# Service difficulty reports: N317QS A list on [N317QS](https://openairdocs.org/aircraft/N317QS.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR DXTA2026041507632](https://openairdocs.org/sdr/DXTA2026041507632.md): G Switch · tripped · Apr 12, 2026 · N317QS · Cessna 680SOV · Emergency Lighting > WITH MAIN BATTERIES OFF AND ALSO DISCONNECTED (EMERGENCY LIGHTS ALSO OFF), 3 CABIN LIGHTS INLINE WITH THE EMERGENCY LIGHTING SYSTEM (LEFT FORWARD TABLE AND LEFT AFT READING LIGHTS AND LEFT AISLE CENTER) REMAIN ON AS WELL AS THE EXTERIOR ENTRY LIGHT. ENTRY LIGH - [SDR DXTA2025091104899](https://openairdocs.org/sdr/DXTA2025091104899.md): Battery Pack · inoperative · Sep 9, 2025 · N317QS · Cessna 680SOV · Emergency Lighting > ON EMERGENECY LIGHTS TEST THE FOLLOWING LIGHTS ARE NOT ILLUMINATING: SEAT LIGHT OVER SEAT 8 RT SIDE WING INSPECTION LIGHT & RT FWD EMERGENCY LIGHT ABOVE WING ALL OF THE OTHER LIGHTS TEST PROPERLY DURING THE TEST & ALL OF THE LIGHTS WORK WHEN THE BATTERIES/APU - [SDR JGVR2025051504](https://openairdocs.org/sdr/JGVR2025051504.md): Hinge Bracket · corroded · May 15, 2025 · N317QS · Cessna 680SOV · Rudder Structure > UPPER RUDDER HINGE BRACKET, CORROSION, THAT REQUIRED THE REPLACEMENT OF THE UPPER RUDDER HINGE BRACKET PN: 6931050-64 - [SDR JGVR20250402005](https://openairdocs.org/sdr/JGVR20250402005.md): Skin · corroded · May 14, 2025 · N317QS · Cessna 680CE · Wing, Plate/Skin > REPAIRED CORRODED AREAS OF THE UPPER INBOARD WING SKINS LOCATED UNDER AND ADJACENT TO THE LH AND RH WING AFT DRAG ANGLES (WING-TO-FUSELAGE FAIRING STRUCTURE), BY R&R THE AFT DRAG ANGLES, BLENDING CORRODED AREAS, PERFORMING NDT AND REPORTING FOR REPAIR DISPOSIT - [SDR 2025F00106](https://openairdocs.org/sdr/2025F00106.md): Angle · corroded · Apr 29, 2025 · N317QS · Cessna 680A · Fuselage Miscellaneous Structure > RH MLG WHEEL WELL AFT SPAR LOWER CLIP INBD OF WS 37.00 IS HEAVILY CORRODED NEAR 2 HI-LOK'S. MECHANICALLY REMOVED CORROSION LOCATED IN RH MLG WHEEL WELL, AFT SPAR, LOWER CAP RWS 17 TO RWS 19 INBD OF WS 37.00 IAW C680 SRM 51-70-02. FOUND CORROSION BLENDS BEYOND - [SDR JGVR20250416003](https://openairdocs.org/sdr/JGVR20250416003.md): Support Beam · corroded · Apr 16, 2025 · N317QS · Cessna 680CE · Wing Main, Frame Structure > MECHANICALLY REMOVED AREA OF CORROSION ROUND CARRY THRU HYDRAULIC FITTING LOCATED IN RH MLG WHEEL WELL FORWARD END OF WS 37.00 BEAM SUPPORT ON INBOARD SIDE, PERFORMED NDT AND REPORTED FOR DISPOSITION. REPAIRED BY LEANING, TREATING, AND PRIMING BLENDED AREAS PE - [SDR JGVR20250416002](https://openairdocs.org/sdr/JGVR20250416002.md): Skin · corroded · Apr 16, 2025 · N317QS · Cessna 680CE · Fuselage Main, Plate/Skin > BLENDED 3 AREAS OF CORROSION ON THE LOWER FUSELAGE SKIN AROUND LH FWD FUSELAGE CHIN FAIRING, R&R LH FORWARD CHIN FAIRING FOR ACCESS, PERFORMED NDT AND REPORTED FOR DISPOSITION. REPAIRED BY INSTALLING ONE REPAIR DOUBLER AS REQUIRED AND CLEANING, TREATING AND PR - [SDR JGVR20250416001](https://openairdocs.org/sdr/JGVR20250416001.md): Structure · corroded · Apr 16, 2025 · N317QS · Cessna 680CE · Emergency Exits > MECHANICALLY REMOVED 11 AREAS OF CORROSION FROM E-EXIT DOOR STRUCTURE NEAR CONTOUR RING, PERFORMED NDT AND REPORTED FOR DISPOSITION. REPAIRED CORROSION BLENDS BY TREATING PRIMING AND PAINTING AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT. - [SDR DXTA2025021402364](https://openairdocs.org/sdr/DXTA2025021402364.md): Handle · lack of lube · Feb 13, 2025 · N317QS · Cessna 680SOV · Passenger/Crew Doors > MAIN DOOR LOCK: WHEN CLOSING THE MAIN CABIN DOOR THE PUSH BUTTON IN THE HANDLE WOULD NOT POP OUT WHEN THE HANDLE WAS IN THE CLOSED POSITION AND THE DOOR WOULD NOT LOCK. THE HANDLE MOVED FREELY FROM THE CLOSED TO OPEN POSITION AND THE CABIN DOOR OPEN CAUTION WO - [SDR DXTA2024122301614](https://openairdocs.org/sdr/DXTA2024122301614.md): Spring · damaged · Dec 19, 2024 · N317QS · Cessna 680SOV · Passenger/Crew Doors > MAIN DOOR: WHEN LOCKING PLANE UP FOR THE NIGHT WHEN WE LIFTED THE UNLOCK BAR TO CLOSE THE AIRSTAIRS WE HEARD A LOUD BANG AND THE DOOR WOULD NOT MOVE. WE REALIZED THE RIGHT CABLE IS JUST HANGING WITH NO TENSION. THE AIRSTAIR HAVE TO BE FORCED UP AND WILL JUST - [SDR JGVR20240306001](https://openairdocs.org/sdr/JGVR20240306001.md): Skin · corroded · Mar 6, 2024 · N317QS · Cessna 680CE · Trailing Edge Flaps > BLENDED CORRODED AREAS UNDER THE NUTPLATES COMMON TO THE LH & RH WING FLAP PANELS 523AB AND 623AB, PERFORMED NDT, AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS BY FABRICATING AND INSTALLING REPAIR DOUBLERS IN ACCORDANCE WITH NETJETS RFTS-110102. - [SDR DXTA2023120810283](https://openairdocs.org/sdr/DXTA2023120810283.md): Unknown · unknown · Dec 8, 2023 · N317QS · Cessna 680SOV · Emergency Lighting > EMERGENCY EXIT SIGN ON THE AFT RIGHT FACING UPPER DIVIDER MIRROR IS OUT. ALL EMERGENCY LIGHTS TESTED OKAY DURING PREFLIGHT INSPECTION AND FAILED IN FLIGHT. IAW 20-30-25 REV 1 AND MM 25-20-10 REV 20 CABIN DIVIDERS MAINT PRACTICES REMOVED LT LAV BULKHEAD AND - [SDR DXTA2023092095950](https://openairdocs.org/sdr/DXTA2023092095950.md): Unknown · unknown · Sep 19, 2023 · N317QS · Cessna 680CE · Passenger Compartment Equipment > SHADE IN THE EMERGENCY EXIT DOOR/HATCH IS FAILED IN THE CLOSED POSITION. REMOVED EMERGENCY DOOR AND GAINED ACCESS TO THE WINDOW SHADE. TROUBLESHOT THE WINDOW SHADE TO THE SHADE ASSY. POSITIONED SHADE IN THE FAILED UP POSITION. PLACED PARTS ON ORDER. DUE TO PA - [SDR 2023F00270](https://openairdocs.org/sdr/2023F00270.md): Spar · corroded · Sep 11, 2023 · N317QS · Cessna 680CE · Wing Structure > R/H MLG WHEEL WELL FUEL AND HYDRAULIC LINE THRU PLATE HAS SURFACE CORROSION. ACCOMPLISHED TEXTRON AVIATION ENGINEERING REPAIR S-680-ATA57/03RD REPAIR OF WING STRUCTURE CORROSION AT TITANIUM BULKHEAD FITTINGS DATED AUGUST 23, 2018 AND FAA FORM 8100-9 DATED 3/18 - [SDR DXTA2023080792420](https://openairdocs.org/sdr/DXTA2023080792420.md): Unknown · unknown · Aug 7, 2023 · N317QS · Cessna 680SOV · Emergency Lighting > UPON TESTING THE EMER LIGHTS ON POWER UP, THE MAIN EXIT LIGHT OVER THE MAIN CABIN DOOR DID NOT ILLUMINATE. VERIFIED DISCREPANCY, ATTEMPTED TO CHARGE #1 BATTERY PACK WITH NO SUCCESS. ACCESSED #1 BATTERY PACK, INSPECTED THE FUSE ON THE #1 BATTERY PACK AND FOUND - [SDR 2023FA0000120](https://openairdocs.org/sdr/2023FA0000120.md): Spar · corroded · Mar 9, 2023 · N317QS · Cessna 680CE · Wing Spar > FOUND DURING BASE CHECK RIGHT MAIN WHEEL WELL AFT SPAR HAS LEVEL 2 CORROSION IN 2 LOCATIONS WILL REQUIRE CLEAN AND BLEND - [SDR DXTA2022052562610](https://openairdocs.org/sdr/DXTA2022052562610.md): Spring · damaged · May 24, 2022 · N317QS · Cessna 680A · Passenger/Crew Doors > MAIN DOOR CABLE: UPON RAISING CABIN DOOR THE FORWARD CABLE RELEASED AND THE DOOR WENT DOWN HARD. CABLE IS STILL ATTACHED AT BOTH ENDS BUT LOOSE. THE REAR CABLE IS WORKING. DOOR WILL NOT CLOSE DROM INSIDE.//CORRECTIVE ACTION// R/R MAIN CABIN DOOR FWD COUNTER B - [SDR JGVR20200506001](https://openairdocs.org/sdr/JGVR20200506001.md): Spar Cap · corroded · May 6, 2020 · N317QS · Cessna 680CE · Wing Spar > REMOVED FOUR HI-LOK FASTENERS FOR ACCESS AND BLENDED CORRODED AREA ON THE UPPER SURFACE OF THE LOWER WING SPAR CAP LOCATED IN THE LEFT HAND MAIN LANDING GEAR WHEEL WELL AREA, PERFORMED NDT REPORTED FOR REPAIR DISPOSITION. PERFORMED BOLT HOLE NDT, POLISHED, CLE - [SDR JGVR20190522002](https://openairdocs.org/sdr/JGVR20190522002.md): Skin · corroded · May 22, 2019 · N317QS · Cessna 680CE · Fuselage Main, Plate/Skin > REPAIRED NUMEROUS AREAS ON LOWER FUSELAGE SKIN, DOUBLERS, AND STRINGERS OF THE DROP AISLE AREA BETWEEN FS 157 AND FS 426 BY BLENDING OUT CORROSION, PERFORMING NDT AND INSTALLING DOUBLERS AND FILLERS AS REQUIRED PER RESEARCH AND DEVELOPMENT MRO ENGINEERING REPA - [SDR JGVR20190522001](https://openairdocs.org/sdr/JGVR20190522001.md): Doubler · gouged · May 22, 2019 · N317QS · Cessna 680CE · Fuselage Miscellaneous Structure > REPAIRED TWO GOUGED AREAS OF THE INTERIOR FUSELAGE DOUBLER NEAR THE ESCAPE HATCH AT FS 399.75 AND FS 403 BY BLENDING/SMOOTHING THE GOUGED AREAS PERFORMING NDT, TREATING, AND PRIMING IN ACCORDANCE WITH FIELD REPAIR. - [SDR JGVR20181102002](https://openairdocs.org/sdr/JGVR20181102002.md): Skin · corroded · Nov 2, 2018 · N317QS · Cessna 680CE · Wing, Plate/Skin > THE LT WING SKIN WAS CORRODED. BLENDED CORRODED AREAS ON THE UPPER WING SKIN. - [SDR JGVR20181031001](https://openairdocs.org/sdr/JGVR20181031001.md): Skin · corroded · Oct 31, 2018 · N317QS · Cessna 680CE · Emergency Exits > FOUND EMERGENCY EXIT DOOR CORRODED AROUND THE CONTOUR RINGS AND DOOR SKIN. REPLACED THE CONTOUR RINGS WITH NEW PARTS AND REPAIRED THE DOOR SKIN BY BLENDING AND TREATING PER REPAIR. - [SDR 2018FA0000010](https://openairdocs.org/sdr/2018FA0000010.md): Spar · corroded · Jan 10, 2018 · N317QS · Cessna 680CE · Wing Spar > DURING GENERAL VISUAL INSPECTION OF THE LEFT MAIN WHEEL WELL INSPECTION, FOUND CORROSION ON THE AFT LOWER WING SPAR ASSEMBLY. - [SDR DXTA2014051305770](https://openairdocs.org/sdr/DXTA2014051305770.md): Switch · failed · May 12, 2014 · N317QS · Cessna 680CE · Landing Gear Position and Warning > AFTER TAKEOFF, GEAR WOULD NOT RETRACT. WOW MISCOMPARE CAS MESSAGE CAME ON FOR THE REST OF THE FLIGHT. FOUND NOSE GEAR WOW SWITCH LOOSE, ADJUSTED & TIGHTENED SWITCH. COMPLETED GEAR SWING, OPS CHECKED GOOD IAW AMM 32-60-00. - [SDR DXTA2014041105726](https://openairdocs.org/sdr/DXTA2014041105726.md): Valve · malfunctioned · Apr 10, 2014 · N317QS · Cessna 680CE · Landing Gear Retraction/Extension System > AFTER TAKEOFF, THE GEAR HANDLE WOULD NOT COME UP. THE PIN NEVER RELEASED & THE GEAR LIGHTS REMAINED GREEN. AMBER WOW INCOMPARABLE CAS MESSAGE CAME ON & REMAINED UNTIL LANDING, LANDING WAS NORMAL. POWERED ACFT & FOUND NO FAULTS ON EICAS. RANG OUT ALL SQUAT - [SDR DXTA2014040705719](https://openairdocs.org/sdr/DXTA2014040705719.md): Squat Switch · damaged · Apr 6, 2014 · N317QS · Cessna 680CE · Landing Gear Retraction/Extension System > AFTER TAKEOFF, THE GEAR HANDLE WOULD NOT MOVE TO THE RETRACT POSITION. ABOUT TWO MINUTES LATER, RECEIVED AN AMBER WOW INCOMPARABLE CAS MESSAGE. BEFORE LANDING THE CAS MESSAGE CLEARED. DID NOT TRY TO RETRACT GEAR AT THAT TIME. GEAR REMAINED DOWN WITH THREE - [SDR DXTA2011092604736](https://openairdocs.org/sdr/DXTA2011092604736.md): Display · malfunctioned · Sep 25, 2011 · N317QS · Cessna 680CE · Central Display > CO-PILOTS PFD WOULD NOT DISPLAY ANY FLIGHT INFORMATION. IT WOULD ONLY DISPLAY RED X. YOU COULD GET THE FLIGHT INFORMATION IF YOU REVERTED THE DISPLAY TO DU 3. CYCLED DU4 C/B DISPLAY NEVER RECOVERED STAYED BLANK REPLACED DU 4, LOADED OPS S/W IAW MM, 34-23-10. - [SDR DXTA2010110804297](https://openairdocs.org/sdr/DXTA2010110804297.md): Brake Assy · weak · Nov 5, 2010 · N317QS · Cessna 680CE · Landing Gear Brake System > LEFT OUTER WHEEL BRAKE INDICATOR AT LIMITS. LT BRAKE MUSHY. REMOVED NR 1 BRAKE ASSY, INSTALLED O/H BRAKE ASSY. BLED BRAKES. REINSTALLED WHEEL ASSY AND TORQUED. ALL WORK PERFORMED IAW MM 32-42-10, 32-41-20. SERVICED HYD RESERVOIR IAW MM 12-12-02. - [SDR DXTA2010072004164](https://openairdocs.org/sdr/DXTA2010072004164.md): Coffeemaker · odor · Jul 19, 2010 · N317QS · Cessna 680CE · Buffet/Galleys > 15 MIN INTO FLIGHT CREW NOTICED BURNING ODOR COMING FROM COFFEE & WATER POTS. TURNED POWER OFF TO POTS & ODOR CEASED. OPERATED BOTH TANKS FOR 30 MINUTES WITH NO ODOR NOTED. REMOVED REFRESHMENT CENTER PANELS & INSPECTED WIRING & CONNECTIONS BEHIND BAR, NO DEF - [SDR DXTA2010041204064](https://openairdocs.org/sdr/DXTA2010041204064.md): Coupling · unsecure · Apr 10, 2010 · N317QS · Cessna 680CE · Humidity Control System > ON CLIMBOUT, "CABIN ALT" LIGHT ILLUMINATED. ACFT WAS 25,000 FT.; PAX O2 MASKS WERE DEPLOYED. CABIN ALT MAINTAINED 9,500' UNTIL DESCENT BELOW 10K'. DURING THE INSP OF THE PRESSURIZATION SYS DUCTING WE FOUND THE EXIT COUPLING ON THE COALESER SOCK CAN HAD BECOME ## 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 = 'N317QS' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N317QS/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.