N320QS
Service difficulty reports · 44
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "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"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DXTA2026061808462Battery · faultySEVERAL 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 INSDR JGVR20251117002Skin · corrodedREPAIRED 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 JGVR20251117001Skin · corrodedMECHANICALLY 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 JGVR20251113002Skin · corrodedFOUND 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 TRESDR JGVR20251112002Skin · corrodedBLENDED 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 REQSDR JGVR20251112001Skin · corrodedFOUND 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 DOUBLSDR JGVR20251111002Tail Cone · corrodedREPAIRED 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 JGVR20251111001Skin · corrodedREPAIRED 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 JGVR20251110003Skin · corrodedMECHANICALLY 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 JGVR20251110002Skin · corrodedBLENDED 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 JGVR20251110001Skin · corrodedMECHANICALLY 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 JGVR20250910002Skin · corrodedMECHANICALLY 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 TSDR JGVR20250910001Angle · corrodedMECHANICALLY 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 2024F00254Fairing · damagedDURING 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 2024FA0000761Case · gougedN320QS (680-0169) RH ENGINE CASE GOUGE.SDR 2024F00248Doubler · corrodedTHE LH AND RH WING FUEL PANELS HAVE CORROSION PRESENT IN MULTIPLE AREAS.SDR DXTA2023101397900Position Switch · damagedDESCENDING 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 GAPPSDR JGVR20230901001Unknown · unknownBLENDED 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, TREASDR JGVR20230831002Unknown · unknownMECHANICALLY 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 JGVR20230831001Unknown · unknownMECHANICALLY 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 JGVR20230810002Unknown · unknownBLENDED 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 JGVR20230810001Unknown · unknownBLENDED 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 DXTA2022100671670Spring · brokenMAIN 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 52-10SDR DXTA2022050561270Spring · damagedMAIN 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 DXTA2021102250710None · noneMAIN 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 DSDR JGVR20210428001Rib · corrodedMECHANICALLY 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 ENGINEERINSDR JGVR20210413001Door Frame · corroded10+ 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 EXISDR DXTA2020110104330Control Unit · defectiveAT 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 RISINSDR JGVR20201027002Spar · corrodedMECHANICALLY 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 EBVR20191022001Skin · corrodedDURING 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 DXTA2019061432496Display · malfunctionedCAPTAIN 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 ONSDR JGVR20190419001Spar · corrodedMECHANICALLY 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 DXTA2019011801925Ecs · odorCABIN 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 DXTA2018011100466Oil System · overservicedINFLIGHT 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 COALESDR DXTA2018010400427Switch · failedON 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 EXTENSSDR DXTAT2PL6D005MNZRCam · defectiveON 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. PESDR DXTA201801010001Unknown · malfunctionedON DEPARTURE THE LANDING GEAR WOULD NOT RETRACT. ICE AND SLUSH ON THE GEAR ARE PROBABLY THE REASON.SDR JGVR20171220001Spar Cap · corrodedFOUND 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 2017F00047Fitting · corrodedAFT WING SPAR BULKHEAD FITTING CORRODED.SDR DXTA2016091306301Uplock Switch · out of rigIN 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 DXTA2014052005776Power Supply · failedDURING 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 FMSDR DXTA2014031705691Power Supply · failedBOTH 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 DXTA2014031705689Starter Gen · failedDURING 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 FSDR CWQD201101Pump · leakingDURING UNSCHEDULED MX, THE RT ENGINE HYD PUMP WAS REPLACED DUE TO INTERNAL LEAKAGE.
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