# N381QS: 2006 Cessna 680, registration cancelled 2024-12-02 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 2, 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: 680-0097 - Year built: 2006 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: August 30, 2006 - Certificate issued: January 21, 2020 - Last registry action: September 30, 2023 - Mode S code: A46070 - 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/N381QS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=381QS - Page: https://openairdocs.org/deregistered/N381QS-2024-12-02 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 (30) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR JGVR20240212001](https://openairdocs.org/sdr/JGVR20240212001), Feb 12, 2024: SPAR. CORRODED. FOUND 2 SPOTS OF CORROSION ON AFT VERTICAL SPAR. FOUND DURING TASK 55-30-00-2200 DURING CORROSION BLEND OUT, FOUND CORROSION TO BE GOING UNDER FASTENER HEAD ON - [SDR 2023F00268](https://openairdocs.org/sdr/2023F00268), Sep 10, 2023: RIB. CRACKED. LH ELEVATOR WEDGES PANEL INBOARD ATTACH RIB IS CRACK. ACCOMPLISHED LH HORIZONTAL STABILIZER INBOARD RIB DAMAGE REPAIR IAW TEXTRON AVIATION REPAIR MEMO DQ41081M1 - [SDR DXTA2023082193590](https://openairdocs.org/sdr/DXTA2023082193590), Aug 21, 2023: BATTERY. INOPERATIVE. EMERGENCY LIGHTING: ALL THE EMERGENCY LIGHTS ASSOCIATED WITH NUMBER 4 BATTERY PACK ARE INOP. GAINED ACCESS TO AND REMOVED AND REPLACED #4 EMERGENCY LIGHT BATTER - [SDR DXTA2023061288450](https://openairdocs.org/sdr/DXTA2023061288450), Jun 12, 2023: UNKNOWN. UNKNOWN. ONCE DESCENDING PRESSURIZATION WILL RAPIDLY SPIKE UP TO 1000FT/MIN THEN STABILIZE CAUSING DISCOMFORT FOR PASSENGERS. CONTINUING THE DESCENT PRESSURIZATION WILL - [SDR 3J7R2023052200001](https://openairdocs.org/sdr/3J7R2023052200001), May 21, 2023: BATTERY PACK. DISCHARGED. FOUR LIGHTS OF THE EMERGENCY LIGHTING SYSTEM FAIL TO ILLUMINATE. THE LAV OVERHEAD LIGHT, THE TABLE OVERHEAD LIGHTS OF SEATS 5 AND 9, AND THE EMERGENCY EXIT FORW - [SDR DXTA2023051886480](https://openairdocs.org/sdr/DXTA2023051886480), May 17, 2023: ROD. BROKEN. MAIN DOOR: WHILE CLOSING THE DOOR SOME MINOR BINDING WAS ENCOUNTERED. THE DOOR WOULD NOT EXTEND FREELY ON OPENING AND FORCE WAS REQUIRED TO OVERCOME THE BINDING - [SDR DXTA2022030958180](https://openairdocs.org/sdr/DXTA2022030958180), Mar 8, 2022: LIGHT. DISCONNECTED. LAV EXIT SIGN/LIGHT: EMERGENCY EXIT SIGN ON BASE OF LAVATORY SEAT DOES NOT ILLUMINATE. //SIGNOFF/ FOUND EMERGENCY EXIT SIGN ON BASE OF LAVATORY SEAT TO BE DISCO - [SDR DXTA2022022156970](https://openairdocs.org/sdr/DXTA2022022156970), Feb 18, 2022: NONE. NONE. CABIN ODOR: AT 41,000FT, APU OFF, ANY POWER SETTING, ODOR FROM BOTH BLEEDS. CREW EYES AND THROAT STINGING, HEADACHE. RH ENGINE REMOVED AND REPLACED. ENG CAL AND - [SDR DXTA2021040840550](https://openairdocs.org/sdr/DXTA2021040840550), Apr 7, 2021: SIGN. INOPERATIVE. MAIN EXIT SIGN/LIGHT: EMERGENCY LIGHT INOP. REMOVED FAILED SPLICE FROM AFT LH BULKHEAD EMERGENCY EXIT SIGN AND REPLACED WITH NEW UNIT. IAW CE-680 SPM 20-30-25. - [SDR JGVR20200922001](https://openairdocs.org/sdr/JGVR20200922001), Sep 22, 2020: DRAG ANGLE. CORRODED. LEFT WING AFT DRAG ANGLE HAS 2 AREAS OF VERIFIED CORROSION ALONG OUTBOARD EDGE AND 8 AREAS OF VERIFIED CORROSION ON MIDDLE DRAG ANGLE OUTBOARD EDGE. RIGHT UPPER - [SDR 2019FA0000235](https://openairdocs.org/sdr/2019FA0000235), Jul 29, 2019: SPLICE STRAP. DEBONDED. HORIZONTAL STABILIZER LEFT SIDE LOWER SKIN SPLICE STRAP DE-BONDED. ACCOMPLISHED ENGINEERING LETTER DQ22440M1 DATED JULY 25, 2019; 680-0097 HORIZONTAL STABILIZER - [SDR JGVR28180402001](https://openairdocs.org/sdr/JGVR28180402001), Apr 2, 2018: TORQUE TUBE. CRACKED. CRACKED RUDDER TORQUE TUBE FROM RUDDER. REPLACED THE RUDDER TORQUE TUBE IAW SRM 51-40-03, 51-40-06, 51-60-03, 55-40-09, AND MM 20-40-20. - [SDR JGVR20170613002](https://openairdocs.org/sdr/JGVR20170613002), Jun 13, 2017: SKIN. CRACKED. CRACK ON LOWER RUDDER SKIN ON RT SIDE EXTENDING FROM BOTTOM OF RUDDER ONE INCH INTO A RIVET. REPAIRED THE RUDDER SKIN IAW ERO-897400, REV IR. PERFORMED EDDY CUR - [SDR DXTA2016092506308](https://openairdocs.org/sdr/DXTA2016092506308), Sep 25, 2016: SWITCH. OUT OF ADJUST. AT 500' ON CLIMBOUT AMBER, NOSE DOOR OPEN RT, CAS ILLUMINATED. WHEN TURNING FINAL AND AT A SLOWER SPEED IT EXTINGUISHED. ADJUSTED BOTH RT DOOR SWITCHES AND OPS - [SDR DXTA2014111605928](https://openairdocs.org/sdr/DXTA2014111605928), Nov 16, 2014: FIRE LOOP. FAILED. RECEIVED AN ENGINE FIRE DETECTOR FAIL ON RT CAS. R & R RT ENG OUTER FIRE LOOP. PERFORMED OPERATIONS CHECK, OPERATIONS CHECKED GOOD AT THIS TIME IAW MM 26-10-01. - [SDR DXTA2013122005602](https://openairdocs.org/sdr/DXTA2013122005602), Dec 4, 2013: FITTING. CORRODED. CORRODED WING RIB FITTINGS. REPAIRED IAW REPAIR DEF S-680-ATA57/01RD - [SDR CWQR20130408028](https://openairdocs.org/sdr/CWQR20130408028), Apr 8, 2013: HEAT EXCHANGER. CRACKED. DURING A SCHEDULED INSPECTION, NOTICED HEAT EXCHANGER SIDE PLATE HAD 3. 35" LONG CRACK AND THE OPPOSITE SIDE WAS ALSO CRACKED IN ONE CORNER. WE PERFORMED A LEAK - [SDR CWQR20130408027](https://openairdocs.org/sdr/CWQR20130408027), Apr 8, 2013: HEAT EXCHANGER. CRACKED. DURING A SCHEDULED INSPECTION, HEAT EXCHANGER SIDE PLATE HAD A .35" LONG CRACK AND THE OPPOSITE SIDE WAS ALSO CRACKED IN ONE CORNER. PERFORMED A LEAK DOWN TEST - [SDR DXTA2012061804999](https://openairdocs.org/sdr/DXTA2012061804999), Jun 16, 2012: UPLOCK. OUT OF ADJUST. LANDING GEAR UNLOCK ANNUNCIATOR ILLUMINATED AT FL430 AND REMAINED ON UNTIL GEAR HANDLE WAS SELECTED TO THE DOWN POSITION. PERFORMED SEVERAL LANDING GEAR RETRACT - [SDR DXTA2011051604583](https://openairdocs.org/sdr/DXTA2011051604583), May 13, 2011: STRUT. DISCHARGED. LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. WOW MISCOMPARE CAS MSG ILLUMINATED. GEAR HANDLE WOULD NOT MOVE. CHECKED SQUAT SWITCH RIGGING ON ALL 3 GEARS. NO DE - [SDR DXTA2010122304376](https://openairdocs.org/sdr/DXTA2010122304376), Dec 22, 2010: VALVE. LEAKING. GEAR WOULD NOT RETRACT (HANDLE LOCKED OUT) WOW MISCOMPARE. VISUALLY INSPECTED SQUAT SWITCHES. OPS CHECKED ALL SQUAT SWITCHES AND VERIFIED INPU IN OT IAW PCB JAC - [SDR DXTA2010120704352](https://openairdocs.org/sdr/DXTA2010120704352), Dec 6, 2010: OIL SYSTEM. OVERSERVICED. AFTER LANDING AND WITHIN 3-5 MINS OF STARTING APU AND SELECTING THE BLEED AIR "ON", THE CABIN FILLED WITH SMOKE AND AN ODOR OF OIL. FOUND APU OIL OVER SERVICED. - [SDR DXTA2009051803656](https://openairdocs.org/sdr/DXTA2009051803656), May 17, 2009: CONTROLLER. MALFUNCTIONED. PRIMARY PITCH TRIM FAIL - POSSIBLY RAN AWAY BUT CAUGHT BY THE CREW. SECONDARY TRIM WORKED AS NEEDED. TOOK BOTH CREW MEMBERS TO INITIALLY LEVEL THE PLANE. LANDED - [SDR DXTA2009031603545](https://openairdocs.org/sdr/DXTA2009031603545), Mar 14, 2009: DISPLAY. SHORTED. APPROX 1.5 HR AFTER TAKEOFF THE LT MCDU (FMS CDU) BECAME INOP (BLANK SCREEN / NO RED X) LT MCDU CB WAS NOT TRIPPED. APPROX 5-10 MINS LATER STARTED SMELLING SLIG - [SDR DXTA200803205](https://openairdocs.org/sdr/DXTA200803205), Jul 29, 2008: WARNING SYSTEM. FALSE ACTIVATION. AFTER TAKEOFF INFLIGHT ANYTIME PITCH TRIM IS ACTIVATED EITHER NOSE UP OR DOWN, AMBER "AP STAB TRIM INOP" & AMBER "PRIMARY STAB TRIM FAIL" & CYAN "AP FAIL A & B" - [SDR DXTA200802861](https://openairdocs.org/sdr/DXTA200802861), Feb 10, 2008: CABIN PRESSURE. MALFUNCTIONED. ON CLIMBOUT, AC PRESSURIZED UNTIL 9.3 PSI SWITCHED TO MANUAL AND WAS ABLE TO CONTROL PRESSURIZATION, SWITCHED BACK TO AUTO FOR THE DESCENT AND APPEARED TO OPERA - [SDR DXTA200802804](https://openairdocs.org/sdr/DXTA200802804), Jan 28, 2008: HEATER. MALFUNCTIONED. AMBER PITOT STATIC COLD R CAME ON DURING T/O ROLL. CYCLED SEVERAL TIMES, INTERMITTENT THEREAFTER. TROUBLESHOT PITOT STATIC SYS AND FOUND SYS TO WORK NORMAL SEVE - [SDR DXTA200702245](https://openairdocs.org/sdr/DXTA200702245), Jun 6, 2007: UNKNOWN. UNKNOWN. AIRCRAFT REQUIRES 2/3 SCALE LT RUDDER TRIM TO MAINTAIN COORDINATED FLIGHT. [07-09-07] RUDDER SKIN DAMAGED AT UPPER, MIDDLE AND LOWER RUDDER HINGE AREA. REMOVED - [SDR DXTA200702229](https://openairdocs.org/sdr/DXTA200702229), May 31, 2007: COUPLER. INOPERATIVE. ON TAKEOFF, WE RECEIVED A (NO TO CAS) MESSAGE THAT WAS CAUSED BY THE SPOILERS. REMOVED AND REPLACED RT SPEED BRAKE COUPLER. PERFORMED ELECTRONIC RIGGING IAW MM - [SDR DXTA200601822](https://openairdocs.org/sdr/DXTA200601822), Dec 28, 2006: TRANSFER PUMP. INOPERATIVE. CROSS FEED (ON) IN AIR (2 OCCASIONS). CROSS FEED VALVES FAILED TO OPEN, BOTH FUEL BOOST PUMPS (LOW PRESS) CAME ON. EICAS MESSAGES APPROPRIATE AMBER FUEL PRESS L --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). 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