# N311QS: 2008 Cessna 680, registration cancelled 2024-12-03 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 3, 2024 - Status when cancelled: Valid registration - Airframe: [Cessna 680](https://openairdocs.org/model/cessna-680) (registry code 2076811) - Engine: [Pratt & Whitney Canada PW306C](https://openairdocs.org/engine/pratt-whitney-canada-pw306c) (registry code 52169) - Data sheets: [TCDS T00012WI](https://openairdocs.org/tcds/T00012WI), [TCDS E35NE](https://openairdocs.org/tcds/E35NE) (OpenAirDocs) - Serial number: 680-0196 - Year built: 2008 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: May 1, 2008 - Certificate issued: August 18, 2020 - Last registry action: March 10, 2023 - Mode S code: A34BF7 - Owner when cancelled: [Netjets Sales Inc](https://openairdocs.org/faa-owner/NETJETS%20SALES%20INC) - Location: [Oklahoma City, OK](https://openairdocs.org/faa-place/OK/Oklahoma%20City) - Owner type: Corporation - Owner's area on the map: 35.5467° N, 97.5646° W: Placed by OpenAirDocs at the center of ZIP code 73116, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N311QS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=311QS - Page: https://openairdocs.org/deregistered/N311QS-2024-12-03 From the FAA registry file of November 7, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Cessna 680: https://openairdocs.org/model/cessna-680.md ## Service difficulty reports (37) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR JGVR20240626003](https://openairdocs.org/sdr/JGVR20240626003), Jun 26, 2024: SPAR CAP. CORRODED. REPAIRED SEVERAL CORRODED AREAS ON THE VERTICAL STABILIZER AFT SPAR RH CAP BY BLENDING, PERFORMING NDT, REPORTING FOR REPAIR DISPOSITION, FABRICATING AND INSTAL - [SDR JGVR20240626002](https://openairdocs.org/sdr/JGVR20240626002), Jun 26, 2024: SPAR CAP. CORRODED. REPAIRED CORRODED AREAS OF THE LOWER FORWARD SPAR CAPS OF THE LH & RH WINGS, LOCATED IN THE MAIN LANDING GEAR WHEEL WELLS, BY REMOVING FASTENERS AS REQUIRED, BL - [SDR JGVR202406264001](https://openairdocs.org/sdr/JGVR202406264001), Jun 26, 2024: SKIN. CORRODED. REPAIRED CORRODED AREAS OF THE LOWER AFT FUSELAGE TAILCONE SKINS LOCATED UNDER AND ADJACENT TO THE AFT CHIN FAIRING AREAS BY BLENDING CORRODED AREAS, PERFORMING - [SDR JGVR20230711001](https://openairdocs.org/sdr/JGVR20230711001), Jul 11, 2023: UNKNOWN. UNKNOWN. BLENDED CORROSION ON THE UPPER SURFACE OF THE UPPER WING SKIN OF THE RH WING, LOCATED ADJACENT TO AND UNDERNEATH THE AFT DRAG ANGLE (WING-TO-FUSELAGE FAIRING AR - [SDR DXTA2022120175180](https://openairdocs.org/sdr/DXTA2022120175180), Nov 30, 2022: SPRING. DEFECTIVE. MAIN DOOR PRECATCH LEVER: LEVER EXTENDED AND WILL NOT RETRACT. VISUALLY VERIFIED PRECATCH SYSTEM IS NOT WORKING PROPERLY. GAINED INTERNAL ACCESS TO PRECATCH SYS - [SDR DXTA2022032859060](https://openairdocs.org/sdr/DXTA2022032859060), Mar 28, 2022: PUMP. DEFECTIVE. FUEL PRESSURE INDICATION: WHILE CROSSFEEDING FROM L TANK, FUEL PRESS LOW L. CASS MESSAGE CAME ON MOMENTAIRLY FOLLOWED BY FUEL BOOST PUMP ON L CASS MESSAGE. FUEL - [SDR DXTA2022031758610](https://openairdocs.org/sdr/DXTA2022031758610), Mar 17, 2022: NONE. NONE. LEFT EMERGENCY LIGHT AFT OF MCD: MULTIPLE EMERGENCY LIGHTS INOP. LEFT EXTERIOR FUSELAGE AFT OF MAIN CABIN DOOR. INTERIOR CEILING LIGHT OVER SEAT 3 AND 5. INTERI - [SDR JGVR20210507002](https://openairdocs.org/sdr/JGVR20210507002), May 7, 2021: RIB. CORRODED. REMOVED RH EMERGENCY BRAKE BULKHEAD FITTING FROM RH WING, RIB AT RWS 37. BLENDED CORROSION FROM FWD INBOARD WEB ON RIB AT RWS 37. EVALUATED REMAINING THICKNESS - [SDR JGVR20210507001](https://openairdocs.org/sdr/JGVR20210507001), May 7, 2021: SPAR. CORRODED. REMOVED LH UPPER AND LOWER BRAKE LINES AND BULKHEAD FITTINGS FROM LH WING, MIDDLE SPAR, AFT SIDE. BLENDED CORROSION FROM LH WING, MIDDLE SPAR, AFT SIDE. EVALUAT - [SDR JGVR20210427001](https://openairdocs.org/sdr/JGVR20210427001), Apr 27, 2021: SPAR CAP. CORRODED. BLENDED CORRODED AREAS ON THE LEFT AND RIGHT HAND WINGS AFT SPARS LOWER SPAR CAPS, LOCATED IN THE MAIN LANDING GEAR WHEEL WELL AREAS, PERFORMED ULTRASONIC AND E - [SDR JGVR20201123002](https://openairdocs.org/sdr/JGVR20201123002), Nov 23, 2020: SKIN. CORRODED. SPOT OF CORROSION ON LT WING INBOARD FWD, JUST BEHIND LEADING EDGE. NOTED DURING 57-00-00-2101-LT FOUND 48 ADDITIONAL CORROSION AREAS AFTER FWD DRAG ANGLE REMOV - [SDR JGVR20201123001](https://openairdocs.org/sdr/JGVR20201123001), Nov 23, 2020: SPAR. CORRODED. CORROSION FOUND ON VERTICAL STAB AFT SPAR. FOUND DURING 1 ADDITIONAL AREA OF CORROSION FOUND ON RT SIDE OF VERTICAL STAB SPAR CLIP JUST BELOW RUDDER MIDDLE HING - [SDR JGVR20201120006](https://openairdocs.org/sdr/JGVR20201120006), Nov 20, 2020: STRUCTURE. CORRODED. FOUND SEVERAL AREAS OF CONFIRMED CORROSION UNDER SEVERAL NUTPLATES ON THE V-STAB AT THE FOLLOWING LOCATIONS: 341DL 7 NUTPLATES, 341CL 5 NUTPLATES,341BL 5 NUTPLA - [SDR JGVR202011110202](https://openairdocs.org/sdr/JGVR202011110202), Nov 11, 2020: SPAR. CORRODED. SPOT OF VERIFIED CORROSION IN LT WHEEL WELL ON AFT SPAR, LOWER SPAR CLIP. MECHANICALLY REMOVED 1 SPOT OF VERIFIED CORROSION IN LT WHEEL WELL ON AFT SPAR LOWER S - [SDR JGVR20201111001](https://openairdocs.org/sdr/JGVR20201111001), Nov 11, 2020: SPAR. CORRODED. SPOTS OF VERIFIED CORROSION IN RT WHEEL WELL ON AFT SPAR, LOWER SPAR CLIP. MECHANICALLY REMOVED 1 SPOT OF VERIFIED CORROSION IN RT WHEEL WELL ON AFT SPAR LOWER - [SDR JGVR20191023001](https://openairdocs.org/sdr/JGVR20191023001), Oct 23, 2019: DOOR FRAME. CHAFED. REPAIRED FIVE CHAFFED AREAS AROUND E-EXIT WEB AND FRAME IN STRINGER 3 SURROUNDING AREAS OF THE INTERIOR FUSELAGE AT FS 409.26 AND FS 426.26 BY INSTALLING REPAIR - [SDR EBVR20190514001](https://openairdocs.org/sdr/EBVR20190514001), May 14, 2019: CHANNEL. CRACKED. FOUND DURING PRELIMINARY INSPECTION. LT PYLON AFT CHANNEL ASSEMBLY IS CRACKED. FABRICATED AND INSTALLED REPAIR DOUBLER. ATTACHED TO MODIFIED EXISTING CHANNEL AS - [SDR 2017F00169](https://openairdocs.org/sdr/2017F00169), Oct 4, 2017: TRUNNION. WORN. REPAIR OF OVERSIZED DOOR ROD PIN HOLE IN LEFT AND RIGHT MLG TRUNNIONS. REPORT NR S-680-0196/06RD DATED SEPTEMBER 29, 2017 WITH FORM FAA 8100-9. - [SDR 2017F00170](https://openairdocs.org/sdr/2017F00170), Oct 4, 2017: DOOR. CORRODED. LEFT AND RIGHT MLG DOOR CORROSION. MEMO DQ9710M1 DATED: OCTOBER 3, 2017. - [SDR 2018F00007](https://openairdocs.org/sdr/2018F00007), Oct 3, 2017: SPAR. CORRODED. LEFT AND RIGHT AFT WING SPAR WEB BULKHEAD FITTING CORRODED. - [SDR 2017FA0000508](https://openairdocs.org/sdr/2017FA0000508), Oct 3, 2017: FLAP. CORRODED. LEFT INBOARD FLAP CORRODED. - [SDR DXTA2017041206393](https://openairdocs.org/sdr/DXTA2017041206393), Apr 12, 2017: CONTROL HANDLE. MALFUNCTIONED. LANDING GEAR WOULD NOT RETRACT, GEAR HANDLE STUCK IN UP POSITION. REMOVED FAILED GEAR HANDLE AND INSTALLED NEW. C/W GEAR SWING. OPERATIONAL CHECK GOOD. WORK COM - [SDR DXTA2016122906349](https://openairdocs.org/sdr/DXTA2016122906349), Dec 29, 2016: UPLOCK SWITCH. OUT OF ADJUST. ABRUPT THUMP FOLLOWED BY RED GEAR UNLOCK LIGHT OCCURRED AT CRUISE AT FL410. TROUBLESHOT TO NOSE LANDING GEAR UPLOCK SWITCH BARLY CONTACTING UPLOCK ROLLER. ADJUS - [SDR DXTA2015100606101](https://openairdocs.org/sdr/DXTA2015100606101), Oct 6, 2015: UNKNOWN. ODOR. WHEN SELECTING AVIONICS ON, WE HEARD A NOISE LIKE A FAN BLADES HITTING SOMETHING, THEN WE SMELLED THE ODOR OF SOMETHING BURNING. TURNED AVIONICS BACK OFF AND WH - [SDR DXTA2015082806069](https://openairdocs.org/sdr/DXTA2015082806069), Aug 27, 2015: PRESSURE SWITCH. MALFUNCTIONED. AT 200 FT AGL THE FUEL BOOST PUMP RT CAS MESSAGE CAME ON. CREW SELECTED RT BOOST PUMP ON. AT 100 FT AGL FUEL PRESS LOW RT CAS MESSAGE CAME ON. ON LANDING ROLL O - [SDR DXTA2015061506029](https://openairdocs.org/sdr/DXTA2015061506029), Jun 12, 2015: BATTERY. FAILED. RED CAS MESSAGE BATTERY O TEMP LIGHT ILLUMINATED ON TAKEOFF ROLL. TEMP, BATTERY, WENT UP TO +71 C. COMPLIED WITH APPROPRIATE EMERGENCY CHECKLIST. THE CYAN BATTE - [SDR DXTA2014010605615](https://openairdocs.org/sdr/DXTA2014010605615), Jan 3, 2014: WARNING MESSAGE. FALSE ACTIVATION. AFTER TAKEOFF, CLIMBING THROUGH 2000 MSL, AMBER ANTI-SKID FAIL CAS ILLUMINATED. COMPLETED ABNORMAL CHECKLIST, CAS DID NOT CLEAR. POWERED ACFT & PERFORMED OPERAT - [SDR DXTA2011012404429](https://openairdocs.org/sdr/DXTA2011012404429), Jan 22, 2011: STRUT. CHAFED. GEAR WOULD NOT RETRACT ON CLIMB-OUT AND THE GEAR HANDLE WOULD NOT MOVE. WHILE CONFIGURING FOR LANDING THE "WOW MISCOMPARE" CAS MESSAGE ILLUMINATED. R & R NLG UP - [SDR DXTA2010121104359](https://openairdocs.org/sdr/DXTA2010121104359), Dec 9, 2010: PRESSURE SWITCH. MALFUNCTIONED. FUEL FILTER BYPASS L CAS ILLUMINATED IN FLIGHT, EMERGENCY DECLARED. REMOVED & INSPECTED LT FUEL FILTER ELEMENT. NO DEBRIS OR FOREIGN MATERIAL FOUND IN ELEMENT O - [SDR DXTA2009082103764](https://openairdocs.org/sdr/DXTA2009082103764), Aug 20, 2009: MODULE. FAILED. THE ENG CONTROL FAULT R FAILED AT FL430. DID NOT FLY THROUGH ANY WEATHER. DASHES ON EVERYTHING RT SIDE. ON POWERING DOWN THE AMBER MAU 2 FAIL CAME ON. REMOVED A - [SDR DXTA2009030903538](https://openairdocs.org/sdr/DXTA2009030903538), Mar 6, 2009: LATCH. UNSECURE. UPPER FWD LATCH OF REAR BAGGAGE DOOR POPPED OPEN IN FLIGHT. INSPECTED DOOR LATCH, PINS, AND LOCKS. FOUND DOOR TO OPERATE AS REQUIRED WITH NO DEFECTS NOTED. - [SDR DXTA2009010303463](https://openairdocs.org/sdr/DXTA2009010303463), Jan 3, 2009: CONTROL UNIT. INOPERATIVE. DURING CRUISE AP A FAIL CAS MESSAGE POSTED FOLLOWED 30 SECONDS LATER BY AP B FAIL CAS MESSAGE. BOTH MESSAGE REMAINED ON THE RESET OF THE FLIGHT REVIEWED CDMS FA - [SDR DXTA200901033462](https://openairdocs.org/sdr/DXTA200901033462), Jan 3, 2009: CONTROL UNIT. INOPERATIVE. DURING CRUISE, AP A FAIL CAS MESSAGE POSTED FOLLOWED 30 SECONDS LATER BY AP B FAIL CAS MESSAGE. BOTH MESSAGES REMAINED ON THE RESET OF THE FLIGHT REPEAT WRITE-U - [SDR DXTA2009010503462](https://openairdocs.org/sdr/DXTA2009010503462), Jan 3, 2009: AUTOPILOT SYS. MALFUNCTIONED. DURING CRUISE AP A FAIL CAS MSG POSTED FOLLOWED 30 SECONDS LATER BY AP B FAIL CAS MSG. - [SDR DXTA200808083220](https://openairdocs.org/sdr/DXTA200808083220), Aug 8, 2008: STEERING SYS. OUT OF LIMITS. AFTER TAKEOFF, POSITIONED GEAR HANDLE UP. MAIN CAME UP BUT NOSE DID NOT RETRACT AND THE RED UNLOCK LIGHT STAYED ILLUMINATED. RECYCLED GEAR AND SAME THING HAPPEN - [SDR DXTA200803220](https://openairdocs.org/sdr/DXTA200803220), Aug 8, 2008: INDICATION SYS. MALFUNCTIONED. AFTER TAKEOFF, POSITIONED GEAR HANDLE UP. THE MAINS CAME UP BUT THE NOSE DID NOT RETRACT AND THE RED UNLOCK LIGHT STAYED ILLUMINATED. (S) - [SDR DXTA200803158](https://openairdocs.org/sdr/DXTA200803158), Jul 2, 2008: STRUT. LOW. GEAR WILL NOT RETRACT AFTER TAKEOFF. "WOW MISCOMPARE" AMBER MESSAGE IN FLIGHT INTERMITTENTLY. WENT OUT BEFORE LANDING. ONLY ON FOR ABOUT 15 SECONDS. NOSE STRUT ## Other aircraft with N311QS - [Registered now](https://openairdocs.org/aircraft/N311QS): Embraer Executive EMB-505, S/N 50500982 --- 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.