N368QS, cancelled Jul 26, 2025

Service difficulty reports · 35

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 = 'N368QS' AND deregistration_id = 'N368QS-2025-07-26'
  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.

SDR DXTA2025032402799Cable · out of adjustMAIN 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 TENSIMar 23, 2025 · N368QS · Cessna 680SOV · Passenger/Crew DoorsSDR DXTA2024120501384Processor · defectiveON 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 RECENTEDec 3, 2024 · N368QS · Cessna 680SOV · Autopilot SystemSDR 2024FA0000815Skin · corrodedREPAIRED 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 ACCORDNov 4, 2024 · N368QS · Cessna 680CE · Fuselage Main, Plate/SkinSDR 2024FA0000784Closeout Panel · corrodedMECHANICALLY 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 SERVOct 22, 2024 · N368QS · Cessna 680CE · Passenger/Crew DoorsSDR DXTA2023070390280Unknown · unknownVIBRATION 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 CHECKJul 3, 2023 · N368QS · Cessna 680CE · Fuselage Structure (General)SDR DXTA2023060788130Coalescer Bag · dirtyON 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 Jun 7, 2023 · N368QS · Cessna 680CE · Air Conditioning SystemSDR DXTA2023060688010Unknown · unknownSMOKE 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 AUTOJun 6, 2023 · N368QS · Cessna 680SOV · Air Conditioning SystemSDR DXTA2023051085740Unknown · unknownCABIN 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.May 9, 2023 · N368QS · Cessna 680CE · Emergency LightingSDR DXTA2022072966940Battery · defectiveCABIN 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 Jul 29, 2022 · N368QS · Cessna 680A · Emergency LightingSDR DXTA2021052442470Blade · missingENGINE 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 MESSAGMay 22, 2021 · N368QS · Cessna 680CE · Engine (Turbine/Turboprop)SDR JGVR20201215001Spar · damagedBLENDED 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.Dec 15, 2020 · N368QS · Cessna 680CE · Vertical Stabilizer, Spar/RibSDR JGVR2020124001Spar · corrodedREMOVED 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 FASTENEDec 14, 2020 · N368QS · Cessna 680CE · Wing SparSDR JGVR20191220001Skin · corrodedMECHANICALLY 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 AREADec 20, 2019 · N368QS · Cessna 680CE · Fuselage Main, Plate/SkinSDR JGVR20191219001Door Frame · corrodedFOUND CORROSION OUT OF LIMITS ON THE EMERGENCY EXIT DOOR LOCATED UNDERNEATH THE CONTOUR RINGS, REPLACED THE EMERGENCY EXIT DOOR WITH NEW TEXTRON PART.Dec 19, 2019 · N368QS · Cessna 680CE · Fuselage Main, StructureSDR DXTA2019FA0000015Skin · gougedLT NOSE SKIN DAMAGE (GOUGES), REF ENGINEERING LETTER DQ17110M1, DATED JAN 17, 2019Jan 20, 2019 · N368QS · Cessna 680CE · Fuselage Main, Plate/SkinSDR DXTA2018010100518Switch · faultyCLIMBING 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 SN0Jan 31, 2018 · N368QS · Cessna 680CE · Door Warning SystemSDR JGVR20170630002Skin · corrodedTHE 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. REPAJun 30, 2017 · N368QS · Cessna 680SOV · Rudder, Plate/SkinSDR JGVR20170630001Skin · corrodedMAIN 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.Jun 30, 2017 · N368QS · Cessna 680SOV · Passenger/Crew DoorsSDR DXTA2015081106055Brake · chatteringBRAKES 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.Aug 10, 2015 · N368QS · Cessna 680CE · BrakeSDR DXTA2014092605896Oil System · overservicedSTARTED 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 Sep 25, 2014 · N368QS · Cessna 680CE · APU Oil SystemSDR DXTA2014090505873Brake Sys · contaminatedON 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.Sep 4, 2014 · N368QS · Cessna 680CE · Landing Gear Brake SystemSDR DXTA2013101405543Line · crackedAFTER 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 Oct 20, 2013 · N368QS · Cessna 680CE · Landing Gear Retraction/Extension SystemSDR DXTA2013072305454Strut · low pressureLANDING 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.Jul 22, 2013 · N368QS · Cessna 680CE · Landing Gear Retraction/Extension SystemSDR DXTA2013062105421Anti-Skid Sys · failedON 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, AJun 20, 2013 · N368QS · Cessna 680CE · Landing Gear System WiringSDR DXTA2013041105353Oil System · leakingAFTER 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 WERApr 10, 2013 · N368QS · Cessna 680CE · APU Oil SystemSDR DXTA2012090605117Door Frame · corrodedCABIN DOOR FORWARD FRAME CORRODED AT SHEAR TIE FITTING. REMOVED SURFACE CORROSION IAW SRM 51-20-01. INSTALLED DOOR FRAME IAW SRM 51-40-03.Sep 4, 2012 · N368QS · Cessna 680CE · Fuselage Main, StructureSDR DXTA2012082905108Door Frame · corrodedMAIN ENTRY DOOR FRAME CORRODED. FOUND DURING INSPECTION.Aug 23, 2012 · N368QS · Cessna 680CE · Fuselage Main, StructureSDR DXTA2011071204657Starter Gen · failedDURING 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. UNJul 12, 2011 · N368QS · Cessna 680CE · Starter-GeneratorSDR DXTA2011042504558Circuit Board · inoperativePRIMARY 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 CONTApr 24, 2011 · N368QS · Cessna 680CE · Stabilizer Control SystemSDR DXTA2010102904283Engine · malfunctionedDECENDING 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 THOct 23, 2010 · N368QS · Cessna 680CE · Engine (Turbine/Turboprop)SDR DXTA200702428Engine · power lossAFTER 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 SQUAug 24, 2007 · N368QS · Cessna 680CE · Engine (Turbine/Turboprop)SDR DXTA200702165Switch · out of adjustFRONT 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.May 1, 2007 · N368QS · Cessna 680CE · Landing Gear Position and WarningSDR DXTA200601763Actuator · inoperativeAUTOPILOT 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.Nov 29, 2006 · N368QS · Cessna 680CE · Autopilot SystemSDR DXTA200601693Electrical Box · shorted(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 TRIPPEDOct 27, 2006 · N368QS · Cessna 680CE · Flight Control System WiringSDR DXTA20061691Electrical Box · inoperative"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 TRIPPEOct 27, 2006 · N368QS · Cessna 680CE · Leading Edge Slat Control System
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