# Service difficulty reports: N320QS

A list on [N320QS](https://openairdocs.org/aircraft/N320QS.md).

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

- [SDR DXTA2026061808462](https://openairdocs.org/sdr/DXTA2026061808462.md): Battery · faulty · Jun 15, 2026 · N320QS · Cessna 680SOV · Emergency Lighting
  > SEVERAL OVERHEAD INTERIOR EMERGENCY LIGHTS AND HALF OF THE EXTERIOR EMERGENCY LIGHTS FAILED TO ILLUMINATE DURING PREFLIGHT CHECKS. REPEAT WRITE-UP. REMOVED FAILED 1 THRU 4 EMERGENCY LIGHT BATTERIES AND INSTALLED CUSTOMER SUPPLIED EMERGENCY LIGHT BATTERIES IN
- [SDR JGVR20251117002](https://openairdocs.org/sdr/JGVR20251117002.md): Skin · corroded · Nov 17, 2025 · N320QS · Cessna 680CE · Fuselage Main, Plate/Skin
  > REPAIRED CORRODED AREAS OF THE INNER SURFACES OF THE BAGGAGE COMPARTMENT SKINS, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. FABRICATED AND INSTALLED REPAIR DOUBLERS PER REQUEST FOR TECHNICAL SERVICES REPORT.
- [SDR JGVR20251117001](https://openairdocs.org/sdr/JGVR20251117001.md): Skin · corroded · Nov 17, 2025 · N320QS · Cessna 680CE · Wing, Plate/Skin
  > MECHANICALLY REMOVED CORROSION LOCATED ON THE LT LOWER WING SKIN AT WS.294 PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED TREATED AND PRIMED REPAIR AREAS PER REQUEST FOR TECHNICAL SERVICES REPORT.
- [SDR JGVR20251113002](https://openairdocs.org/sdr/JGVR20251113002.md): Skin · corroded · Nov 13, 2025 · N320QS · Cessna 680CE · Wing, Plate/Skin
  > FOUND CORROSION ON THE UPPER INBOARD WING SKINS LOCATED ALONG AND UNDER THE DRAG ANGLES (FUSELAGE TO WING FARING ATTACH STRUCTURE), REMOVED THE DRAG ANGLES, BLENDED CORROSION, REPORTED FOR REPAIR DISPOSITION. REPLACED BLENDED FASTENERS AS REQUIRED, CLEANED TRE
- [SDR JGVR20251112002](https://openairdocs.org/sdr/JGVR20251112002.md): Skin · corroded · Nov 12, 2025 · N320QS · Cessna 680CE · Fuselage Main, Plate/Skin
  > BLENDED CORRODED AREAS LOCATED ON THE NUTPLATE-SIDE OF THE FUSELAGE STRUCTURE WHERE THE SPADE DOOR (MAIN ENTRY DOOR LOWER FAIRING DOOR) ATTACHES TO THE AIRCRAFT, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. FABRICATED AND INSTALLED REPAIR DOUBLERS AS REQ
- [SDR JGVR20251112001](https://openairdocs.org/sdr/JGVR20251112001.md): Skin · corroded · Nov 12, 2025 · N320QS · Cessna 680CE · Wing, Plate/Skin
  > FOUND 5 AREAS OF CORROSION ON THE UPPER SURFACE OF THE LH UPPER WING SKIN AND 2 AREAS ON THE UPPER SURFACE OF THE RH UPPER WING SKIN, MECHANICALLY BLENDED CORRODED AREAS, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. FABRICATED AND INSTALLED REPAIR DOUBL
- [SDR JGVR20251111002](https://openairdocs.org/sdr/JGVR20251111002.md): Tail Cone · corroded · Nov 11, 2025 · N320QS · Cessna 680CE · Aerodynamic Fairings
  > REPAIRED CORRODED AREA LOWER TAILCONE SKINS AT THE AIRCRAFT DATA PLATE BY BLENDING, PERFORMING NDT, REPORTING FOR REPAIR DISPOSITION, FABRICATING AND INSTALLING REPAIR DOUBLERS PER ENGINEERING REPAIR ORDER.
- [SDR JGVR20251111001](https://openairdocs.org/sdr/JGVR20251111001.md): Skin · corroded · Nov 11, 2025 · N320QS · Cessna 680CE · Wing, Plate/Skin
  > REPAIRED CORRODED AREA ON THE LOWER WING SKIN IN THE RH LANDING GEAR WELL, BY BLENDING, PERFORMING NDT, REPORTING FOR REPAIR DISPOSITION, FABRICATING AND INSTALLING REPAIR DOUBLER PER ENGINEERING ORDER.
- [SDR JGVR20251110003](https://openairdocs.org/sdr/JGVR20251110003.md): Skin · corroded · Nov 10, 2025 · N320QS · Cessna 680CE · Vertical Stabilizer, Plate/Skin
  > MECHANICALLY REMOVED CORROSION LOCATED ON RH VERTICAL STABILIZER SKIN, JUST FORWARD OF ACCESS PANEL 341BR PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION, CLEANED, TREATED AND PRIMED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.
- [SDR JGVR20251110002](https://openairdocs.org/sdr/JGVR20251110002.md): Skin · corroded · Nov 10, 2025 · N320QS · Cessna 680CE · Wing, Plate/Skin
  > BLENDED 7 AREAS OF CORROSION PLUS 1 ADDITIONAL AREA LOCATED ON RH UPPER WING SKIN AT WS 294 TO THE WING TIP, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED AND PRIMED AREAS NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.
- [SDR JGVR20251110001](https://openairdocs.org/sdr/JGVR20251110001.md): Skin · corroded · Nov 10, 2025 · N320QS · Cessna 680CE · Emergency Exits
  > MECHANICALLY BLENDED 1 AREA OF CORROSION LOCATED ON E-EXIT EXTERIOR SKIN LOCATED ON INNER EDGE PERIMETER OF CONTOUR RINGS, LOWER AREA OF E-EXIT PERFORMED NDT AND FOUND BLEND TO BE WITHIN LIMITS, CLEANED, TREATED AND PRIMED BLENDED AREA IAW TEXTRON ENGINEERING
- [SDR JGVR20250910002](https://openairdocs.org/sdr/JGVR20250910002.md): Skin · corroded · Sep 10, 2025 · N320QS · Cessna 680CE · Fuselage Main, Plate/Skin
  > MECHANICALLY REMOVED 1 AREA OF CORROSION LOCATED ON FUSELAGE SKIN AT THE RH NOSE DOOR AFT LATCH AREA, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPAIRED CORROSION BLENDS IAW NETJETS REQUEST FOR TECHNICAL SERVICES BY CLEANING, TREATING, PRIMING, AND T
- [SDR JGVR20250910001](https://openairdocs.org/sdr/JGVR20250910001.md): Angle · corroded · Sep 10, 2025 · N320QS · Cessna 680CE · Fuselage Miscellaneous Structure
  > MECHANICALLY REMOVED 1 AREA OF CORROSION LOCATED IN LH MLG WHEEL WELL AFT SPAR LOWER CLIP, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPAIRED CORROSION BLENDS IAW NETJETS REQUEST FOR TECHNICAL SERVICES BY CLEANING, TREATING, AND PRIMING BLENDED AREA.
- [SDR 2024F00254](https://openairdocs.org/sdr/2024F00254.md): Fairing · damaged · Oct 17, 2024 · N320QS · Cessna 680CE · Aerodynamic Fairings
  > DURING INSPECTION 80 HOLES WERE OVERSIZED DURING HI-LOCK REMOVAL ON THE BELLY FAIRING. 40 OVERSIZED HOLES AT LWS 37 AND 40 OVERSIZED HOLES AT RWS 37. REPAIR WAS ACCOMPLISHED IAW AQRD ENGINEERING REPAIR ORDER ERO-981793 AND CESSNA 680 SRM 51-40-03.
- [SDR 2024FA0000761](https://openairdocs.org/sdr/2024FA0000761.md): Case · gouged · Oct 9, 2024 · N320QS · Cessna 680CE · Nacelle/Pylon, Main Frame
  > N320QS (680-0169) RH ENGINE CASE GOUGE.
- [SDR 2024F00248](https://openairdocs.org/sdr/2024F00248.md): Doubler · corroded · Oct 9, 2024 · N320QS · Cessna 680CE · Wing, Plate/Skin
  > THE LH AND RH WING FUEL PANELS HAVE CORROSION PRESENT IN MULTIPLE AREAS.
- [SDR DXTA2023101397900](https://openairdocs.org/sdr/DXTA2023101397900.md): Position Switch · damaged · Oct 12, 2023 · N320QS · Cessna 680CE · Door Warning System
  > DESCENDING THROUGH 7000 FEET THE CABIN DOOR OPEN AMBER MESSAGE ILLUMINATED. UPON LANDING THE SIGHT GAUGES SHOWED THE HASH MARKS THAT'S THE PINS WERE IN PLACE. VERIFIED INTERNAL DOOR SWITCHES WERE GAPPED PER THE AMM, VERIFIED THE DOOR LOCK PIN PROX SWITCH GAPP
- [SDR JGVR20230901001](https://openairdocs.org/sdr/JGVR20230901001.md): Unknown · unknown · Sep 1, 2023 · N320QS · Cessna 680CE · Wing, Plate/Skin
  > BLENDED TWO AREAS OF CORROSION ON THE UPPER SURFACE OF THE UPPER INBOARD WING SKIN AT THE TRAILING EDGE OF THE LH WING AND TWO ADDITIONAL AREAS ON THE FORWARD EDGE OF THE SAME SKIN PANEL. PERFORMED NDT AND REPORTED RESULTS FOR REPAIR DISPOSITION. CLEANED, TREA
- [SDR JGVR20230831002](https://openairdocs.org/sdr/JGVR20230831002.md): Unknown · unknown · Aug 31, 2023 · N320QS · Cessna 680CE · Wing Spar
  > MECHANICALLY BLENDED CORROSION AROUND RH WING AFT SPAR #8 SPOILER/SPEED BRAKE RETURN AND PRESSURE FITTINGS. R&R THE BULKHEAD FITTINGS FOR ACCESS. PERFORMED NDT, CLEANED, TREATED, PRIMED AND TOP COATED AREAS PER TEXTRON REPAIR DEFINITION.
- [SDR JGVR20230831001](https://openairdocs.org/sdr/JGVR20230831001.md): Unknown · unknown · Aug 31, 2023 · N320QS · Cessna 680CE · Wing Spar
  > MECHANICALLY BLENDED CORRODED AREAS OF THE AFT SPAR LOWER CAP AND SPAR FACE LOCATED IN THE LH MAIN LANDING GEAR WHEEL, PERFORMED NDT AND REPORTED RESULTS FOR REPAIR DISPOSITION. REPAIRED BLENDED AREAS BY CLEANING, TREATING, PRIMING AND TOP COATING IAW TEXTRON
- [SDR JGVR20230810002](https://openairdocs.org/sdr/JGVR20230810002.md): Unknown · unknown · Aug 10, 2023 · N320QS · Cessna 680CE · Fuselage Structure (General)
  > BLENDED 2 AREAS OF CORROSION ON THE EXTERIOR OF THE FUSELAGE SKIN LOCATED JUST AFT OF THE EMERGENCY EXIT DOOR OPENING, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, PRIMED AND TOP COATED REPAIR AREAS IAW TEXTRON REPAIR MEMO.
- [SDR JGVR20230810001](https://openairdocs.org/sdr/JGVR20230810001.md): Unknown · unknown · Aug 10, 2023 · N320QS · Cessna 680CE · Emergency Exits
  > BLENDED 5 AREAS OF CORROSION ON THE EXTERIOR SKIN OF THE EMERGENCY EXIT DOOR, PERFORMED NDT AND REPORTED RESULTS FOR REPAIR DISPOSITION. CLEANED, TREATED, PRIMED AND TOP COATED REPAIR AREAS IAW TEXTRON FIELD REPAIR.
- [SDR DXTA2022100671670](https://openairdocs.org/sdr/DXTA2022100671670.md): Spring · broken · Oct 5, 2022 · N320QS · Cessna 680CE · Passenger/Crew Doors
  > MAIN DOOR CABLE: MAIN DOOR FORWARD CABLE DOES NOT WORK. REMOVED AND REPLACED MAIN CABIN DOOR FWD AND AFT LUBRICATED SPRINGS AND FWD SUPPORT STRUT ASSY WITH A CUSTOMER SUPPLIED NEW PARTS. PERFOEMED SATISFACTORY OPS CHECKS OF MAIN CABIN DOOR IAW CE-680 AMM 52-10
- [SDR DXTA2022050561270](https://openairdocs.org/sdr/DXTA2022050561270.md): Spring · damaged · May 4, 2022 · N320QS · Cessna 680CE · Passenger/Crew Doors
  > MAIN DOOR: UNABLE TO OPEN MAIN CABIN DOOR FROM INSIDE USING NORMAL METHOD. AFTER FLIGHT/ SHUTDOWN (VERIFIED UNPRESSURIZED) UNABLE TO PRESS IN RED PUSH BUTTON ON MAIN CABIN DOOR HANDLE. HAD TO PUSH AUXILLARY LOCK BUTTON RELEASE HANDLE BEHIND MAIN HANDLE TO GET
- [SDR DXTA2021102250710](https://openairdocs.org/sdr/DXTA2021102250710.md): None · none · Oct 21, 2021 · N320QS · Cessna 680CE · Passenger/Crew Doors
  > MAIN DOOR: WHEN THE MAIN CABIN DOOR IS OPEN, IT DOES NOT FULLY EXTEND THE EXTENSION GUIDE RODS. THERE IS A LITTLE BOUNCE AS PEOPLE BOARD AND DEPLANE FROM THE DOOR MOVING SLIGHTLY UP AND DOWN (NOT THE AIRPLANE SHOCKS). SEEMS IT COULD BE A TRIP HAZARD AS THE D
- [SDR JGVR20210428001](https://openairdocs.org/sdr/JGVR20210428001.md): Rib · corroded · Apr 28, 2021 · N320QS · Cessna 680A · Wing, Rib/Bulkhead
  > MECHANICALLY REMOVED 13 AREAS OF CORROSION IN LH MLG, OUTBD RIB AT WS 67.25 INBD ROW OF FASTENERS. FOUND CORROSION BLENDS TO BE BEYOND C680 SRM 51-70-02 LIMITATIONS. SUBMITTED FINDINGS TO TEXTRON ENGINEERING. REPAIRED 13 CORROSION BLENDS IAW TEXTRON ENGINEERIN
- [SDR JGVR20210413001](https://openairdocs.org/sdr/JGVR20210413001.md): Door Frame · corroded · Apr 13, 2021 · N320QS · Cessna 680A · Fuselage Main, Structure
  > 10+ AREAS OF VERIFIED CORROSION AROUND PERIMETER OF EMERGENCY EXIT DOOR. MECHANICALLY REMOVED 10 AREAS OF CORROSION ON OUTER SKIN OF E-EXIT. PERFORMED AN EDDY CURRENT AND ULTRASONIC THICKNESS CHECK OF THE BLENDED AREAS AROUND THE PERIMETER OF THE EMERGENCY EXI
- [SDR DXTA2020110104330](https://openairdocs.org/sdr/DXTA2020110104330.md): Control Unit · defective · Nov 1, 2020 · N320QS · Cessna 680A · Elevator Control System
  > AT APPROXIMATELY 150' AGL THE PRIMARY TRIM FAIL LIGHT CAME ON AND THE TRIM STARTED TO RUN AWAY NOSE UP. I PRESSED THE AP/TRIM/NWS DISC BUTTON WHICH STOPPED THE NOSE TRIM UP CONDITION. DURING THE PROCESS HEAVY PRESSURE WAS REQUIRED TO STOP THE NOSE FROM RISIN
- [SDR JGVR20201027002](https://openairdocs.org/sdr/JGVR20201027002.md): Spar · corroded · Oct 27, 2020 · N320QS · Cessna 680A · Wing Spar
  > MECHANICALLY REMOVED CORROSION FROM AFT SPAR, LOWER FORWARD SPAR CAP ANGLE LOCATED IN RT WHEEL WELL AT WS35. PERFORMED NDT AND REPORTED RESULTS FOR REPAIR DISPOSITION. CLEANED, TREATED AND TOP COATED REPAIRED AREA, IAW TEXTRON STRUCTURES FIELD REPAIR.
- [SDR EBVR20191022001](https://openairdocs.org/sdr/EBVR20191022001.md): Skin · corroded · Oct 22, 2019 · N320QS · Cessna 680SOV · Fuselage Main, Plate/Skin
  > DURING INSPECTION FOUND CORROSION UNDER FLOORBOARD PANEL 162AC. COMPLIED WITH AQRD ERO-962576 FUSELAGE REPAIR, REVISION IR, DATED OCTOBER 26, 2019. AND 8110-3 DATED: OCT.22,2019.
- [SDR DXTA2019061432496](https://openairdocs.org/sdr/DXTA2019061432496.md): Display · malfunctioned · Jun 13, 2019 · N320QS · Cessna 680CE · Flight Management Computing Hardware System
  > CAPTAIN MCDU BLANK/WENT BLANK - IN FLIGHT ON ARRIVAL WITH APU ON, THE #1 MCDU WENT BLANK AND WE NOTICED WHAT APPEARED TO BE AN ACCOCIATED HOT ELECTRICAL SMELL. WITHIN 2MIN THE MCDU CAME BACK ON
- [SDR JGVR20190419001](https://openairdocs.org/sdr/JGVR20190419001.md): Spar · corroded · Apr 19, 2019 · N320QS · Cessna 680SOV · Wing Spar
  > MECHANICALLY BLENDED AREA OF CORROSION ON AFT SPAR IN LH GEAR WELL, POLISHED, AND PERFORMED NDT FOR REPAIR DISPOSITION. TREATED, TOPCOATED AND REPLACED FASTENER AS REQUIRED PER TEXTRON REPAIR MEMO.
- [SDR DXTA2019011801925](https://openairdocs.org/sdr/DXTA2019011801925.md): Ecs · odor · Jan 17, 2019 · N320QS · Cessna 680CE · Cabin Cooling System
  > CABIN ODOR OIL SMELL - PUNGENT OILY SMELL NOTICED IN COCKPIT/CABIN AT LOW POWER SETTINGS/SPEEDS AT LOW ALTITUDES DURING DESCENT. APU WAS NOT RUNNING.**WAITING FOR SUPPLEMENTAL (RESOLUTION) INFORMATION. **SUPPLEMENTAL(RESOLUTION) INFORMATION - ACCOMPLISHED NJA
- [SDR DXTA2018011100466](https://openairdocs.org/sdr/DXTA2018011100466.md): Oil System · overserviced · Jan 11, 2018 · N320QS · Cessna 680SOV · APU Oil System
  > INFLIGHT AT FL430 PASSENGERS NOTED A STRONG ODOR OF BURNING RUBBER/HOT OIL. NOTED A HOT/BURNING ODOR FROM THE GALLEY AREA. FOUND APU OIL OVERSERVICED DURING A GOLF CHECK. DRAINED APU OIL TO CORRECT SERVICE LEVEL IAW NJA TC-680-21-120905M. REPLACED ECS COALE
- [SDR DXTA2018010400427](https://openairdocs.org/sdr/DXTA2018010400427.md): Switch · failed · Dec 31, 2017 · N320QS · Cessna 680SOV · Landing Gear Retraction/Extension System
  > ON DEPARTURE, HAD TO CYCLE THE GEAR 3 - 4 TIMES BEFORE FINALLY LOCKING INTO PLACE. REMOVED THE NOSE GEAR SQUAT SWITCH AND ACTUATING CAM. INSTALLED NEW SWITCH AND CAM. PERFORMED NOSE GEAR LUBRICATION AND SERVICED NOSE GEAR STRUT. PERFORMED LANDING GEAR EXTENS
- [SDR DXTAT2PL6D005MNZR](https://openairdocs.org/sdr/DXTAT2PL6D005MNZR.md): Cam · defective · Dec 29, 2017 · N320QS · Cessna 680SOV · Landing Gear Position and Warning
  > ON DEPARTURE, THE LANDING GEAR WOULD NOT RETRACT. ICE AND SLUSH ON THE GEAR ARE PROBABLY THE REASON. REMOVED THE NOSE GEAR SQUAT SWITCH ACTUATING CAM. INSTALLED A NEW SWITCH CAM AND HARDWARE. PERFORMED NOSE GEAR LUBRICATION AND SERVICED NOSE GEAR STRUT. PE
- [SDR DXTA201801010001](https://openairdocs.org/sdr/DXTA201801010001.md): Unknown · malfunctioned · Dec 29, 2017 · N320QS · Cessna 680SOV · Landing Gear Retraction/Extension System
  > ON DEPARTURE THE LANDING GEAR WOULD NOT RETRACT. ICE AND SLUSH ON THE GEAR ARE PROBABLY THE REASON.
- [SDR JGVR20171220001](https://openairdocs.org/sdr/JGVR20171220001.md): Spar Cap · corroded · Dec 20, 2017 · N320QS · Cessna 680CE · Wing Spar
  > FOUND CORROSION AROUND TWO LOCK FASTENERS LOCATED IN THE RT WING LOWER SPAR CAP NEAR RWS 49.50. REMOVED AFFECTED LOCK FASTENERS, PERFORMED BLEND AND TREAT REPAIR, AND REPLACED THE FASTENERS WITH NEW 10563M1 RRL.
- [SDR 2017F00047](https://openairdocs.org/sdr/2017F00047.md): Fitting · corroded · Feb 17, 2017 · N320QS · Cessna 680SOV · Wing Spar
  > AFT WING SPAR BULKHEAD FITTING CORRODED.
- [SDR DXTA2016091306301](https://openairdocs.org/sdr/DXTA2016091306301.md): Uplock Switch · out of rig · Sep 13, 2016 · N320QS · Cessna 680CE · Landing Gear Position and Warning
  > IN FLIGHT LEVEL 41,000, HEARD AND FELT A THUNK NOISE FROM THE FRONT OF THE PLANE. THE RED LANDING GEAR UNLOCK LIGHT ILLUMINATED BUT THERE WERE NO UNUSUAL RUMBLE NOISES OR DRAG INDICATIONS AS IF A GEAR EXTENDED. SUSPECT THE NOSE GEAR DOORS HELD THE GEAR FROM
- [SDR DXTA2014052005776](https://openairdocs.org/sdr/DXTA2014052005776.md): Power Supply · failed · May 19, 2014 · N320QS · Cessna 680CE · Instrument Panel
  > DURING CRUISE AT FL410, FIRST MONITOR WARNING FAIL CAS MESSAGE, FOLLOWED BY MONITOR WARNING FAIL RT IN DESCENT. ALSO MAU 1 & 2 FAIL, GPS 2 INACTIVE, TAWS FAILURE, LOSS OF ALL PIC FLIGHT INSTRUMENTS, INTERMITTENT LOSS OF ALL SIC FLIGHT INSTRUMENTS, LOSS OF FM
- [SDR DXTA2014031705691](https://openairdocs.org/sdr/DXTA2014031705691.md): Power Supply · failed · Mar 16, 2014 · N320QS · Cessna 680CE · Central Computers
  > BOTH MAU1 & MAU2 FAILED. REPLACED MAU 1 & 2 POWER SUPPLIES & NIC PROCESSOR IAW MM 34-17-00. LOADED SOFTWARE & OPS CHECKED WITH NO FAULTS NOTED.
- [SDR DXTA2014031705689](https://openairdocs.org/sdr/DXTA2014031705689.md): Starter Gen · failed · Mar 15, 2014 · N320QS · Cessna 680CE · Starter-Generator
  > DURING CRUISE AT FLIGHT LEVEL 410, RECEIVED AN AMBER DC GENERATOR OFF LIGHT & AN AMBER DC EMERGENCY BUSS LIGHT, CAS MESSAGE. LOST THE NR 1 DISPLAY UNIT, THE NR 3 DISPLAY UNIT & LOST THE FLAPS & AUTOPILOT. CHECKLIST INDICATED A GENERATOR OVER CURRENT WAS AT F
- [SDR CWQD201101](https://openairdocs.org/sdr/CWQD201101.md): Pump · leaking · Jan 26, 2011 · N320QS · Cessna 680SOV · Hydraulic Pump (Electric/Engine), Main
  > DURING UNSCHEDULED MX, THE RT ENGINE HYD PUMP WAS REPLACED DUE TO INTERNAL LEAKAGE.

## 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 = 'N320QS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N320QS/reports

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