N313QS

Service difficulty reports · 54

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 = 'N313QS' 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.

SDR JGVR20260516201Skin · corrodedBLENDED MULTIPLE AREAS OF CORROSION ON THE UPPER AND LOWER SKINS OF THE HORIZONTAL STABILIZER, NEAR LT AND RT TIP CAP, LH AND RH IB ELEVATOR HINGE, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, PRIMED, AND TOPCOATED AREAS.May 16, 2026 · N313QS · Cessna 680CE · Horizontal Stabilizer, Plate/SkinSDR JGVR20260515204Skin · corrodedMECHANICALLY REMOVED 1 AREA OF CORROSION ON THE UPPER AFT CORNER OF THE CUT OUT OF THE E-EXIT ON FUSELAGE SKIN, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.May 15, 2026 · N313QS · Cessna 680CE · Fuselage Main, Plate/SkinSDR JGVR20260515203Spar · corrodedMECHANICALLY REMOVED CORROSION LOCATED ON RH WING AFT SPAR, AFT FACE OF SPAR WEB BELOW SPOILER PANEL #9 AROUND PRESSURE AND RETURN HYDRAULIC LINE CARRY THROUGH FITTINGS, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED AREAS PER May 15, 2026 · N313QS · Cessna 680CE · Wing SparSDR JGVR20260515202Spar Cap · corrodedMECHANICALLY REMOVED 2 AREAS OF CORROSION LOCATED INSIDE LH HORIZONTAL STAB ELEVATOR COVE, LOWER SPAR CLIP BETWEEN INBOARD AND MIDDLE ELEVATOR HINGE ATTACHMENTS, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED AREAS PER NETJETS May 15, 2026 · N313QS · Cessna 680CE · Horizontal Stabilizer, Spar/RibSDR JGVR20260515001Skin · corrodedMECHANICALLY REMOVED 1 AREA OF CORROSION AND 1 AREA OF BARE METAL LOCATED ON LH HORIZONTAL STAB UPPER SKIN NEAR INBOARD ELEVATOR HINGE, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. FABRICATED AND INSTALLED REPAIR DOUBLERS PER NETJETS REQUEST FOR TECHNICAMay 15, 2026 · N313QS · Cessna 680CE · Horizontal Stabilizer, Plate/SkinSDR JGVR20260515201Skin · corrodedMECHANICALLY REMOVED 1 AREA OF CORROSION AND 1 AREA OF BARE METAL LOCATED ON LH HORIZONTAL STAB UPPER SKIN NEAR INBOARD ELEVATOR HINGE, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. FABRICATED AND INSTALLED REPAIR DOUBLERS PER NETJETS REQUEST FOR TECHNICAMay 15, 2026 · N313QS · Cessna 680CE · Horizontal Stabilizer, Plate/SkinSDR 2025FA0000779Wing Root · corrodedCORROSION FOUND WHERE LT AND RT WING AND FUSELAGE MEET.Nov 21, 2025 · N313QS · Cessna 680CE · Fuselage, Wing Attach FittingsSDR 2025FA0000771Wing Root · corrodedCORROSION FOUND WHERE LT AND RT WING AND FUSELAGE MEET.Nov 19, 2025 · N313QS · Cessna 680CE · Wing, Fuselage Attach FittingsSDR 2025FA0000740Skin · corrodedCORROSION FOUND ON TAIL AROUND AIRCRAFT DATA PLATE AND JUST AFT OF DATA PLATE. PERFORMED EDDY CURRENT INSPECTION FOR CRACKS AND CORROSION ON BLENDED AREAS LOCATED ON AFT FUSELAGE AROUND AIRCRAFT DATA PLATE AND JUST AFT OF DATE PLATE. PERFORMED ULTRASONIC REMAINov 4, 2025 · N313QS · Cessna 680CE · Fuselage Main, Plate/SkinSDR 2025FA0000739Skin · corrodedCORROSION FOUND ON TAIL AROUND AIRCRAFT DATA PLATE AND JUST AFT OF DATA PLATE. PERFORMED EDDY CURRENT INSPECTION FOR CRACKS AND CORROSION ON BLENDED AREAS LOCATED ON AFT FUSELAGE AROUND AIRCRAFT DATA PLATE AND JUST AFT OF DATE PLATE. PERFORMED ULTRASONIC REMAINov 4, 2025 · N313QS · Cessna 680CE · Fuselage Main, Plate/SkinSDR DXTA2025060603759Battery Pack · inoperativeLIGHTS CONNECTED TO THEIR RESPECTIVE EMERGENCY LIGHTING BATTERY PACK FAILED TO OPERATE AFTER TWO 30 MINUTE CHARGING SESSIONS. THE TWO LOWER SIDES OF MAIN CABIN DOOR FRAME, ONE ABOVE EMERGENCY EXIT, ONE ON BULKHEAD BEHIND SEAT 9. CORRECTIVE ACTION: REMOVED AND Jun 3, 2025 · N313QS · Cessna 680SOV · Emergency LightingSDR 2024FA0000757Skin · corrodedREPAIRED CORRODED AREAS OF THE VERTICAL STABILIZER SKINS LOCATED NEAR THE UPPER EDGE AND ONE NEAR THE FORWARD EDGE BY BLENDING, PERFORMING NDT, REPORTING FOR REPAIR DEPOSITION, CLEANING, TREATING, PRIMING AND FABRICATING AND INSTALLING REPAIR DOUBLERS IAW AEROOct 7, 2024 · N313QS · Cessna 680A · Vertical Stabilizer, Plate/SkinSDR DXTA2024090300378Fuse · defectiveEMERG EXIT SIGN/LIGHT: THE AFT LAV EMERGENCY EXIT SIGN IS INOP. THE AFT DIVIDER OVERHEAD EMERGENCY EXIT SIGN IS INOP. CORRECTIVE ACTION: CHECKED THE EMERGENCY POWER SUPPLY BATTERY #4 FUSE AND FOUND IT BURNT. PERFORMED WIRING CHECK AND FOUND WIRES GOING TO THE Aug 29, 2024 · N313QS · Cessna 680SOV · Emergency LightingSDR DXTA2024062512164Fadec · faultedDURING DESCENT FROM FL350 WITH ANTI-ICE ON THE ENGINE CONTROL FAULT R AMBER CAS MESSAGE ILLUMINATED. FAULT MESSAGE WAS RESET AFTER PUSHING THE FADEC RESET. REMOVED PN HG1153CA04, SN 08053096 DUE TO "RH ENG CONTROL FAULT" CAS MESSAGE. INSTALLED A REPAIRED UNJun 25, 2024 · N313QS · Cessna 680CE · Fuel Controlling SystemSDR DXTA2023082894000Fuse · blownON PREFLIGHT, ALL EMERGENCY LIGHTS INTERIOR AND EXTERIOR DO NOT ILLUMINATE WITH THE EMER LTS SELECTED ON. IN ARM, AFT EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE. MET WITH CREW AND VERIFIED DISCREPANCY. GAINED ACCESS TO #4 EMER LIGHT POWER SUPPLY AND INSPECTED COAug 27, 2023 · N313QS · Cessna 680CE · Emergency LightingSDR JGVR20230720001Unknown · unknownREPAIRED CRACKED INBOARD END RIB OF THE RH HORIZONTAL STABILIZER, LOWER FLANGE AT RBL 8.8, PER REPAIR -2 OF TEXTRON REPAIR DEFINITION S-680-ATA55/08RD REVISION – BY NDT MAPPING CRACK, TRIMMING CRACKED AREA, FABRICATING AND INSTALLING REPAIR PIECES.Jul 20, 2023 · N313QS · Cessna 680CE · Horizontal Stabilizer StructureSDR DXTA2022112374570Coalescer Bag · dirtyDEPARTED APF, APU OFF FOR TAKEOFF. LEVELED OFF AT 2000 FT PER CLEARANCE & NOTICED A HOT BURNING OIL ODOR, REDUCED POWER AT 2,000 FT TO KEEP A SLOW AIRSPEED, ODOR BEGAN TO EASE. VISUAL INSP SHOWED NO OIL ON ENG COWLINGS OR UNDER APU. OIL LEVELS CHECKED GNov 22, 2022 · N313QS · Cessna 680CE · Air Distribution SystemSDR DXTA2022062764570Acm · defectiveAPU BLEED AIR: COULD NOT CONTROL CABIN TEMP BELOW 80 DEGREES. STARTED APU AND SELECTED BLEED AIR ON. ODOR OF BURNT OIL ENTERED CABIN AND THEN BLEED SELECTED OFF. ON GROUND BEFORE FLIGHT THERE WAS NO ODOR W BLEED AIR ON. APU WAS STARTED AFTER SLOWING AIJun 24, 2022 · N313QS · Cessna 680A · APU Cowling/ContainmentSDR DXTA2022011755260Battery Pack · inoperativeEMERGENCY LIGHTING: WHEN DOING THE EMERGENCY LIGHT CHECK, THE ONLY LIGHTS WORKING ARE THE EXIT LIGHT OVER THE MAIN CABIN DOOR, THE OVERHEAD LIGHT BETWEEN SEATS 3 AND 5 AND THE OVERHEAD LIGHT OVER SEAT 9. THE DOORFRAME EXIT SIGNS, THE AISLE LIGHTING, THE DIVIJan 15, 2022 · N313QS · Cessna 680CE · Emergency LightingSDR DXTA2021123154490Unknown · unknownCABIN EMERG LIGHT: RIGHT SIDE CABIN EMERGENCY LIGHTS INOP. LEFT SIDE OPERATES NORMALLY. // SIGNOFF// RAN APU FOR 1 HOUR TO CHARGE THE EMERGENCY BATTERIES. PREFORMED OPS CHECK OF THE EMERGENCY LIGHTS AND NO DEFECTS FOUND JAW SOVEREIGN 680 AMM 33-50-00Dec 30, 2021 · N313QS · Gulstm 680 · Emergency LightingSDR DXTA2021121553510Controller · defectiveANTISKID FAIL AMBER CAS: ON CLIMB OUT WE HAD A FLICKERING AMBER ANTISKID FAIL CAS MESSAGE. THE CHECKLIST HAD US TURN IT OFF SINCE THE MESSAGE WOULD NOT CLEAR. WE LANDED IN THE OFF POSITION. // SIGNOFF // REMOVED THE ANTI-SKID CONTROLLER AND INSTALLED SERVICEABDec 13, 2021 · N313QS · Cessna 680CE · Brake Anti-Skid SectionSDR JGVR20210319003Skin · corrodedBLENDED CORRODED AREAS OF THE LOWER SURFACE OF THE RH LOWER WING SKIN, BELOW THE AFT SPAR CAP NEAR THE MAIN LANDING GEAR WHEEL WELL AREA, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPLACED BLENDED FASTENERS AS REQUIRED, TREATED, PRIMED, AND TOP COATEDMar 19, 2021 · N313QS · Cessna 680CE · Wing, Plate/SkinSDR DXTA022220213833Wheel · icedRIGHT INBOARD MLG TIRE: BRAKE FROZEN. TIRE DAMAGED. WE FOUND THAT THERE WAS ICE BUILD-UP 0F THE RT INBOARD BRAKE. AFTER REMOVING THE ICE WE WERE ABLE TO TURN THE WHEEL AND WE CONFIRMED THAT THE TIRE WILL NEED TO BE REPLACED. WE REMOVED THE MLG WHEEL ASSY REFeb 18, 2021 · N313QS · Cessna 680CE · Wheel/Ski/FloatSDR DXTA021920213833Brake · frozenRIGHT INBOARD MLG TIRE: BRAKE FROZEN. TIRE DAMAGED.Feb 18, 2021 · N313QS · Cessna 680CE · Landing Gear Brake SystemSDR JGVR202002192001Spar · corrodedVERTICAL STAB HAS 1 AREA OF VERIFIED CORROSION ON LH SPAR CLIP BELOW UPPER RUDDER HINGE. FOUND DURING 6 MONTH INSPECTION. REMOVED LEVEL 1 CORROSION FROM VERTICAL STAB LH SPAR CLIP BELOW UPPER RUDDER HINGE IAW CESSNA 680 SRM 51-70-02. FOUND BLENDED AREA TO BE BFeb 20, 2020 · N313QS · Cessna 680A · Vertical Stabilizer, Spar/RibSDR DXTA2019111403074Strut · stuckALL LANDING GEAR RETRACTION DID NOT RETRACT - WHEN NOSEWHEEL CAME OFF THE GROUND ON TAKEOFF, THE MASTER WARNING LIGHT ILLUMINATED. THE GEAR HANDLE WOULD NOT MOVE AND "WOW MISCOMPARE" AMBER CAS MESSAGE DISPLAYED. "CORRECTIVE ACTION" TROUBLESHOT LANDING GEAR SYSNov 13, 2019 · N313QS · Cessna 680CE · Nose/Tail Landing Gear Strut/AxleSDR DXTA2018030800694Compressor · stalledDURING CLIMB OUT, AT APPROXIMATELY FL 350 IN MCT THRUST, THERE WERE SEVERAL ENGINE COMPRESSOR STALLS ON THE RT ENGINE. DURING THE STALLS THE ITT EXCEEDED 900. THE STALLS WERE SEVERE ENOUGH TO CAUSE THE AIRPLANE TO YAW. THE STALLS WENT AWAY WHEN POWER WAS REDUCMar 8, 2018 · N313QS · Cessna 680CE · Turbine Engine Compressor SectionSDR DXTA2018010400434Unknown · smokeSHORTLY AFTER STARTING THE APU AND SELECTING BLEED ON, A GRAYISH SMOKE COULD BE SMELLED AND SEEN THROUGHOUT THE CABIN AND COCKPIT. SMOKE DISSIPATED AFTER APU SHUT DOWN.Jan 2, 2018 · N313QS · Cessna 680SOV · Air Distribution SystemSDR DXTAT2PL6D005MFJNBleed Valve · defectiveAT CRUISE FL340, THE AIRPLANE MADE A LOUD POP, THEN A BANG, FOLLOWED BY A VIBRATION , YAW, AND ITT OVERTEMP/ N1 OVERSPEED ON THE RIGHT ENGINE. BOTH POWER LEVERS REDUCED IMMEDIATELY. BOTH ENGINE PARAMETERS INDICATED NORMAL RANGES. FLIGHT RETURNED TO DEPARTURE ADec 27, 2017 · N313QS · Cessna 680CE · Compressor Bleed ValveSDR JGVR20170823001Door · corrodedEMERGENCY EXIT DOOR SKIN HAS SEVERAL AREAS OF CORROSION AROUND PERIPHERY NEAR COMPOSITE RING. FOUND DURING PAINT PROCESS. REMOVED SEAL AND COMPOSITE RINGS AND BLENDED CORROSION. CORROSION FOUND TO BE BEYOND LIMITS. REMOVED THE EMERGENCY EXIT DOOR, AND INSTAAug 23, 2017 · N313QS · Cessna 680CE · Emergency ExitsSDR 2017F00165Fairing · damagedFAIRING DAMAGE.Jul 13, 2017 · N313QS · Cessna 680CE · Aerodynamic FairingsSDR 2017F00156Skin · corrodedVERTICAL STABILIZER LEFT AND RIGHT SKIN DAMAGE.Jul 12, 2017 · N313QS · Cessna 680CE · Vertical Stabilizer, Plate/SkinSDR 2017F00151Skin · corrodedHORIZONTAL STABILIZER LEFT AND RIGHT UPPER AND LOWER SKIN DAMAGE.Jul 7, 2017 · N313QS · Cessna 680CE · Horizontal Stabilizer, Plate/SkinSDR 2017F00149Spar · damagedVERTICAL FIN REAR SPAR DAMAGED.Jul 6, 2017 · N313QS · Cessna 680CE · Vertical Stabilizer, Spar/RibSDR 2017F00147Bulkhead · damagedBULKHEAD BOND ASSY. DAMAGED, DOUBLER CRACKED, NICKED AND DEBONDED.Jul 6, 2017 · N313QS · Cessna 680CE · Nacelle/Pylon, Bulkhead/FirewallSDR 2017F00146Hinge Bracket · corrodedRUDDER HINGE BRACKET CORRODED.Jul 6, 2017 · N313QS · Cessna 680CE · Rudder StructureSDR 2017F00145Access Panel · delaminatedVERTICAL STAB LEADING EDGE UPPER LEFT EDGE DELAMINATED.Jul 6, 2017 · N313QS · Cessna 680CE · Vertical Stabilizer, Plate/SkinSDR 2017F00144Skin · corrodedLEFT ELEVATOR SKIN CORRODED.Jul 6, 2017 · N313QS · Cessna 680CE · Elevator, Plate/SkinSDR DXTR2016031003Skin · corrodedCORROSION FOUND AT DISCRETE LOCATIONS ON THE STR AND TAILCONE SKINS. REPAIRED IAW STRUCTURES REPORT S-680-0140/04RD.Mar 4, 2016 · N313QS · Cessna 680SOV · Fuselage Main, Plate/SkinSDR DXTR2016031002Skin · corrodedCORROSION FOUND AT MULTIPLE SITES ON THE LT & RT VERTICAL STABILIZER SKINS. REPAIRED IAW STRUCTURES REPORT NR: S-680-014/05RD.Mar 4, 2016 · N313QS · Cessna 680SOV · Vertical Stabilizer, Plate/SkinSDR DXTR2016031001Skin · corrodedCORROSION DAMAGE FOUND ON LT UPPER WING SKIN. REPAIRED IAW STRUCTURES REPORT NR: S-680-0140/06RD.Mar 4, 2016 · N313QS · Cessna 680SOV · Wing, Plate/SkinSDR DXTA2014080605845Control Handle · faultyGEAR WOULD NOT RETRACT, GEAR HANDLE COULD NOT BE MOVED. AFTER ACFT WAS JACKED BROUGHT UP CDMS TO LANDING GEAR PAGE. WITH NO HYD TRIED TO PULL GEAR HANDLE BUT HANDLE WOULD NOT PULL FROM DOWN POSITION. VIEWED CDMS & CORRECT COMMANDS WHERE PRESENT POWER & GND Jul 4, 2014 · N313QS · Cessna 680CE · Landing Gear SelectorSDR DXTA2014080605844Control Handle · faultyGEAR WOULD NOT RETRACT, GEAR HANDLE COULD NOT BE MOVED. REMOVED GEAR HANDLE & BENCH CHECKED SOLENOID OPERATION. APPLIED POWER & GND, HANDLE REMAINS LOCKED DOWN. INTERMITTENTLY HANDLE WILL UNLOCK. SOLENOID COIL HAS EXCESSIVE RESISTANCE. GEAR HANDLE ASSEMBLJul 2, 2014 · N313QS · Cessna 680CE · Landing Gear SelectorSDR CWQR20131203049Filter Element · mismanufacturedDURING A SCHEDULED INSPECTION WE TRIED TO INSTALL A NEW FILTER ELEMENT. THE ELEMENT WOULD NOT SIT INTO THE BOTTOM OF THE FILTER HOUSING BOWL. THE FILTER WAS REJECTED & RED TAGGED BY THE TECHNICIAN & RETURNED TO THE MATERIALS DEPARTMENT. WE HAD IN THE PAST RDec 3, 2013 · N313QS · Cessna 680CE · Hydraulic Filter, MainSDR DXTA2013111205562Engine · malfunctionedAPPROXIMATELY 20 MIN INTO FLIGHT AT FL430, CREW NOTICED A HOT SMELL. 5 MINUTES LATER A WHITE GRAY SMOKE ENTERED THE COCKPIT & CABIN. THE PRESS SOURCE SELECT KNOB WAS SELECTED TO L IAW ENVIRONMENTAL SMOKE CHECKLIST. SMOKE DISSIPATED DURING DESCENT & LANDING Nov 11, 2013 · N313QS · Cessna 680CE · Engine (Turbine/Turboprop)SDR DXTA2013100705531Engine · odorSMOKE IN CABIN AT FL 430. DURING CLIMBOUT ABOUT 14,000 APU SYS FAIL ANNUNCIATOR CAME ON AND APU SHUTDOWN. APU GEN HAD BEEN OFF, BUT BLEED AIR ON. APPROX 30 MINUTES LATER, LEVEL AT FL 430 ADVISED OF A LITTLE SMOKY IN CABIN. FINE GREY ENVIRONMENTAL SMOKE/HAZE Oct 7, 2013 · N313QS · Cessna 680CE · Engine (Turbine/Turboprop)SDR DXTA2013053105404Bearing · dirtyNOSE GEAR MADE LOUD BANGING NOISE UPON GEAR RETRACTION, SHOOK GLARE SHIELD. NOSE STRUT WITHIN LIMITS RETRACTION GUIDES SEEM TO ALIGNED CORRECTLY. CYCLED GEAR, UNABLE TO DUPLICATE. CHECKED SERVICE OF NOSE STRUT FOUND LOWER CHAMBER TO BE LOWER AT 15 PSI. May 30, 2013 · N313QS · Cessna 680CE · Wheel/Ski/FloatSDR DXTA2013051305392Coalescer Bag · dirtyGETTING AN INTERMITTENT ACRID "DIRTY SOCK" ODOR IN CABIN DURING FLIGHT WITH APU OFF. R & R THE WATER SEPARATOR COALESCER IAW MM 21-21-03, 21-50-00. THE OPS AND LEAK CHECKS ARE SATISFACTORY. THERE WAS NO EVIDENCE OR ANY OIL IN THE WATER SEPARATOR.May 12, 2013 · N313QS · Cessna 680CE · Humidity Control SystemSDR DXTA2011092304734Ecu · failedUPON CLIMBING TO CRUISE ALTITUDE, BRIEF ODOR OF "HEAT" WAS NOTED IN THE COCKPIT. FOLLOWED LATER BY THE PASSENGERS WHO ALERTED THE CREW TO WHITE SMOKE COMING FROM BACK OF THE CABIN. A DIVERSION WAS DECLARED AND UPON REDUCTION OF POWER, SMOKE SOMEWHAT ABBATED Sep 22, 2011 · N313QS · Cessna 680CE · Cabin Cooling SystemSDR 2011FA0000090Connector · damagedWHILE PERFORMING THE 2B INTERNAL WING INSP, FOUND THAT THE LT AND RT ELECTRICAL CONNECTOR BLANKING PINS WERE FALLING OUT BECOMING FOD IN THE CTR FUEL TANK. CONNECOTRS ARE LOCATED IN FUEL ACCESS PANELS 175AB AND 176AB, ON THE FWD WALL.Jan 11, 2011 · N313QS · Cessna 680CE · Fuel System Wiring
Back to N313QS