# N375QS: 2008 Cessna 680, registration cancelled 2025-01-22 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: January 22, 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: 680-0230 - Year built: 2008 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 24, 2008 - Certificate issued: January 2, 2019 - Last registry action: July 7, 2023 - Mode S code: A447CD - 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/N375QS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=375QS - Page: https://openairdocs.org/deregistered/N375QS-2025-01-22 From the FAA registry file of October 31, 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 (34) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 2024FA0000579](https://openairdocs.org/sdr/2024FA0000579), Aug 7, 2024: SKIN. CORRODED. BLENDED CORRODED AREA ON THE LH SKIN ON THE RUDDER NEAR THE REPAIRED LEVEL 2 CORROSION FOUND ON LH SIDE OF RUDDER, JUST AFT OF THE RUDDER TRIM ACTUATOR CUTOUT, - [SDR DXTA2024030111048](https://openairdocs.org/sdr/DXTA2024030111048), Feb 29, 2024: POWER SUPPLY. FAILED. EMERG EXIT SIGN/LIGHT: EMERGENCY EXIT LIGHTS AT THE CABIN ENTRY DO NOT WORK AS WELL AS THE LEFT EXTERIOR EMERGENCY LIGHT. DID 2-30 MINUTE CHARGES WITH THE GPU W - [SDR DXTA2024012510723](https://openairdocs.org/sdr/DXTA2024012510723), Jan 24, 2024: BATTERY. FAULTED. SEVERAL INTERIOR EMERGENCY LIGHTS AND THE LEFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. ARRIVED AT AC. POWERED ON EMERGENCY BAIT SWITCH, CONFIRMED DISCREPANCY AND - [SDR DXTA2023091194970](https://openairdocs.org/sdr/DXTA2023091194970), Sep 9, 2023: BATTERY. DEFECTIVE. WHEN EMERGENCY LIGHTS ARE PLACED IN ARMED POSITION EMERGENCY EXIT LIGHTED SIGNS BEHIND SEAT 9, AND ABOVE LAVATORY SEAT DO NOT ILLUMINATE AS WELL AS SEAT LIGHT O - [SDR EBVR20230623450](https://openairdocs.org/sdr/EBVR20230623450), Jun 23, 2023: UNKNOWN. UNKNOWN. CORROSION FOUND ON THE SKIN AROUND THE EMERGENCY EXIT DOOR ON R/H SIDE OF FUSELAGE. BLENDED SIGNS OF CORROSION FROM 2 SPOTS ON THE E-EXIT OUTER SKIN. REMAINING - [SDR DXTA2023022381040](https://openairdocs.org/sdr/DXTA2023022381040), Feb 22, 2023: UNKNOWN. UNKNOWN. NLG LANDING GEAR RETRACTION: REPEAT WRITEUP. AFTER GEAR RETRACTION RED UNLOCK LIGHT REMAINED ILLUMINATED. COMPLIED WITH QRH UNLOCK ON RETRACTION, EXTENSION NORM - [SDR DXTA2022121275960](https://openairdocs.org/sdr/DXTA2022121275960), Dec 10, 2022: LIGHT. DEFECTIVE. EMERGENCY LIGHTING: L H EMER LIGHT NOT ILLUMINATED // SIGNOFF // TURNED ON EMERGENCY LIGHTING, FOUND ALL EMERGENCY LIGHTING TO BE OPS ILLUMINATING SATISFACTORY, - [SDR DXTA2022101972370](https://openairdocs.org/sdr/DXTA2022101972370), Oct 18, 2022: ACTUATOR. DEFECTIVE. AFTER CLIMBING THROUGH 10000 FT AND ACCELERATING TOWARDS 300 KIAS, THE A AUTOPILOT FAILED AND WE EXPERIENCED A NOSE UP PITCH MOTION. THE PF WAS UNABLE TO TRIM N - [SDR DXTA2021082547550](https://openairdocs.org/sdr/DXTA2021082547550), Aug 23, 2021: RELAY. ABNORMAL. EMERGENCY LIGHTING: EMERGENCY LIGHTING OFF FUNCTION INOP. UNABLE TO EXTINGUISH INTERIOR OR EXTERIOR EMERGENCY LIGHTING THROUGH NORMAL SWITCH FUNCTIONS. LIGHTS R - [SDR JGVR20201120005](https://openairdocs.org/sdr/JGVR20201120005), Nov 20, 2020: SKIN. CORRODED. MECHANICALLY REMOVED 12 AREAS OF CORROSION LOCATED AT LT UPPER WING FWD, MIDDLE AND AFT DRAG ANGLES. REPAIRED CORROSION BLENDS, IAW TEXTRON ENGINEERING STANDARD - [SDR JGVR20201120004](https://openairdocs.org/sdr/JGVR20201120004), Nov 20, 2020: DRAG ANGLE. DAMAGED. REPAIRED BLENDED AREAS ON LT AND RT WING INBOARD SKINS NEXT TO FORWARD DRAG ANGLES, PER TEXTRON FIELD REPAIR, FR-680-0230-8540 REV-. TITLED: FIELD REPAIR-CORROS - [SDR JGVR20201120003](https://openairdocs.org/sdr/JGVR20201120003), Nov 20, 2020: SKIN. CORRODED. FOUND 17 AREAS OF VERIFIED CORROSION ALONG FUSELAGE AFT CHIN FAIRING. FOUND ADDITIONAL 120 AREAS OF CORROSION UNDER AFT CHIN FAIRING. REPAIRED BLENDED AREAS OF - [SDR JGVR20201120002](https://openairdocs.org/sdr/JGVR20201120002), Nov 20, 2020: SKIN. CORRODED. RT LOWER WING SKIN IN GEAR WELL HAS VERIFIED CORROSION UNDER 7 FASTENERS. PERFORM TEXTRON MINOR REPAIR MEMO DQ27295M1 DATED: OCT 9, 2020 FOR RT LOWER CENTER WIN - [SDR JGVR20201120001](https://openairdocs.org/sdr/JGVR20201120001), Nov 20, 2020: SKIN. CORRODED. FOUND 11 AREAS OF VERIFIED CORROSION ON E-EXIT OUTER SKIN. FOUND DURING TASK 52-20-00-2202 FOUND 4 ADDITIONAL SPOTS OF VERIFIED CORROSION UNDERNEATH CONTOUR RIN - [SDR JGVR20201113002](https://openairdocs.org/sdr/JGVR20201113002), Nov 13, 2020: DOOR FRAME. CHAFED. REPAIRED CHAFED E-EXIT SURROUND WEB AND FRAME AT APPROXIMATELY FS 400 PER AEROSPACE QRD ERO-967189 REV IR, TITLED "E-EXIT SURROUND WEB AND FRAME REPAIR" DATED O - [SDR JGVR20201113001](https://openairdocs.org/sdr/JGVR20201113001), Nov 13, 2020: STRUCTURE. CORRODED. REPAIRED SEVERAL AREAS OF CORROSION ON FUSELAGE DROP AISLE STRUCTURE BETWEEN FS 165 AND FS 426 PER AEROSPACE QRD ERO-967178 REV IR DATED NOVEMBER 09, 2020 AND S - [SDR JGVR202001112001](https://openairdocs.org/sdr/JGVR202001112001), Nov 12, 2020: SPAR. CORRODED. VERTICAL STAB AFT SPAR LT UPPER ANGLE HAS 2 AREAS OF VERIFIED INTERGRANULAR CORROSION. MECHANICALLY BLENDED CORROSION ON VERTICAL STAB AFT SPAR RT UPPER ANGLE, - [SDR DXTA2019093002907](https://openairdocs.org/sdr/DXTA2019093002907), Sep 29, 2019: DOWNLOCK SWITCH. MALFUNCTIONED. RIGHT MLG LANDING GEAR EXTENSION DID NOT EXTEND - UPON GEAR DOWN SELECTION 6 MILE FINAL 28R SFO RIGHT MAIN GEAR DID NOT LOCK (NO GREEN). ADVISED TOWER TO EXECUT - [SDR DXTR2017121800648](https://openairdocs.org/sdr/DXTR2017121800648), Dec 18, 2017: TEE FITTING. CORRODED. MAIN CABIN DOOR SPADE DOOR HINGE ATTACH NUTPLATES CORRODED. MEMO 10436M2 DATED DECEMBER 14, 2017. - [SDR 2018F00053](https://openairdocs.org/sdr/2018F00053), Dec 13, 2017: NONE. NONE. REPAIR OF OVERSIZED DOOR ROD PIN HOLE IN RIGHT MAIN LANDING GEAR TRUNNION. REPORT NO. S-680-0230/02RD DATED DECEMBER 6, 2017 WITH FAA FORM 8100-9 DATED DECEMBER - [SDR 2018F00052](https://openairdocs.org/sdr/2018F00052), Dec 13, 2017: NONE. NONE. REPAIR OF DRILL STARTS IN RIGHT WING LEADING EDGE SKIN. REPORT NO. S-680-0230/03RD DATED DECEMBER 6, 2017 WITH FAA FORM 8100-9 DATED DECEMBER 7, 2017. - [SDR 2018F00051](https://openairdocs.org/sdr/2018F00051), Dec 13, 2017: NONE. NONE. MAIN CABIN DOOR SPADE DOOR HINGE ATTACH NUT-PLATES. MEMO 10436M1 DATED DECEMBER 7, 2017. - [SDR DXTA2017041606397](https://openairdocs.org/sdr/DXTA2017041606397), Apr 16, 2017: SENSOR. MALFUNCTIONED. LEFT ENGINE OIL TEMP IN RED IN THE CLIMB PASSING 14,000 FT. HIGHEST NOTED TEMP WAS 144 DEGREES. UPON POWER REDUCTION, OIL TEMP RETURNED TO GREEN AND REDUCED SET - [SDR 2016F00206](https://openairdocs.org/sdr/2016F00206), Oct 25, 2016: SPAR CAP. CORRODED. CORROSION ON VERTICAL STABILIZER AFT SPAR CAP. - [SDR DXTA2016010406152](https://openairdocs.org/sdr/DXTA2016010406152), Jan 3, 2016: MONITOR. FAILED. TV MONITOR AT SEAT 7 BEGAN SMOKING & HAS A SPOT WHERE PLASTIC ON BACK OF MONITOR STARTED TO MELT. FOUND BURN HOLE IN BACK OF MONITOR HOUSING. REMOVED MONITOR. I - [SDR DXTA2015092206088](https://openairdocs.org/sdr/DXTA2015092206088), Sep 21, 2015: CONDENSER. FAILED. BLUE SMOKE & OIL ODOR FROM OVERHEAD WEMAC VENTS. COMPLIED WITH TASK CARD ECS DUCT BURN OUT, FORM TC-680-21-120905M. REMOVED CONDENSER FROM WATER SEPARATOR. REMO - [SDR DXTA2014090905877](https://openairdocs.org/sdr/DXTA2014090905877), Sep 8, 2014: DRAIN LINE. OBSTRUCTED. IN CRUISE CREW NOTICED ENVIRONMENTAL SYS ODOR & SMOKE IN CABIN. ACCOMPLISHED ABNORMAL PROCEDURE, SMOKE APPEARED TO DECREASE WHEN PRESS SOURCE SELECTOR WAS IN RI - [SDR DXTA2011021704469](https://openairdocs.org/sdr/DXTA2011021704469), Feb 16, 2011: STRUT. DISCHARGED. AFTER TAKEOFF "WOW MISCOMPARE" ILLUMINATED AND GEAR WOULD NOT RETRACT. FOUND NLG STRUT UPPER CHAMBER 10PSI LOW AND LOWER CAMBER AT OPSI. PERFORMED NLG STRUT SER - [SDR DXTA2010070204138](https://openairdocs.org/sdr/DXTA2010070204138), Jul 1, 2010: DUCT. LEAKING. SUPPLY BLEED LEAK R, CASS MESSAGE. RAN ABNORMAL CHECKLIST AND CASS MESSAGE CAME BACK ON AFTER SYSTEM RESET. R & R RT PRECOOLER UPPER DUCT ASSY AND LOWER DUCT SE - [SDR DXTA2008122903449](https://openairdocs.org/sdr/DXTA2008122903449), Dec 28, 2008: UNKNOWN. ODOR. DESCENDING THROUGH 18000 FT, ACM O' TEMP AND EMER PRESS ANNUNCIATORS ILLUMINATED. AFTER 15 SECONDS, BOTH CLEARED. CABIN HAD SMALL AMOUNT OF SMOKE AND CLEARED AS - [SDR DXTA2008122803448](https://openairdocs.org/sdr/DXTA2008122803448), Dec 28, 2008: UNKNOWN. ODOR. DESCENDING THROUGH 18000 FT, ACM OVERTEMP AND EMER PRESS ANNUNCIATORS ILLUMINATED. AFTER 15 SECONDS, BOTH CLEARED. CABIN HAD SMALL AMOUNT OF SMOKE AND CLEARED A - [SDR DXTA2008122903448](https://openairdocs.org/sdr/DXTA2008122903448), Dec 28, 2008: WARNING LIGHT. ILLUMINATED. ACM OVERTEMP AND EMERGENCY PRESSURE ANNUNCIATORS ILLUMINATED. SMALL AMOUNT OF SMOKE IN CABIN. - [SDR DXTA20082870](https://openairdocs.org/sdr/DXTA20082870), Feb 12, 2008: LANDING GEAR. MALFUNCTIONED. UPON RETRACTION OF LANDING GEAR, GEAR UNSAFE LIGHT ILLUMINATED. JACKED AND SWUNG GEAR TEN TIMES WITH NO FAULTS. LUBED ALL UP LOCK ROLLERS AND GEAR. OPS CHECKED - [SDR DXTA200802810](https://openairdocs.org/sdr/DXTA200802810), Jan 30, 2008: HOSE. LEAKING. DURING TOUCHDOWN AT PDK, COPILOT'S LT BRAKE PEDAL WENT COMPLETELY TO THE FLOOR. REMOVED AND REPLACED BOTH CO-PILOTS UPPER MASTER CYLINDER HOSES. IAW MM CHAP 32- --- 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.