# N364QS: 2006 Cessna 680, registration cancelled 2023-11-07

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: November 7, 2023
- Status when cancelled: Valid registration
- Airframe: [Cessna 680](https://openairdocs.org/model/cessna-680) (registry code 2076811)
- Engine: [Pratt & Whitney PW300 series](https://openairdocs.org/engine/pratt-whitney-pw300-series) (registry code 52128)
- Data sheets: [TCDS T00012WI](https://openairdocs.org/tcds/T00012WI) (OpenAirDocs)
- Serial number: 680-0062
- Year built: 2006
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: January 23, 2006
- Certificate issued: October 19, 2021
- Last registry action: June 16, 2023
- Mode S code: A41C97
- 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/N364QS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=364QS
- Page: https://openairdocs.org/deregistered/N364QS-2023-11-07

From the FAA registry file of November 5, 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 (50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR DXTA2023062689480](https://openairdocs.org/sdr/DXTA2023062689480), Jun 26, 2023: UNKNOWN. UNKNOWN. AT FL410, FLAPS FAIL AMBER CAS. FLAP INDICATOR AMBER. WENT TO 7 AMBER IND & BACK TO 0 W/O BEING TOUCHED. DIVERTED & AT 14,000' RAN FAIL QRC. NO RESET. RAN QRC 1
- [SDR DXTA2023061588770](https://openairdocs.org/sdr/DXTA2023061588770), Jun 15, 2023: UNKNOWN. UNKNOWN. MAIN DOOR PRECATCH: PRECATCH HANDLE MISSING//CORRECTIVE ACTION//INSTALLED MAIN DOOR PRECATCH HANDLE ( CANNIBALIZE FROM N308QS SN: 680-0116 FOR CONTINUE SERVICE 
- [SDR DXTA2022090970010](https://openairdocs.org/sdr/DXTA2022090970010), Sep 8, 2022: BATTERY PACK. DEFECTIVE. EMERGENCY LIGHTING: REPEAT WRITE UP. WITH THE EMERGENCY LIGHTS SWITCH IN THE OFF POSITION AND BOTH AIRCRAFT BATTERY SWITCHES OFF, THE FOLLOWIMG EMER LIGHTS ARE 
- [SDR DXTA2022090769890](https://openairdocs.org/sdr/DXTA2022090769890), Sep 7, 2022: NONE. NONE. MAIN DOOR HANDLE: THE THUMB PUSH BUTTON THAT RELEASES THE MAIN CABIN DOOR (WHITE LETTERING ON RED BACKGROUND) IS INTERMITTENT AND OCCASIONALLY REQUIRES GIGGLING
- [SDR DXTA2022090669660](https://openairdocs.org/sdr/DXTA2022090669660), Sep 5, 2022: NONE. NONE. EMERGENCY LIGHTING: WITH THE EMERGENCY LIGHTS SWITCH IN THE OFF POSITION AND BOTH AIRCRAFT BATTERIE SWITCHES IN THE OFF POSITION, THE FOLLOWING EMERGENCY LIGHTS
- [SDR DXTA2022080167120](https://openairdocs.org/sdr/DXTA2022080167120), Jul 31, 2022: SWITCH. OUT OF ADJUST. CABIN EMERG LIGHT: AFT EMERGENCY SIGN, LAV EMERGENCY SIGN AND LIGHT AND RIGHT WING AFT EMER LIGHT ILUMINATED WITH ALL POWER OFF AND UNABLE TO TURN THEM OFF WITH
- [SDR DXTA2022070565160](https://openairdocs.org/sdr/DXTA2022070565160), Jul 2, 2022: POWER SUPPLY. INOPERATIVE. EMERGENCY LIGHTING: RIGHT WING AFT EMERGENCY LIGHT, LAV EMER LIGHT, LAV EXIT SIGN, AND REAR EXIT SIGN ON MIRROR DIVIDER ALL REMAIN ON WITH ALL EMER LIGHT SWITCH
- [SDR DXTA2022051361670](https://openairdocs.org/sdr/DXTA2022051361670), May 12, 2022: SQUAT SWITCH. OUT OF ADJUST. WOW MISCOMPARE AMBER CAS: ON DEPARTING TEB GEAR HANDLE WOULD NOT RETRACT, AMBER CAS WOW MISCOMPARE ILLUMINATED. RAN CHECKLIST. DIVERTED TO NEWARK FOR 10,000 FT 
- [SDR DXTA2021102250730](https://openairdocs.org/sdr/DXTA2021102250730), Oct 22, 2021: COALESCER BAG. DIRTY. COCKPIT ODOR: AT THE END OF RIGHT ENGINE START SEQUENCE, STRONG ODOR FILLED THE COCKPIT AREA. THE ODOR WAS MUCH STRONGER THAN THE OCCASIONAL/TYPICAL AFTER START
- [SDR DXTA2021031939720](https://openairdocs.org/sdr/DXTA2021031939720), Mar 18, 2021: HANDLE. OUT OF ADJUST. MAIN DOOR HANDLE: MAIN CABIN DOOR HANDLE (OUTSIDE) FAILS TO GO FLUSH WHEN CLOSED FROM THE INSIDE. CLOSES FLUSH WHEN CLOSED FROM THE OUTSIDE.///SIGN-OFF///ADJUST
- [SDR JGVR20210122001](https://openairdocs.org/sdr/JGVR20210122001), Jan 22, 2021: SPAR CAP. CORRODED. BLENDED CORRODED AREA OF THE AFT LOWER SPAR CAP INBOARD OF WS 37 LOCATED IN THE RT MAIN LANDING GEAR WHEEL WELL, PERFORMED NDT, AND REPORTED FOR REPAIR DISPOSIT
- [SDR JGVR20190814005](https://openairdocs.org/sdr/JGVR20190814005), Aug 14, 2019: SKIN. CORRODED. L/H WING UPPER SKIN SECTION P/N 6922680-27 REPLACED (ABOVE L/H MLG) DUE TO CORROSION
- [SDR JGVR20190814004](https://openairdocs.org/sdr/JGVR20190814004), Aug 14, 2019: DRAG ANGLE. CORRODED. RIGHT WING UPPER DRAG ANGLES HAS CORROSION ALONG SEAMS APX TOTAL LENGTH OF 28 INCHES ALONG DRAG ANGLE OUTBD SEAMS ON WS 37.00.
- [SDR JGVR20190814003](https://openairdocs.org/sdr/JGVR20190814003), Aug 14, 2019: SKIN. CORRODED. LH & RH WING UPPER SKIN UPPER DRAG ANGLES HAVE CORROSION ALONG SEAMS AT WS 37.00 TOTAL LENGTH OF 53 INCHES ALONG DRAG ANGLE OUTBD SEAMS. FOUND WHILE PERFORMING 
- [SDR JGVR20190814002](https://openairdocs.org/sdr/JGVR20190814002), Aug 14, 2019: SKIN. CORRODED. CORROSION ON LH AND RH OVERWING FUEL ADAPTER LANDS ON WING SKIN. THIS WAS FOUND DURING OVERWING FUEL CAP AND ADAPTER REPLACEMENT.
- [SDR JGVR20190814001](https://openairdocs.org/sdr/JGVR20190814001), Aug 14, 2019: DOOR. CORRODED. EMERGENCY EXIT HAS LEVEL 1 CORROSION FOUND ON THE OUTER SKIN AND UNDERNEATH CONTOUR RINGS.
- [SDR DXTA2019F00014](https://openairdocs.org/sdr/DXTA2019F00014), Feb 20, 2019: FAIRING. DAMAGED. FASTENER PULLED THROUGH WING CUFF FAIRING 6922590-1. ACCOMPLISHED ENGINEERING MINOR REPAIR DQ18493 DATED FEB. 17, 2019.
- [SDR DXTA2019F00015](https://openairdocs.org/sdr/DXTA2019F00015), Feb 20, 2019: PANEL. DAMAGED. FASTENER PULLED THROUGH WING LENS PANEL 6922530-46. ACCOMPLISHED ENGINEERING MINOR REPAIR DQ18494 DATED FEB. 17, 2019.
- [SDR DXTA2019FA0000044](https://openairdocs.org/sdr/DXTA2019FA0000044), Feb 20, 2019: PANEL. DAMAGED. FASTENER PULLED THROUGH WING LENS PANEL 6922530-46. ACCOMPLISHED ENGINEERING MINOR REPAIR DQ18494 DATED FEB 17, 2019.
- [SDR DXTA2018031400709](https://openairdocs.org/sdr/DXTA2018031400709), Mar 13, 2018: ENGINE. ODOR. COCKPIT HAD AN ODOR OF OIL, VERY STRONG IN THE COCKPIT FROM TAKE-OFF THRU CLIMB OUT. IT SUBSIDED AT ALTITUDE BUT STRENGTHEN AGAIN DURING APPROACH. REMOVED AND R
- [SDR DXTA2018030800690](https://openairdocs.org/sdr/DXTA2018030800690), Mar 5, 2018: UNKNOWN. ODOR. COCKPIT ODOR AFTER TAKEOFF, STRONG ODOR AT HIGH POWER SETTING, RIGHT OIL TEMP 20 DEGREES HIGHER THAN LEFT ENGINE. AFTER LEVEL OFF SMELL WENT AWAY AND RIGHT OIL 
- [SDR DXTA201802220621](https://openairdocs.org/sdr/DXTA201802220621), Feb 22, 2018: ACM. ODOR. OIL ODOR IN THE COCKPIT, DURING CLIMB THRU 18,000 FT, A STRONG EXHAUST, OIL ODOR FILLED THE AIRPLANE. THE ODOR LASTED A FEW MINUTES AND CAME AND WENT THRU DURAT
- [SDR EBVR2018010900001](https://openairdocs.org/sdr/EBVR2018010900001), Jan 9, 2018: SKIN. CORRODED. DURING SCHEDULED MAINTENANCE, SEVERE CORROSION WAS FOUND BELOW DROP AISLE FLOOR RESULTING IN 2 AREAS THAT PENETRATED 100% OF SKIN THICKNESS. AREA WAS LOCATED JU
- [SDR EBVR20171222001](https://openairdocs.org/sdr/EBVR20171222001), Dec 22, 2017: STRUCTURE. CHAFED. CHAFES AT BS 426. REPAIRED IAW ERO-912745-001
- [SDR EBVR20171219001](https://openairdocs.org/sdr/EBVR20171219001), Dec 19, 2017: STRUCTURE. CHAFED. CHAFE AT BS 496. FABRICATED A DOUBLER AND INSTALLED IAW ERO-912745 REVISION IR.
- [SDR DXTA2013121205594](https://openairdocs.org/sdr/DXTA2013121205594), Dec 11, 2013: TRIM SWITCH. FAILED. PRIMARY TRIM FAILED. ON LT SIDE CONTROL CANNOT TRIM NOSE DOWN, WORKS NOSE UP. RT SIDE TRIM WORKS NORMAL. REMOVED PILOT'S PRIMARY TRIM SWITCH, PN S3860 1, SN 050
- [SDR CWQD20130703002](https://openairdocs.org/sdr/CWQD20130703002), Jul 3, 2013: SQUIB. MISINSTALLED. THE CONNECTORS FOR THE FIRE BOTTLE IN THE RT FWD BAGGAGE COMPARTMENT ARE EXTREMETLY DIFFICULT TO CONNECT- UPON FURTHER INVESTIGATION IT WAS DETERMINED THAT THE 
- [SDR CWQD20130703001](https://openairdocs.org/sdr/CWQD20130703001), Jul 3, 2013: STRUCTURE. DAMAGED. SQUIB ON SHARED FIRE BOTTLE IN RT NOSE COMPARTMENT HITTING AIRFRAME. DUE TO THE LIMITED SPACE ALLOWED IN RT NOSE COMPARTMENT AS COMPARED TO THE SIZE AND WEIGHT 
- [SDR CWQR20120318024](https://openairdocs.org/sdr/CWQR20120318024), Mar 18, 2013: HEAT EXCHANGER. CRACKED. DURING A SCHEDULED INSPECTION, PREFORMED A PRODUCT IMPROVEMENT, REPLACEMENT OF DUCT ASSY 6914070-67. NOTICED THAT THE HEAT EXCHANGER SIDE PLATE HAD TWO CRACKS A
- [SDR CWQR20120318023](https://openairdocs.org/sdr/CWQR20120318023), Mar 18, 2013: HEAT EXCHANGER. CRACKED. DURING A SCHEDULED INSPECTION, NOTICED HEAT EXCHANGER SIDE PLATE HAD FOUR CRACKS ABOUT .30 INCH LONG. A NEW HEAT EXCHANGER WAS INSTALLED. LEAK CHECK OF DEFECTIV
- [SDR DXTR20121214001](https://openairdocs.org/sdr/DXTR20121214001), Dec 7, 2012: DUCT. DELAMINATED. UNABLE TO CONTROL CABIN TEMP IN AUTOMODE. TROUBLESHOT AND FOUND DEBRIS IN CABIN CONDITIONED AIR DUCT CHECK VALVE. REMOVED CHECK VALVE TO REMOVED DEBRIS. FOUND C
- [SDR DXTA2012110505167](https://openairdocs.org/sdr/DXTA2012110505167), Nov 2, 2012: ACTUATOR. MALFUNCTIONED. DURING GEAR EXTENSION THE NOSE GEAR AND LEFT MAIN EXTENDED NORMALLY. THE RT MAIN TOOK BETWEEN 10-12 SECONDS TO EXTEND. NORMAL EXTENSION IS 5-6 SECONDS. ALSO REC
- [SDR DXTA2012062505015](https://openairdocs.org/sdr/DXTA2012062505015), Jun 24, 2012: SQUAT SWITCH. OUT OF ADJUST. AFTER TAKEOFF NOSE GEAR WOULD NOT RETRACT. UNLOCK LIGHT REMAINED ILLUMINATED AND NOSE GEAR CONTINUE TO CYCLE IN THE WELL. WOULD NOT LOCK. CYCLING PRODUCED LOUD 
- [SDR DXTA2011102704767](https://openairdocs.org/sdr/DXTA2011102704767), Oct 26, 2011: ACTUATOR. FAILED. DURING GEAR EXTENSION, RT MLG DID NOT SHOW ANY GREEN INDICATION AND THE RED UNLOCK LIGHT WAS ILLUMINATED. DISCONTINUED APPROACH AND WENT THROUGH THE CHECKLIST. 
- [SDR DXTA2011102004757](https://openairdocs.org/sdr/DXTA2011102004757), Sep 28, 2011: ENGINE. FLAMED OUT. AS THROTTLES ADVANCED, RECEIVED A RED "RIGHT ENGINE FAIL" CAS MESSAGE. THE ENGINE FAILED (SHUTDOWN) AND A FEW SECONDS LATER RE-LIT. PERFORMED TROUBLESHOOTING PR
- [SDR DXTA2011041404547](https://openairdocs.org/sdr/DXTA2011041404547), Apr 14, 2011: DISPLAY. INOPERATIVE. APPROACHING DESTINATION, SHOWED RED X'S ON AIRSPEED, ALTITUDE, AND VSI. ALSO RED ATT FAIL AND RED HEADING FAIL. AFTER ARRIVAL, FOUND DISPLAY UNIT 4 BLANK. ACCES
- [SDR DXTA2011031004501](https://openairdocs.org/sdr/DXTA2011031004501), Mar 10, 2011: SQUAT SWITCH. INOPERATIVE. AFTER GEAR RETRACTION, RECEIVED A GEAR UNLOCK LIGHT, NOSE GEAR UP, RIGHT MAIN UP LEFT MAIN DOWN INDICATION, WOW MISCOMPARE MESSAGE, THE RIGHT MAIN GEAR CAME DOW
- [SDR DXTA2010121104361](https://openairdocs.org/sdr/DXTA2010121104361), Dec 9, 2010: LANDING GEAR. MALFUNCTIONED. LT MLG HAD UNSAFE GEAR INDICATIONS. ON FINAL AND LANDING GEAR HANDLE ACTUATED TO GEAR DOWN POSITION THE LT MLG DOWN AND LOCKED INDICATOR DID NOT ILLUMINATE. EME
- [SDR DXTA2010022604005](https://openairdocs.org/sdr/DXTA2010022604005), Feb 25, 2010: UPLOCK SWITCH. FAILED. AFTER TAKEOFF, LT MAIN DID NOT RETRACT. UNLOCK LIGHT ON. R & R LT UPLOCK SWITCH IAW MM 32-60-00, OPS CHECK GOOD. NO DISC NOTED. ALSO FOUND NOSE STRUT NEEDED TO 
- [SDR DXTA2010012503953](https://openairdocs.org/sdr/DXTA2010012503953), Jan 24, 2010: PACKING. FAILED. "UNLOCK" INDICATION DURING GEAR RETRACT ACCOMPANIED BY LOUD GRINDING SOUND. ICAS REPORTED "WOW MISCOMPARE". REPACKED NLG STRUT IAW MM 32-20-01. SERVICED NLG STR
- [SDR DXTA2010012503952](https://openairdocs.org/sdr/DXTA2010012503952), Jan 24, 2010: LANDING GEAR. MALFUNCTIONED. "UNLOCK" INDICATION DURING GEAR RETRACT ACCOMPANIED BY LOUD GRINDING SOUND. ICAS REPORTED "WOW MISCOMPARE".
- [SDR DXTA2009110303842](https://openairdocs.org/sdr/DXTA2009110303842), Nov 2, 2009: FILTER. CONTAMINATED. AMBER "ENGINE CHIP DETECTOR R" CAS MESSAGE CAME ON IN FLIGHT - FL290 ABOUT 10 MINUTES AFTER TAKEOFF. MESSAGE REMAINED ON FOR ABOUT FIVE MINUTES THEN CAME ON AND
- [SDR DXTA2009101903814](https://openairdocs.org/sdr/DXTA2009101903814), Oct 16, 2009: ACTUATOR. MALFUNCTIONED. AFTER MOVING GEAR HANDLE TO RETRACT POSITION, 3 GREEN LIGHTS WENT OUT BUT RED UNLOCK LIGHT REMAINED ILLUMINATED. TROUBLESHOT NLG SYSTEM AND FOUND ACTUATOR NOT F
- [SDR DXTA2009042003608](https://openairdocs.org/sdr/DXTA2009042003608), Apr 18, 2009: STRUT. LOW. LANDING GEAR HANDLE WOULD NOT RAISE AFTER T/O. ALL GEAR REMAINED DOWN AND LOCKED, (3 GREEN, NO RED). WOW MISCOMPARE AMBER CAS MGS POSTED, THEN EXTINGUISHED PRIO
- [SDR DXTA2009031903556](https://openairdocs.org/sdr/DXTA2009031903556), Mar 18, 2009: ACTUATOR. INOPERATIVE. PRIMARY STAB TRIM INOP ON CLIMBOUT. BECAME INTERMITTENT AS AIRSPEED WAS DECREASED. REMOVED AND REPLACED PRIMARY STABILIZER TRIM ACTUATOR WITH OVERHAULED UNIT, A
- [SDR DXTA200803030](https://openairdocs.org/sdr/DXTA200803030), Apr 28, 2008: PUMP. MALFUNCTIONED. GEAR WOULD NOT EXTEND NORMALLY.TROUBLESHOT SYSTEM. SYSTEM OPS CHECK GOOD. SUSPECT LT HYDRAULIC PUMP WAS CAUSE OF DISCREPANCY. REMOVED AND REPLACED LT HYDRAULIC 
- [SDR DXTA200601786](https://openairdocs.org/sdr/DXTA200601786), Dec 7, 2006: PROCESSOR. INOPERATIVE. (MAU 1 FAILURE), AMBER CAS NO AIR DATA, AHRS; AUTO PILOT' ETC, ON LT SIDE IN FLIGHT. REPLACED NR 1 NIC PROC MODULE IAW MM 34-17-00. OPS OK IAW MM 34-23-10.
- [SDR DXTA200601594](https://openairdocs.org/sdr/DXTA200601594), Sep 7, 2006: COALESCER BAG. DIRTY. AFTER TAKEOFF THERE WAS AN ACRID SMELL IN THE COCKPIT. NO VISUAL SIGNS OF SMOKE WERE EVIDENT. REMOVED + CLEANED WATER SEPARATOR COALESCER CLOTH IAW CE-680 M/M C
- [SDR DXTA200601485](https://openairdocs.org/sdr/DXTA200601485), Jul 6, 2006: HANDLE. STUCK. AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT (THE GEAR HANDLE WAS STUCK IN THE DOWN POSITION.) SHORTLY AFTER TAKEOFF, THE WOW MISCOMPARE CAS MESSAGE ILLUMINATE
- [SDR DXTA200601374](https://openairdocs.org/sdr/DXTA200601374), Apr 24, 2006: POSITION SWITCH. OUT OF ADJUST. AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT. 1 MINUTE LATER THE WOW MISCOMPARE AMBER CAS MESSAGE ILLUMINATED AND REMAINED ON UNTIL 30 SECONDS AFTER LANDIN

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