS CRACKED-UPPER MID UPPER. REFERENCE AQRD ENGINEERING REPAIR ORDER NO. ERO-104483 REV IR DATED JAN 25 2021
- [SDR DXTA202004213648](https://openairdocs.org/sdr/DXTA202004213648.md): Line · disconnected · Apr 20, 2020 · N385QS · Cessna 680CE · Cabin Cooling System
  > CABIN ALTITUDE AMBER CAS ILLUMINATED - ON CLIMB OUT AT 20000 FEET WE OBSERVED CABIN CLIMBING HIGHER THAN NORMAL AND AT 34000 FEET THE AMBER CAS (8500) LIGHT ILLUMINATED. EMERG CHECKLIST WAS ACCOMPLISHED WTIH NO CHANGE AND AN EMERGENCY WAS DECLARED AND CABIN RE
- [SDR JGVR20190219002](https://openairdocs.org/sdr/JGVR20190219002.md): Access Panel · corroded · Feb 19, 2019 · N385QS · Cessna 680CE · Passenger/Crew Doors
  > BLENDED AND TREATED 28 AREAS OF CORROSION ON THE CABIN ENTRY DOOR INNER DOOR SKIN ACCESS PANELS PER REPAIR MEMO.
- [SDR JGVR20190219001](https://openairdocs.org/sdr/JGVR20190219001.md): Skin · corroded · Feb 19, 2019 · N385QS · Cessna 680CE · Fuselage Main, Plate/Skin
  > REPAIRED 22 CORRODED AREAS OF THE DROPPED AISLE FLOOR (INTERIOR FUSELAGE SKIN) BY BLENDING AREAS, PERFORMING ULTRASONIC AND EDDY CURRENT INSPECTIONS, TREATING, PRIMING, AND INSTALLING REPAIR DOUBLERS AS REQUIRED IAW ENGINEERING REPAIR ORDER ERO-936469 REV IR,
- [SDR 2017F00063](https://openairdocs.org/sdr/2017F00063.md): Frame · damaged · Mar 1, 2017 · N385QS · Cessna 680CE · Fuselage Main, Frame
  > ELONGATED & OVERSIZED HOLES AT BS 624 FRAME IN TAILCONE FOR RUDDER BIAS ATTACHMENT.
- [SDR 2017F00062](https://openairdocs.org/sdr/2017F00062.md): Fitting · corroded · Mar 1, 2017 · N385QS · Cessna 680CE · Wing, Attach Fittings
  > AFT LEFT AND RIGHT SIDE SPAR WEB BULKHEAD FITTING CORRODED.
- [SDR 2017F00061](https://openairdocs.org/sdr/2017F00061.md): Spar · corroded · Mar 1, 2017 · N385QS · Cessna 680CE · Wing Spar
  > CENTER SPAR BULKHEAD AND LEFT AND RIGHT WING STATION 37.0 RIB FITTING CORRODED.
- [SDR 2017F00060](https://openairdocs.org/sdr/2017F00060.md): Fitting · corroded · Mar 1, 2017 · N385QS · Cessna 680CE · Wing, Attach Fittings
  > AFT LEFT AND RIGHT SIDE SPAR WEB BULKHEAD FITTING CORRODED.
- [SDR DXTA2015071706044](https://openairdocs.org/sdr/DXTA2015071706044.md): Fan · failed · Jul 16, 2015 · N385QS · Cessna 680CE · Air Distribution Fan
  > SMOKE IN THE CABIN ON THE GROUND WITH THE APU RUNNING & BLEED AIR ON. DISCONNECTED BLEED AIR DUCT COUPLING & BORESCOPED APU INLET COMPRESSOR AREA & BLEED AIR PORT FOR OIL LEAK. NO OIL LEAKAGE NOTED AT THIS TIME. CONNECTED BLEED AIR COUPLING, LEAK CHECK NO
- [SDR DXTA2015052206021](https://openairdocs.org/sdr/DXTA2015052206021.md): Actuator · failed · May 18, 2015 · N385QS · Cessna 680CE · Rudder Actuator
  > NO TAKEOFF MSG, DUE TO ROLL SYS. UPON INITIAL OPS CHECKS NOTED NO CAS MSGS. REMOVED THE ACCESS PANEL & INSPECTED THE PROXIMITY SWITCH & TARGET. NOTED THE TARGET IS NOT FULLY CENTERED ON THE PROXIMITY SWITCH. REMOVED THE BELLY PANEL & FURTHER INSPECTED. CO
- [SDR DXTA2014121505946](https://openairdocs.org/sdr/DXTA2014121505946.md): Wire · chafed · Dec 13, 2014 · N385QS · Cessna 680CE · Landing Gear System Wiring
  > DURING GEAR RETRACTION, ALL FOUR GEAR LIGHTS EXTINGUISHED NORMALLY, BUT WITHIN 1-2 SECONDS, RED UPLOCK LIGHT FLICKERED & THEN STAYED ON. GEAR EXTENDED NORMALLY. JACKED AIRCRAFT, CONNECTED HYD AND CYCLED GEAR. UNLOCK WOULD REMAIN ON, ON THE FIRST TIME THE GE
- [SDR DXTA2013043005366](https://openairdocs.org/sdr/DXTA2013043005366.md): Display · inoperative · Apr 30, 2013 · N385QS · Cessna 680CE · Independent Instruments
  > AS THE FLYING PILOT, SMELLED SMOKE AND SAW FLAGS ON THE STNDBY ATTITUDE INDICATOR. MY PARTNER SAW IT AT THE SAME TIME AND TURNED OFF THE STANDYBY INDICATOR. THAT REDUCED THE SMELL. DEPLOYED THE MASKS AND DIVERTED. VERIFIED ATTITUDE INDICATOR IS INOPERATIVE
- [SDR CWQR20130311018](https://openairdocs.org/sdr/CWQR20130311018.md): Heat Exchanger · cracked · Mar 11, 2013 · N385QS · Cessna 680CE · Pneumatic Distribution System
  > DURING A SCHEDULED INSPECTION WE WERE PREFORMING A PRODUCT IMPROVEMENT (REPLACEMENT OF DUCT ASSY 6914070-67) WE NOTICED THAT THE HEAT EXCHANGER SIDE PLATE HAD 1 CRACKS ABOUT.40" LONG. A NEW HEAT EXCHANGER WAS INSTALLED. WE PREFORMED A LEAK CHECK ON THE DEFE
- [SDR CWQR20130305015](https://openairdocs.org/sdr/CWQR20130305015.md): Heat Exchanger · cracked · Mar 5, 2013 · N385QS · Cessna 680CE · Pneumatic Distribution System
  > DURING A SCHEDULED INSPECTION, NOTICED THE HEAT EXCHANGER SIDE PLATE HAD THREE CRACKS ABOUT.30 INCH LONG. OPPOSITE SIDE OF THE HEAT EXCHANGER WAS CRACKED IN THREE OF THE FOUR CORNERS. A NEW HEAT EXCHANGER WAS INSTALLED. PREFORMED A LEAK CHECK ON THE DEFEC
- [SDR DXTA2012092105130](https://openairdocs.org/sdr/DXTA2012092105130.md): Apu · leaking · Sep 20, 2012 · N385QS · Cessna 680CE · APU Oil System
  > ON PREFLIGHT WITH APU RUNNING AND AC ON, SMELLED OILY ODOR AND SAW LIGHT SMOKE IN CABIN. WITH BLEED AIR OFF, SMOKE WENT AWAY WITH JUST A LITTLE OIL ODOR. REMOVED L/R APU PANELS, REMOVED INLET TEMP BULB, UNBOLTED INLET AND MOVED UPWARD TO ACCESS APU INLET.
- [SDR DXTA2012033004934](https://openairdocs.org/sdr/DXTA2012033004934.md): Warning Light · no indication · Mar 29, 2012 · N385QS · Cessna 680CE · Landing Gear Position and Warning
  > RIGHT MLG LIGHT WOULD NOT ILLUMINATE. FOLLOWED THE CHECKLIST PROCEDURE. RESET GEAR SYS IAW MM 32-00-00, BLED SYS. RESERVICED N2 BOTTLE AND SAFETIED. GEAR SWING CHECKED GOOD.
- [SDR DXTA2012031904923](https://openairdocs.org/sdr/DXTA2012031904923.md): Seal · leaking · Mar 16, 2012 · N385QS · Cessna 680CE · Nose/Tail Landing Gear Strut/Axle
  > AFTER TAKEOFF, GEAR WOULD NOT RETRACT. A SHORT TIME LATER WE GOT THE AMBER "WOW MISCOMPRE" CAS MESSAGE. ALL CBS ARE SET.
- [SDR DXTA200803254](https://openairdocs.org/sdr/DXTA200803254.md): Control Unit · faulty · Aug 29, 2008 · N385QS · Cessna 680CE · Landing Gear Selector
  > AFTER TAKEOFF, ATTEMPTED TO RAISE GEAR. HANDLE MOVED TO THE UP POSITION, BUT THE GEAR REMAINED EXTENDED. NO OTHER INDICATIONS PRESENT - NO CAS MESSAGE, NO RED LIGHT, THREE GREEN REMAINED ON, NO AUDIO WARNINGS. HANDLE PLACED TO DOWN POSITION FOR LANDING AND L
- [SDR DXTA200803176](https://openairdocs.org/sdr/DXTA200803176.md): Strut · out of adjust · Jul 14, 2008 · N385QS · Cessna 680CE · Nose/Tail Landing Gear Strut/Axle
  > LOUD NOISE FROM NOSE WAS HEARD DURING GEAR RETRACTION. NOISE (THUMP) WAS FOLLOWED WITH RED GEAR UNLOCK LIGHT REMAINING ILLUMINATED. GEAR EXTENDED WITH 3 GREEN AND UNLOCK LIGHT EXTINGUISHED. JACKED ACFT AND INSPECTED NLG AND NLG WHEELWELL DUE TO RECENT NLG SER
- [SDR DXTA200803164](https://openairdocs.org/sdr/DXTA200803164.md): Squat Switch · out of adjust · Jul 8, 2008 · N385QS · Cessna 680CE · Landing Gear Position and Warning
  > ON GEAR RETRACTION, NOSE GEAR MADE A NOTICEABLE CLUNK AND BANG AND THE RED GEAR UNLOCK LIGHT REMAINED ILLUMINATED. JACKED AIRCRAFT AND CHECKED FOR PLAY IN NLG AND FOUND NLG TO BE FREE OF EXCESSIVE PLAY. CHECKED UPPER AND LOWER BARREL PRESSURES AND FOUND LOWE
- [SDR DXTA20082904](https://openairdocs.org/sdr/DXTA20082904.md): Strut · unknown · Feb 28, 2008 · N385QS · Cessna 680CE · Nose/Tail Landing Gear Strut/Axle
  > UPON GEAR RETRACTION, A THUMPING NOISE WAS COMING FROM THE NOSEWHEEL COMPARTMENT ALONG WITH A FLASHING RED UNLOCK LIGHT. PERFORMED SEVERAL GEAR RETRACTIONS AND EXTENSIONS. SERVICED UPPER AND LOWER BARREL (STRUT) PRESSURES. ALL SYSTEMS OPS CHECK GOOD. IAW M

## 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 = 'N385QS' AND deregistration_id = 'N385QS-2026-06-01'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N385QS-2026-06-01/reports

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