# N382QS: 2008 Cessna 680, registration cancelled 2024-12-06 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 6, 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: 680-0245 - Year built: 2008 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 16, 2008 - Certificate issued: September 30, 2020 - Last registry action: March 17, 2023 - Mode S code: A46427 - 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/N382QS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=382QS - Page: https://openairdocs.org/deregistered/N382QS-2024-12-06 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 (39) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DXTA2024090900440](https://openairdocs.org/sdr/DXTA2024090900440), Sep 4, 2024: CONNECTOR. DAMAGED. EMERGENCY LIGHTING: MAIN EXIT DOOR EXIT SIGNS NOT ILLUMINATING ALING WITH THE GALLEY WORK LIGHT ALL THE REST OF THE EMERGENCY LIGHTS WORK PROPERLY. CORRECTIVE A - [SDR DXTA2024071212336](https://openairdocs.org/sdr/DXTA2024071212336), Jul 11, 2024: BATTERY. DEFECTIVE. EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK #4 REMAIN ILLUMINATED WHEN ALL POWER IS REMOVED FROM THE AIRCRAFT. THE EMER LIGHTS WERE NO LONGER ON. WITH TH - [SDR 2023F00306](https://openairdocs.org/sdr/2023F00306), Oct 17, 2023: WEB. CRACKED. LH WING FWD WEB P/NP/N 6910269-39. CRACKED. ACCOMPLISHED TEXTRON AVIATION ENGINEERING REPAIR OF THE LH WING FWD WEB CRACK SR-680A-ATA57-33170 DATED APRIL 25, 20 - [SDR 2023F00287](https://openairdocs.org/sdr/2023F00287), Sep 25, 2023: SPAR CAP. CORRODED. RH LOWER REAR SPAR CAP CORRODED. ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ41229M1 DATED SEPTEMBER 21, 2023; RH LOWER REAR SPAR CAP CORROSION. - [SDR 2023F00286](https://openairdocs.org/sdr/2023F00286), Sep 25, 2023: UNKNOWN. UNKNOWN. LH LOWER REAR SPAR CAP CORRODED. ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ41230M1 DATED SEPTEMBER 21, 2023; LH LOWER REAR SPAR CAP CORROSION. - [SDR DXTA2023072491650](https://openairdocs.org/sdr/DXTA2023072491650), Jul 23, 2023: CONDENSER. DIRTY. PNEUMATIC DISTRIBUTION: DURING A LONGER FLIGHT, ONCE THE CABIN BECOMES COLD SOAKED, AND THE SUPPLY DUCT TEMPERATURE WARMS UP WE NOTICED A SLIGHT OIL BURNING ODO - [SDR DXTA2023060888160](https://openairdocs.org/sdr/DXTA2023060888160), Jun 7, 2023: FLAG. DAMAGED. MAIN CABIN DOOR EXTERIOR FLAG INDICATOR, REMAINS RED WITH THE DOOR HANDLE IN THE STOW DOWN POSITION. NORMAL INDICATION WOULD BE BLACK AND WHITE CROSS MARKS. VER - [SDR EBVR202305180001](https://openairdocs.org/sdr/EBVR202305180001), May 18, 2023: UNKNOWN. UNKNOWN. CORROSION FOUND ON VERTICAL STAB SPAR LH CAP ANGLE BETWEEN VFS 180-184. REPAIRED USING TEXTRON FIELD REPAIR FR-680-0245-11912 AND 8100-9 DATED 17MAY2023. THIS I - [SDR DXTA2022120775710](https://openairdocs.org/sdr/DXTA2022120775710), Dec 6, 2022: COUNTERBALANCE. OUT OF ADJUST. DOOR SEEMS TO BE OUT OF RIG. THE BOTTOM STEP APPEARS TO BE 3 TO 4 INCHES HIGHER THAN NORMAL. ALSO THE COUNTERBALANCE IS NOT WORKING WHEN THE DOOR IS CLOSED. IT - [SDR DXTA2022070565260](https://openairdocs.org/sdr/DXTA2022070565260), Jul 3, 2022: BATTERY. INOPERATIVE. CABIN EMERG LIGHT: DURING POWER ON CHECKLIST ALL EMERERGENCY LIGHTS INOP. WITH BATTERY ON EMERGENCY LIGHTS OPERATIONAL. "CORRECTIVE ACTION" COMPLIED WITH CE-680 - [SDR DXTA2022010354690](https://openairdocs.org/sdr/DXTA2022010354690), Jan 1, 2022: NOT REPORTED. NOT REPORTED. EMERGENCY LIGHT SWITCH: WHEN YOU TURN THE EMER LIGHTS SWITCH OFF THE FOLLOWING LIGHTS REMAIN ON: AFT OVER WING EMERGENCY LIGHT. EXIT LIGHT IN THE DIVIDER, OVERH - [SDR DXTA2021060743320](https://openairdocs.org/sdr/DXTA2021060743320), Jun 6, 2021: STRUCTURE. BENT. MAIN DOOR: MAIN CABIN DOOR CORNER BENT OUT APPROXIMATELY 3/4 INCH(JUST TO THE RIGHT OF THE HANDLE). // SIGNOFF // MAIN ENTRANCE DOOR LOWER HALF AFT MID SECTION - [SDR JGVR20210526003](https://openairdocs.org/sdr/JGVR20210526003), May 26, 2021: SPAR CAP. CORRODED. MECHANICALLY REMOVED 2 AREAS OF CORROSION LOCATED ON AFT SPAR , LOWER SPAR CAP AT WS 37.00. FOUND INBD BLEND TO BE WITHIN LIMITS. PER NJA GMM 2.2.2 THIS IS LEVE - [SDR JGVR20210526002](https://openairdocs.org/sdr/JGVR20210526002), May 26, 2021: RIB. CORRODED. MECHANICALLY REMOVED AREA OF CORROSION LOCATED IN RH WING GEARWELL BAY 720DR OUTBD RIB LOWER MIDDLE AREA IAW C680 SRM 51-70-02. FOUND CORROSION BLEND TO BE BEYO - [SDR JGVR20210526001](https://openairdocs.org/sdr/JGVR20210526001), May 26, 2021: RIB. CORRODED. MECHANICALLY REMOVED AREA OF CORROSION LOCATED IN LH WING GEARWELL BAY 730DL OUTBD RIB LOWER MIDDLE AROUND HI-LOK IAW C680 SRM 51-70-02. FOUND CORROSION BLEND T - [SDR DXTA2021041240650](https://openairdocs.org/sdr/DXTA2021041240650), Apr 10, 2021: SENSOR. DEFECTIVE. ENG FIRE DETECT FAIL R AMBER CAS: IN CRUISE FLIGHT AT FL380 AMBER 'ENG FIRE DETECT FAIL R' CAS MESSAGE DISPLAYED. REMOVED INTERNAL FIRE & OVERHEAT SENSOR, PN:- - [SDR JGVR20210219003](https://openairdocs.org/sdr/JGVR20210219003), Feb 19, 2021: DOOR FRAME. CORRODED. REMOVED THE FWD AND AFT CONTOUR RINGS FROM THE EMERGENCY EXIT DOOR AND FOUND SEVERE AREAS OF CORROSION ON THE DOOR STRUCTURE. SENT THE EMERGENCY EXIT DOOR OUT F - [SDR JGVR20210219002](https://openairdocs.org/sdr/JGVR20210219002), Feb 19, 2021: STRUCTURE. CORRODED. MECHANICALLY BLENDED AREAS OF BUBBLING PAINT AND CORROSION FROM MAIN CABIN DOOR STRUCTURE, LOCATED UNDER MOVABLE STEP BETWEEN THE TWO CENTER ATTACH POINTS, PERF - [SDR JGVR20210219001](https://openairdocs.org/sdr/JGVR20210219001), Feb 19, 2021: FLOOR SUPPORT. CORRODED. MECHANICALLY BLENDED SEVEN AREAS OF CORROSION IN CABIN DROP AISLE FLOOR CONSISTING OF TWO AREAS ON LT FWD ANGLE APPROXIMATELY 3.5 AND 8 INCHES AFT OF FWD END OF - [SDR JGVR20200605001](https://openairdocs.org/sdr/JGVR20200605001), Jun 5, 2020: RIB. CORRODED. CORROSION AROUND 2 HI-LOKS ON UPPER OUTBOARD RIB ABOVE LT MLG AT APPROXIMATELY MIDLINE. REMOVED 2 HI-LOK FASTENERS AND MECHANICALLY BLENDED CORROSION IN AREA AR - [SDR 2TJR201910210001](https://openairdocs.org/sdr/2TJR201910210001), Oct 21, 2019: SPAR CAP. CORRODED. CORROSION WAS FOUND AT THREE LOCATIONS ON THE 6931012-1 LH AFT SPAR CAP OF THE VERTICAL STABILIZER. ALL CORROSION WAS REMOVED BY BLENDING IAW CESSNA FIELD REPAI - [SDR DXTA2018052100157](https://openairdocs.org/sdr/DXTA2018052100157), May 21, 2018: SKIN. CORRODED. TAILCONE SKIN CORRODED. - [SDR DXTA2018FA0000156](https://openairdocs.org/sdr/DXTA2018FA0000156), May 21, 2018: DRAG ANGLE. CRACKED. RT WING DRAG ANGLE CRACKED. - [SDR DXTA2016020206175](https://openairdocs.org/sdr/DXTA2016020206175), Feb 1, 2016: SWITCH. FAULTY. LEFT MAIN GEAR STAYED DOWN AFTER GEAR RETRACTION WITH A LT GEAR DOWN GREEN INDICATION & NO RED INDICATION. OHMED OUT LT GEAR UPLOCK SWITCH SG007 & FOUND WITH TH - [SDR DXTA2015101206106](https://openairdocs.org/sdr/DXTA2015101206106), Oct 6, 2015: BRAKE ASSY. LOCKED. EMERGENCY BRAKING WAS USED & RT OTBD TIRE APPEARS TO HAVE LOCKED UP & BLOWN. REMOVED FAULTY RT NR 3 & 4 WHEEL & TIRE ASSEMBLY. INSTALLED OVERHAULED NR 3 & 4 WHE - [SDR DXTA2015100606103](https://openairdocs.org/sdr/DXTA2015100606103), Oct 6, 2015: HYDRAULIC LINE. FAULTY. IMMEDIATELY AFTER GEAR EXTENSION & 3 GREEN GEAR DOWN & LOCK LIGHTS, RECEIVED AMBER HYD VOLUME LOW CAS MSG. EMER BRAKING WAS USED & RT OTBD TIRE APPEARS TO HAVE - [SDR CWQR20130305013](https://openairdocs.org/sdr/CWQR20130305013), Mar 5, 2013: HEAT EXCHANGER. CRACKED. DURING A SCHEDULED INSPECTION WE WERE PREFORMING A PRODUCT IMPROVEMENT (REPLACEMENT OF DUCT ASSY 6914070-67) WE NOTICED THAT THE HEAT EXCHANGER SIDE PLATE HAD 2 - [SDR CWQR20130305014](https://openairdocs.org/sdr/CWQR20130305014), Mar 5, 2013: HEAT EXCHANGER. CRACKED. HEAT EXCHANGER SIDE PLATE HAD TWO CRACKS ABOUT .37 INCH LONG. THE OPPOSITE SIDE OF THE HEAT EXCHANGER WAS CRACKED IN THREE OF THE FOUR CORNERS. A NEW HEAT EXCHA - [SDR CWQR20121221054](https://openairdocs.org/sdr/CWQR20121221054), Dec 21, 2012: TUBE. CRACKED. ACFT CAME IN WITH A REPORTED TREND SHIFT IN ITT. DURING AN ENGINE RUN, FOUND A BLEED AIR LEAK ON THE TOP SIDE OF THE RT ENGINE. REMOVED CLAMP AND FOUND THE TUBE - [SDR DXTA2012092405133](https://openairdocs.org/sdr/DXTA2012092405133), Sep 24, 2012: DOOR FRAME. CORRODED. MINOR CORROSION FOUND ADJACENT TO AFT SHEAR TIE ON CABIN DOOR FRAME. .023 DEEP, OUT OF LIMITS, DOOR FRAME WILL BE CHANGED. - [SDR DXTA2011092004733](https://openairdocs.org/sdr/DXTA2011092004733), Sep 19, 2011: BRAKE. LEAKING. MAIN WHEEL LEAKING HYD FLUID. BRAKES VERY RIGID ON BOTH RUDDER PEDALS WHEN BRAKES APPLIED ON TAXI/TAKEOFF/LANDING ROLLOUT. BOTH PILOT BRAKE APPLICATIONS REQUIRE - [SDR DXTA2010092804253](https://openairdocs.org/sdr/DXTA2010092804253), Sep 27, 2010: LANDING GEAR. MALFUNCTIONED. RED MLG UNLOCK INDICATION REMAIND ILLUMINATED AFTER MLG HANDLE WAS PLACED IN THE UP POSITION. 3 GREEN MLG INDICATORS EXTINGUISHED. MLG DEPLOYED NORMALLY. JACKED - [SDR DXTA2010032304049](https://openairdocs.org/sdr/DXTA2010032304049), Mar 22, 2010: STRUT. MALFUNCTIONED. ON DEPARTURE, LANDING GEAR HANDLE COULD NOT BE MOVED TO THE UP POSITION, LANDING GEAR REMAINED DOWN AND LOCKED. APPROX 1-2 MINS LATER THE "WOW MISCOMPARE" CAS M - [SDR DXTA2009111003856](https://openairdocs.org/sdr/DXTA2009111003856), Nov 9, 2009: LANDING GEAR. MALFUNCTIONED. WHILE ENROUTE AT FL400, APPROX 25 MINUTES INTO FLIGHT, NOSE GEAR EXTENDED UNCOMMANDED, NOSE DOORS OPENED, THEN NOSE GEAR RETRACTED VERY ABRUPTLY. INDICATIONS ON - [SDR DXTA2009111003852](https://openairdocs.org/sdr/DXTA2009111003852), Nov 9, 2009: LANDING GEAR. MALFUNCTIONED. WHILE EN ROUTE AT FL400, APPROX 25 MINUTES INTO FLIGHT, NOSE GEAR EXTENDED UNCOMMANDED, NOSE DOORS OPENED, THEN NOSE GEAR RETRACTED VERY ABRUPTLY. INDICATIONS O - [SDR DXTA2008122703444](https://openairdocs.org/sdr/DXTA2008122703444), Dec 27, 2008: SWITCH. SHORTED. AT APPROX 13,000 FT ON APPROACH, GOT AN "AMC O' HEAT" TEMP CAS MESSAGE FOLLOWED BY AN EMER PRESS ACTIVATION. SHORTLY AFTER EMER PRESS CAME ON CABIN STARTED TO A - [SDR DXTA2008122903444](https://openairdocs.org/sdr/DXTA2008122903444), Dec 27, 2008: UNKNOWN. SMOKE. SMOKE IN COCKIT DURING APPROACH - [SDR DXTA20082935](https://openairdocs.org/sdr/DXTA20082935), Mar 12, 2008: UPLOCK SENSOR. MALFUNCTIONED. UPON GEAR RETRACTION, OUT OF DEPARTURE, RT GEAR WOULD NOT RETRACT. REMOVED AND REPLACED RT UPLOCK SWITCH WITH NEW. C/W FULL GEAR FUNCTIONAL CHECK. ALL OPS CHECK - [SDR DXTA20082880](https://openairdocs.org/sdr/DXTA20082880), Feb 17, 2008: LANDING GEAR. MALFUNCTIONED. MANUAL GEAR EXTENSION WITH BLOW DOWN DUE TO NOSE GEAR NOT EXTENDED DURING LANDING. RESET BLOWDOWN BOTTLE AND SERVICED SWING GEAR MULTIPLE TIMES. UNABLE TO DUPLI --- 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.