# N370QS: 2006 Cessna 680, registration cancelled 2025-07-28

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 28, 2025
- 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: 680-0099
- Year built: 2006
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 15, 2006
- Certificate issued: June 1, 2021
- Last registry action: May 19, 2023
- Mode S code: A4353A
- 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/N370QS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=370QS
- Page: https://openairdocs.org/deregistered/N370QS-2025-07-28

From the FAA registry file of November 4, 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 (54, newest 50)

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

- [SDR DXTA2024120201355](https://openairdocs.org/sdr/DXTA2024120201355), Dec 1, 2024: COUNTERBALANCE. OUT OF ADJUST. ENTRANCE STAIR: COUNTER BALANCE ON MAIN CABIN DOOR. DOOR IS VERY HEAVY TO CLOSE AND FALLS OPEN EASILY. CORRECTIVE ACTION; ADJUSTED BOTH REELS OPS CHECK GOOD. AL
- [SDR 2024F00296](https://openairdocs.org/sdr/2024F00296), Nov 20, 2024: SKIN. NICKED. DURING ELEVATOR TRAVEL CHECKS NOTICED SKIN DAMAGE AROUND THE TRIM ACTUATOR COVE AREA. UPPER ELEVATOR SKIN AND LOWER TRIM ACTUATOR COVE SKIN.
- [SDR 2024F00295](https://openairdocs.org/sdr/2024F00295), Nov 20, 2024: SPAR. CHAFED. WHILE ACCOMPLISHING ELEVATOR TRAVEL CHECKS FOUND ELEVATOR CONTROL HORNS HITTING HILOCKS PREVENTING FULL TRAVEL, NEED TO LOOK INTO AQRD REPAIR DEFINITION OF VERT
- [SDR JGVR20231114002](https://openairdocs.org/sdr/JGVR20231114002), Nov 14, 2023: UNKNOWN. UNKNOWN. LH/RH H STAB UPPER AND LOWER SKINS ON THE TRAILING EDGE HAVE MULTIPLE AREAS OF CORROSION. MECHANICALLY BLENDED MULTIPLE AREAS OF CORROSION ON LH AND RH, UPPER A
- [SDR JGVR20231114001](https://openairdocs.org/sdr/JGVR20231114001), Nov 14, 2023: UNKNOWN. UNKNOWN. REPAIRED HORIZONTAL STABILIZER RH LOWER SKIN DUE TO LEVEL 2 CORROSION. MECHANICALLY BLENDED MULTIPLE AREAS OF CORROSION ON RH LOWER HORIZONTAL STABILIZER TRAILI
- [SDR JGVR20231113001](https://openairdocs.org/sdr/JGVR20231113001), Nov 13, 2023: UNKNOWN. UNKNOWN. RH VERT AFT SPAR IS HEAVILY CORRODED. LOCATED ABOVE RUDDER UPPER HINGE. REPAIRED 2 BLENDED AREAS OF VERTICAL STABILIZER R/H AFT SPAR CAP AT APPROXIMATELY VFS 17
- [SDR JGVR20231005002](https://openairdocs.org/sdr/JGVR20231005002), Oct 5, 2023: UNKNOWN. UNKNOWN. REPAIRED CORRODED AREAS ON THE RUDDER LEADING EDGE NEAR THE BALANCE WEIGHT HARDWARE BY BLENDING AREAS, PERFORMING NDT AND REPORTING FOR REPAIR DISPOSITION. REPA
- [SDR JGVR20201104005](https://openairdocs.org/sdr/JGVR20201104005), Nov 4, 2020: SUPPORT BRACKET. CORRODED. FOUND LT AND RT LOWER RUDDER SUPPORT BRACKETS CORRODED BEYOND REPAIR AND REPLACED WITH NEW CESSNA P/NS 6931045-17 AND 69031045-18.
- [SDR JGVR20201104004](https://openairdocs.org/sdr/JGVR20201104004), Nov 4, 2020: PLATE. CORRODED. FOUND SEVERE CORROSION OF THE UPPER RIB PLATE OF THE VERTICAL STABILIZER’S RUDDER TRIM ACTUATOR MOUNT, REPLACED WITH A NEW CESSNA P/N 6961526-5 WET WITH PS870B 
- [SDR JGVR20201104003](https://openairdocs.org/sdr/JGVR20201104003), Nov 4, 2020: SKIN. CORRODED. BLENDED CORRODED AREA ON THE UPPER SURFACE OF THE UPPER WING SKIN, JUST INBOARD OF THE LT OVER-WING FUEL FILLER, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITI
- [SDR JGVR20201104002](https://openairdocs.org/sdr/JGVR20201104002), Nov 4, 2020: SPAR CAP. CORRODED. BLENDED MULTIPLE CORRODED AREAS ON THE LT AND RT SPAR CAPS AND WEB OF THE VERTICAL STABILIZER AFT SPAR, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPLA
- [SDR JGVR20201104001](https://openairdocs.org/sdr/JGVR20201104001), Nov 4, 2020: SKIN. CORRODED. REMOVED THE LT UPPER WING DRAG MIDDLE AND AFT ANGLES (WING-TO-FUSELAGE FAIRINGS) AND BLENDED CORRODED AREAS OF THE UPPER SURFACE OF THE LT UPPER WING SKIN, PERF
- [SDR 2020FA0000217](https://openairdocs.org/sdr/2020FA0000217), Apr 6, 2020: INLET. DAMAGED. LH ENGINE INLET DUCT DEEP COUNTERSINK. REFERENCE TEXTRON AVIATION ENGINEERING MEMO: DQ25329M1 RRL DATED: 3/31/2020.
- [SDR 2020FA0000216](https://openairdocs.org/sdr/2020FA0000216), Apr 6, 2020: SKIN. CORRODED. R/H HORIZONTAL STABILIZER UPPER SKIN CORROSION. REFERENCE FAA FORM 8100-9, FR-680-0099-7851 REV- DATED: 4/3/2020.
- [SDR 2020FA0000215](https://openairdocs.org/sdr/2020FA0000215), Apr 6, 2020: SKIN. CORRODED. MINOR CORROSION AROUND HILOCK COLLARS IN LH AND RH MLG WHEEL WELL ABOVE TRUNNION. REFERENCE TEXTRON AVIATION ENGINEERING MEMO DQ25322M1 RRL DATED: APRIL 1, 2020
- [SDR 2020FA0000214](https://openairdocs.org/sdr/2020FA0000214), Apr 6, 2020: DOOR. CORRODED. EMERGENCY EXIT DOOR CORROSION. REFERENCE TEXTRON AVIATION ENGINEERING MEMO DQ25313M1 RRL DATED: MARCH 31, 2020.
- [SDR DXTA2019121203190](https://openairdocs.org/sdr/DXTA2019121203190), Dec 11, 2019: UNKNOWN. ODOR. COCKPIT ODOR BURNING SMELL - BURNING ODOR NOTICED BY CREW AT 11000 FEET IN CRUISE. SOURCE COULD NOT BE IDENTIFIED AND CRASH/FIRE/RESCUE COULD NOT IDENTIFY A HEA
- [SDR 2019F00205](https://openairdocs.org/sdr/2019F00205), May 15, 2019: FAIRING. CRACKED. LT LOWER WING FAIRING TRIM CRACK REPAIR RFTS-103325 REV 0 DATED MAY 15, 2019.
- [SDR 2019F00193](https://openairdocs.org/sdr/2019F00193), May 6, 2019: TRUSS. CORRODED. APU TRUSS MOUNT (FLANGE) CORROSION. REFERENCE ENGINEERING MEMO DQ19368M1 DATED: MAY 3, 2019.
- [SDR DXTA2019011001901](https://openairdocs.org/sdr/DXTA2019011001901), Jan 10, 2019: DISPLAY. OVERHEATED. DU3 WENT BLANK AND ELECTRICAL SMOKES FUMES NOTICED CLIMBING THROUGH FL360. RAN EMERGENCY CHECKLIST AND DIVERTED INTO KFSM. **SUPPLEMENTAL INFORMATION: REMOVED &
- [SDR DXTA2018123101854](https://openairdocs.org/sdr/DXTA2018123101854), Dec 31, 2018: ACTUATOR. FAULTY. AFTER RETRACTING THE GEAR ON TAKEOFF, THE LEFT MAIN INDICATOR CONTINUED TO SHOW IT WAS DOWN AND LOCKED. WE DIDN'T HAVE A RED UNLOCK, OR ANY HORN. PER THE CHECKL
- [SDR JGVR20171206002](https://openairdocs.org/sdr/JGVR20171206002), Dec 6, 2017: AXLE. CORRODED. LH MLG AXLE HAS AREAS OF MISSING CHROME AND RUST. REMOVED LH MLG TRAILING LINK FOR AXLE REPLACEMENT AND FOUND BOTH TRUNNION LUGS TO BE CORRODED ON OUTER SURFACE
- [SDR JGVR20171206001](https://openairdocs.org/sdr/JGVR20171206001), Dec 2, 2017: PANEL. CORRODED. LEVEL 1 CORROSION AROUND MULTIPLE FASTENERS ON LH AND RH H-STAB IB CLOSEOUT PANELS 351AC AND 352AC. BLENDED LEVEL 1 CORROSION AROUND MULTIPLE FASTENERS ON LH AN
- [SDR DXTA2017031906386](https://openairdocs.org/sdr/DXTA2017031906386), Mar 19, 2017: CIRCUIT BOARD. FAILED. ENGINE FIRE DETECT FAIL LEFT CAS MESSAGE DISPLAYED INFLIGHT. CB TRIPPED. TROUBLESHOT TO LEFT ENG FIRE & SMOKE PRINTED CIRCUIT BOARD. REMOVED AND REPLACED THE PC
- [SDR JGVR201609210008](https://openairdocs.org/sdr/JGVR201609210008), Sep 21, 2016: ATTACH ANGLE. CORRODED. CORROSION ON UPPER TAIL CONE COVER FAIRING ATTACH ANGLES. THE AREAS THAT CORRODE ONLY HAVE PRIMER PAINT. SHOULD BE PAINTED WITH AN ADDITIONAL CORROSION RESISTAN
- [SDR JGVR201609210007](https://openairdocs.org/sdr/JGVR201609210007), Sep 21, 2016: SPAR WEB. CORRODED. CORROSION ON THE FORWARD WEB IN LT WHEEL WELL AROUND LT INBD BRAKE FITTING. SUGGEST APPLYING CPC TO WHEEL WELL SPARS.
- [SDR JGVR201609210006](https://openairdocs.org/sdr/JGVR201609210006), Sep 21, 2016: FITTING. CORRODED. CORROSION FOUND AROUND EMERGENCY BRAKE LINE FITTING ON OTBD SIDE OF WS 37.00 IN RT MLG WHEEL WELL. SUGGEST APPLYING CPC IN WHEEL WELLS.
- [SDR JGVR201609210005](https://openairdocs.org/sdr/JGVR201609210005), Sep 21, 2016: SPAR WEB. CORRODED. CORROSION ON THE FORWARD WEB IN THE RT MLG WHEEL WELL AROUND THE RT INBD BRAKE FITTING. SUGGEST APPLYING CPC ON THE WHEEL WELL SPARS.
- [SDR JGVR201609210004](https://openairdocs.org/sdr/JGVR201609210004), Sep 21, 2016: THRUST REVERSER. CORRODED. CORROSION ON THE OUTER SKIN OF THE LT AND RT THRUST REVERSER LOWER BUCKETS. SUGGEST PAINTING WITH A HIGH TEMPERATURE CORROSION RESISTANT PAINT SIMILAR TO WHAT I
- [SDR JGVR201609210003](https://openairdocs.org/sdr/JGVR201609210003), Sep 21, 2016: THRUST REVERSER. CORRODED. CORROSION ON THE OUTER SKIN OF THE LT AND RT THRUST REVERSER BUCKETS. SUGGEST PAINTING WITH A HIGHER TEMPERATURE CORROSION RESISTANT PAINT SIMILAR TO WHAT IS US
- [SDR JGVR201609210002](https://openairdocs.org/sdr/JGVR201609210002), Sep 21, 2016: SKIN. CORRODED. CORROSION ON UPPER SURFACE OF LT ELEVATOR FORWARD OF TRIM TAB.
- [SDR JGVR201609210001](https://openairdocs.org/sdr/JGVR201609210001), Sep 21, 2016: THRUST REVERSER. CORRODED. CORROSION ON THE OUTER SKIN OF THE LT AND RT THRUST REVERSER LOWER BUCKETS. SUGGEST PAINTING WITH A HIGH TEMPERATURE CORROSION RESISTANT PAINT SIMILAR TO WHAT I
- [SDR DXTA2015110606118](https://openairdocs.org/sdr/DXTA2015110606118), Nov 7, 2015: CIRCUIT BOARD. FAILED. UPON GEAR RETRACTION, ENCOUNTERED A LOUD CONTINUOUS BANGING NOISE ALONG WITH SEVERE VIBRATIONS. RED GEAR UNLOCK LIGHT REMAINED ON UNTIL THUMPING STOPPED. PROBLE
- [SDR DXTA2014102805918](https://openairdocs.org/sdr/DXTA2014102805918), Oct 27, 2014: FIRE WARNING. FALSE ACTIVATION. AMBER CAS MESSAGE FOR RT ENGINE FIRE DETECTION ILLUMINATED INFLIGHT 15 - 20 TIMES. PERFORMED ENGINE RUNS AND COULD NOT DUPLICATE FAULT. MEASURED RESISTANCE OF R
- [SDR DXTA2014100105902](https://openairdocs.org/sdr/DXTA2014100105902), Sep 30, 2014: MODULE. FAILED. AMBER CAS MESSAGE FOR THE RT ENGINE FIRE DETECTION FAILED ILLUMINATED 15 MINUTES INTO FLIGHT. RAN ENGS & ATTEMPTED TO DUPLICATE SQUAWK. NO FAIL LIGHT PRESENT AF
- [SDR DXTA2014092905898](https://openairdocs.org/sdr/DXTA2014092905898), Sep 26, 2014: FIRE DETECTOR. FAILED. AMBER ENGINE FIRE DETECTOR FAILED RT CAS MESSAGE ILLUMINATED DURING FLIGHT. RANG OUT INNER FIRE LOOP, RINGS GOOD. INSPECTED WIRING HARNESS, NO DAMAGE FOUND. R &
- [SDR DXTA2014092505892](https://openairdocs.org/sdr/DXTA2014092505892), Sep 23, 2014: PRINTED CKT BOARD. FAULTY. DURING INITIAL CLIMB OUT ENG FIRE DETECT FAIL R CAS MSG POSTED. THE MSG CLEARED & RE-POSTED SEVERAL TIMES DURING FLIGHT. THIS WAS NOT ASSOCIATED WITH ANY THROTT
- [SDR DXTA2014092205890](https://openairdocs.org/sdr/DXTA2014092205890), Sep 21, 2014: FIRE LOOP. FAULTY. UPON DEPARTURE ENG FIRE DETECT FAIL R ILLUMINATED STEADY. DURING DESCENT BECAME INTERMITTENT & EXTINGUISHED ITSELF ON SHORT FINAL. R & R RT ENG FIRE LOOP IAW MM
- [SDR 2014F00140](https://openairdocs.org/sdr/2014F00140), Jul 19, 2014: COALESCER BAG. DIRTY. TWENTY MINUTES AFTER TAKEOFF AND CRUISING AT 15,000 FT, THE APU WAS STARTED AND A STRONG ELECTRICAL BURNING ODOR WAS NOTED. THE BLEED AIR WAS TURNED OFF AND APU
- [SDR DXTA2014072105823](https://openairdocs.org/sdr/DXTA2014072105823), Jul 19, 2014: COALESCER BAG. DIRTY. TWENTY MINUTES AFTER TAKEOFF AT 15000 FT, APU STARTED USING THE APPROPRIATE CHECKLIST. AFTER THE APU STABILIZED & THE BUSS TIE WAS OPENED, A STRONG BURNING ELEC
- [SDR DXTA2014060505793](https://openairdocs.org/sdr/DXTA2014060505793), Jun 4, 2014: BRAKE ASSY. WORN. BRAKES CHATTER AT SLOW SPEED COMING TO A COMPLETE STOP, FEEL GRABBY DURING TAXI, PULLS TO THE LEFT DURING DECELERATION. INSPECTED BRAKES, FOUND NR 2 BRAKE LEFT 
- [SDR CWQR20131031048](https://openairdocs.org/sdr/CWQR20131031048), Oct 31, 2013: SOLENOID. BINDING. ACFT LANDED, AFTER ENGINES WERE SHUTDOWN, CREW WAS UNABLE TO OPEN CABIN DOOR. LINE CREW AND TECHNICIANS WERE NOT ABLE TO OPEN THE DOOR FROM THE OUTSIDE HANDLE. 
- [SDR 2013FA0000512](https://openairdocs.org/sdr/2013FA0000512), Sep 12, 2013: ACTUATOR. MALFUNCTIONED. THE AILERON TRIM ACTUATOR WAS INSTALLED ON THE RT AILERON. AFTER THE INSTALLATION, IT WAS FOUND THAT THE COCKPIT EICAS DISPLAY SHOWED THE INDICATOR MOVING IN TH
- [SDR DXTA2011120104807](https://openairdocs.org/sdr/DXTA2011120104807), Nov 30, 2011: DISPLAY. FAILED. NR 1MCDU SCREEN GOES BLANK FOLLOWED BY ELECTRICAL SMOKE EMINATING WITHIN THE COCKPIT. AFTER POWER UP WITH AVIONICS ON, FLIGHT PLAN PROGRAMMED AND READY TO GO. N
- [SDR DXTA2011031604509](https://openairdocs.org/sdr/DXTA2011031604509), Mar 15, 2011: DISPLAY. FAILED. DURING CRUISE FLIGHT, DU NR 2 WENT BLACK ACCOMPANIED BY A SMALL AMOUNT OF ELECTRICAL SMOKE AND ODOR. WHILE ACCOMPLISHING THE ELECTRICAL SMOKE OR FIRE CHECKLIST,
- [SDR DXTA2010072604174](https://openairdocs.org/sdr/DXTA2010072604174), Jul 24, 2010: ANTI-SKID SYS. FAILED. ANTI-SKID FAILED ON TAKEOFF ROLL AT 45 KTS. ABORTED TAKEOFF, MESSAGE REMAINED ON UNTIL SPEED DROPPED BELOW 45 KTS. POWERED ACFT, NO ANTI-SKID FAIL. SPUN EACH WH
- [SDR DXTA2010062804133](https://openairdocs.org/sdr/DXTA2010062804133), Jun 25, 2010: UNKNOWN. ODOR. CREW REPORTED PUNGENT ODOR IN COCKPIT DURING PREFLIGHT. ODOR DISSIPATED QUICKLY AFTER APU BLEED AIR WAS SELECTED ON. REMOVED ALL FOUR DISPLAY UNITS, INSPECTED D
- [SDR DXTA2010010703932](https://openairdocs.org/sdr/DXTA2010010703932), Jan 6, 2010: STRUT. LEAKING. UPON LANDING GEAR RETRACTION, NOSE GEAR MADE HEAVY BANGING NOISE REPEATEDLY IN WHEEL WELL AND RED NOSE GEAR UNLOCK LIGHT REMAINED ON. EXTENDED GEAR NORMALLY AND
- [SDR 2009F00108](https://openairdocs.org/sdr/2009F00108), Nov 13, 2009: WARNING LIGHT. ILLUMINATED. RED CAS MESSAGE "CABIN ALTITUDE" CAME ON PASSING THRU 13,500 FT. PRESS CONTROL FAULT LIGHT WAS ON AS WELL AS CABIN DUMP SWITCH IN DUMP.
- [SDR 2008FA0000771](https://openairdocs.org/sdr/2008FA0000771), Oct 26, 2008: RUDDER PEDAL. JAMMED. ON ACFT DEPARTURE, THE RUDDER PEDALS JAMMED ON THE COCKPIT SIDE PANELS ON THE TAKEOFF. AN EMERGENCY WAS DECLARED AND THE ACFT LANDED UNEVENTFULLY. DURING THE PR

All 54: https://openairdocs.org/deregistered/N370QS-2025-07-28/reports.md

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20140719012999I](https://openairdocs.org/incident/20140719012999I), Jul 19, 2014: Cessna 680 (N370QS), Santa Ana, CA, No damage. 20 Minutes after take off and cruising at 15000 feet the APU was started and a strong electrical burning smell was noted. The bleed air was turned off and APU…

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