# N397QS: 2007 Cessna 680, registration cancelled 2026-07-21 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 21, 2026 - 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: 680-0144 - Year built: 2007 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: May 25, 2007 - Certificate issued: October 16, 2019 - Last registry action: September 9, 2023 - Mode S code: A49E39 - Owner type: Corporation - The mark today: https://openairdocs.org/aircraft/N397QS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=397QS - Page: https://openairdocs.org/deregistered/N397QS-2026-07-21 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 (43) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 2026FA0000015](https://openairdocs.org/sdr/2026FA0000015), Jan 9, 2026: SPAR CAP. CORRODED. CORROSION, RH HORIZONTAL STABILIZER, AFT SPAR UPPER CAP AND LOWER SKIN, APPROX. HSS 86.00 AND HSS 156.80 - [SDR DXTA2025092305039](https://openairdocs.org/sdr/DXTA2025092305039), Sep 21, 2025: DOOR. VIBRATION. MAIN CABIN DOOR ACOUSTIC SEAL GENERATES LOUD, HARMONIC VIBRATION WHEN DOOR IS OPERATED --PARTICULARLY WHEN IT IS BEING OPENED. THE DOOR JETTISONED OUTWARD UNDER - [SDR DXTA2025091204907](https://openairdocs.org/sdr/DXTA2025091204907), Sep 10, 2025: ELEC CONNECTOR. DAMAGED. DURING PREFLIGHT IT WAS DISCOVERED THAT THE EMERGENCY LIGHTING SYSTEM IS INOPERATIVE. CORRECTIVE ACTION: DURING INITIAL INSPECTION AND OPERATION OF THE EMERGENC - [SDR 3J7R2025061400001](https://openairdocs.org/sdr/3J7R2025061400001), Jun 14, 2025: LIGHT. DIM. EXTERIOR EMERGENCY EXIT LIGHT NEAR MAIN CABIN DOOR VERY DIM. ALSO DIM WHEN BEING USED AS PAX SAFETY LIGHT. - [SDR 2024FA0000690](https://openairdocs.org/sdr/2024FA0000690), Sep 5, 2024: SKIN. CORRODED. REMOVED CORROSION ON THE WING SKINS AT THE FOUR AILERON SECTOR BUTTON PLUGS LH AND RH WING LOWER SURFACE, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLE - [SDR DXTA2024090500689](https://openairdocs.org/sdr/DXTA2024090500689), Sep 5, 2024: SKIN. CORRODED. REMOVED 2 AREAS OF CORROSION ON TOP SIDE OF LH HORIZONTAL STAB UPPER SKIN, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, PRIMED AND TOPCA - [SDR 3J7R2024082600001](https://openairdocs.org/sdr/3J7R2024082600001), Aug 25, 2024: LIGHT. DIM. CABIN DOOR EMERGENCY EXIT LIGHT DIM - [SDR DXTA2023111310038](https://openairdocs.org/sdr/DXTA2023111310038), Nov 12, 2023: UNKNOWN. UNKNOWN. SPADE DOOR SEPARATED FROM ATTACH RODS PASSING 2,500 FEET ON DEPARTURE. MAINTAINED 140KTS TO REDUCE VIBRATIONS ON THE RETURN. REMOVED AND REPLACE PUSHROD. ACCOMP - [SDR JGVR20230913002](https://openairdocs.org/sdr/JGVR20230913002), Sep 13, 2023: UNKNOWN. UNKNOWN. REPAIRED CORRODED AREAS OF THE UPPER INBOARD SKINS OF THE LH & RH WINGS ALONG AND UNDERNEATH THE DRAG ANGLES (WING-TO-FUSELAGE FAIRING ATTACH ANGLES) BY R&R THE - [SDR JGVR20230913001](https://openairdocs.org/sdr/JGVR20230913001), Sep 13, 2023: UNKNOWN. UNKNOWN. REPAIRED CORRODED AREAS OF THE VERTICAL STABILIZER AFT SPAR CAPS BY MECHANICALLY BLENDING PERFORMING NDT AND REPORTING FOR REPAIR DISPOSITION. CLEANED TREATED A - [SDR JGVR20230714004](https://openairdocs.org/sdr/JGVR20230714004), Jul 14, 2023: UNKNOWN. UNKNOWN. BLENDED SEVERAL CORRODED AREAS ON LH AND RH WING UPPER SKINS AT THE AT THE AILERON BELLCRANK ACCESS BUTTON PLUGS, PERFORMED NDT AND REPORTED RESULTS FOR REPAIR - [SDR JGVR20230714003](https://openairdocs.org/sdr/JGVR20230714003), Jul 14, 2023: UNKNOWN. UNKNOWN. BLENDED SEVERAL CORRODED AREAS ON THE RH SIDE OF THE VERTICAL STABILIZER JUST UNDER THE TIP CAP, PERFORMED NDT AND REPORTED RESULTS FOR REPAIR DISPOSITION. TREA - [SDR JGVR20230714002](https://openairdocs.org/sdr/JGVR20230714002), Jul 14, 2023: UNKNOWN. UNKNOWN. BLENDED SEVERAL CORRODED AREAS ON THE LOWER SKIN TRAILING EDGE OF THE RH HORIZONTAL STABILIZER, PERFORMED NDT AND REPORTED RESULTS FOR REPAIR DISPOSITION. TREAT - [SDR JGVR20230714001](https://openairdocs.org/sdr/JGVR20230714001), Jul 14, 2023: UNKNOWN. UNKNOWN. BLENDED CORRODED AREAS LOCATED ON THE UPPER AND LOWER SKINS OF THE LH & RH HORIZONTAL STABILIZERS LOCATED NEAR THE HORIZONTAL STABILIZER “PIE FAIRINGS” (ACCESS - [SDR 2023FA0000100](https://openairdocs.org/sdr/2023FA0000100), Feb 18, 2023: SPAR. CORRODED. CORROSION - EXFOLIATION FOUND ON THE WING AFT SPAR IN THE LH AND RH MLG WHEEL WELLS - [SDR DXTA2022101972380](https://openairdocs.org/sdr/DXTA2022101972380), Oct 18, 2022: FUSE. FAILED. CABIN EMERG LIGHT: FOLLOWING POWER ON CHECLIST , STEP 5 EMER LTS - ARM, NONE OF THE EMERGENCY LIGHTS COME ON. THEY DO TURN ON WITH SWITCH IN ON POSSITION (YES, - [SDR DXTA2022092170810](https://openairdocs.org/sdr/DXTA2022092170810), Sep 20, 2022: NONE. NONE. CABIN EMERG LIGHT: EMERGENCY LIGHTS DO NOT COME ON WITH THE PAX SAFETY ON OR WITH THE EMERGENCY LIGHTS IN ARM POSITION WITH NO DC POWER APPLIED. WITH THE EMERGE - [SDR DXTA2022091370340](https://openairdocs.org/sdr/DXTA2022091370340), Sep 13, 2022: NONE. NONE. EMERGENCY LIGHTING: WHEN BATTERY SWITCHES ARE OFF AND EMER LIGHT SWITCH IS ON, THE GALLEY LIGHT, THE LIGHT BETWEEN SEATS 1 AND 3, LIGHT BETWEEN SESTS 5 AND 7, A - [SDR DXTA2022050961500](https://openairdocs.org/sdr/DXTA2022050961500), May 8, 2022: WIRE. DAMAGED. DC EMER BUS R AMBER CAS: IN FLIGHT DC EMER BUS R DC GEN OFF R DU 4 OFF DU 3 RED X'S FMS 2 INITIALLY TRIED TO USE DC GEN OFF R QRH THE BUS TIE WOULD NOT CLOSE. C - [SDR DXTA2021051041760](https://openairdocs.org/sdr/DXTA2021051041760), May 7, 2021: CONTROL VALVE. DEFECTIVE. COCKPIT ODOR: DESCENDING THROUGH 5000 FEET WITH THE APU OFF, WE STARTED TO FEEL LIKE BURNED OIL ODOR IN THE COCKPIT, NO SMOKE ASSOCIATED WITH IT. SIGNOFF. INSPE - [SDR DXTA2021011904622](https://openairdocs.org/sdr/DXTA2021011904622), Jan 19, 2021: SPRING. DEFECTIVE. TECH HEARD NOISE WHEN HE OPENED MED, NOTICED COUNTER BALANCE CABLE LOOSE. REMOVED AND REPLACED MED AFT COUNTERBALANCE SPRING P/N: S3194-6, IAW CE680 AMM, 52-10- - [SDR JGVR20200819001](https://openairdocs.org/sdr/JGVR20200819001), Aug 7, 2020: SPAR. CORRODED. BLENDED AREA OF CORROSION ON RT SIDE OF VERTICAL STABILIZER AFT SPAR AT VFS 118.79. PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED AND TREATED BLEND - [SDR DXTA2020030203531](https://openairdocs.org/sdr/DXTA2020030203531), Mar 2, 2020: SQUAT SWITCH. DEFECTIVE. LANDING GEAR HANDLE STUCK - REPEAT WRITE-UP: GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION AFTER TAKEOFF. GEAR REMAINED DOWN AND LOCKED (3 GREEN) WOW MISCOMPARE - [SDR JGVR20200150001](https://openairdocs.org/sdr/JGVR20200150001), Jan 15, 2020: SPAR. CORRODED. 6 SPOTS OF CORROSION ON THE VERTICAL STAB AFT SPAR. - [SDR 2019F00148](https://openairdocs.org/sdr/2019F00148), Mar 11, 2019: DOUBLER. CHAFED. GOUGES, AFT CABIN ESCAPE HATCH SURROUND, 6911166-2, DOUBLER AND 6911121-5 UPPER FRAME SEGMENT, MULTIPLE LOCATIONS. ACCOMPLISHED FIELD REPAIR FR-680-0144-5312, R - [SDR 2019F00143](https://openairdocs.org/sdr/2019F00143), Mar 7, 2019: SPAR CAP. CORRODED. CORROSION, RT WING, SPAR CAP AND WEB, BETWEEN WS 37 AND WS 52. ACCOMPLISHED ENGINEERING FIELD REPAIR FR-680-0144-5291 REV- FAA FORM 8100-9 DATED 3/01/2019; FIEL - [SDR 2019F00142](https://openairdocs.org/sdr/2019F00142), Mar 7, 2019: GUSSET. CHAFED. LEFT AND RIGHT GUSSETS ABOVE COCKPIT SIDE WINDOW DAMAGE (CHAFE MARKS). ACCOMPLISHED LETTER DQ18665M1 DATED MARCH 6, 2019; 680-0144 LEFT AND RIGHT GUSSETS ABOVE - [SDR 2019F00136](https://openairdocs.org/sdr/2019F00136), Feb 28, 2019: TRUSS FITTING. CORRODED. APU TRUSS MOUNT (FLANGE) CORROSION. ACCOMPLISHED ENGINEERING LETTER DQ18604M1 DATED FEB. 26, 2019; 680-0144 (N397QS) APU TRUSS MOUNT (FLANGE) CORROSION. - [SDR DXTA2018100801515](https://openairdocs.org/sdr/DXTA2018100801515), Oct 7, 2018: SQUAT SWITCH. OUT OF RIG. ALL LANDING GEAR RETRACTION DID NOT RETRACT - AFTER LIFTOFF GEAR HANDLE MOVED TO RETRACT POSITION. GEAR DID NOT RETRACT. INDICATORS HAD 3 GREEN AND ONE RED UNLO - [SDR 2018FA0000389](https://openairdocs.org/sdr/2018FA0000389), Sep 26, 2018: CHANNEL. CORRODED. REPAIRED CORRODED AREA ON THE NOSE WHEEL WELL FORWARD CHANNEL P/N 6731051-57 LOWER FLANGE, JUST FORWARD OF THE NLG UPLOCK, BY BLENDING, PERFORMING EDDY CURRENT - [SDR 2018F00126](https://openairdocs.org/sdr/2018F00126), Sep 26, 2018: ANGLE. CORRODED. FOUND THE LT WING AFT SPAR LOWER CAP FORWARD ANGLE CORRODED AT WS 30.36 AND WS 41.54, AND CENTER SPAR WEB CORRODED JUST IB OF THE TRUNNION SUPPORT AT WS 56.36. - [SDR JGVR20180621003](https://openairdocs.org/sdr/JGVR20180621003), Jun 21, 2018: SKIN. CORRODED. CORROSION FOUND ON THE OUTBOARD EDGE AND UNDERNEATH THE RT WING UPPER AFT DRAG ANGLE, WING TO FUSELAGE FAIRING. BLENDED THE CORROSION, PERFORMED AN EDDY CURRENT - [SDR JGVR20180621002](https://openairdocs.org/sdr/JGVR20180621002), Jun 21, 2018: SKIN. CORRODED. REMOVED AIRCRAFT DATA TAG AND MECHANICALLY BLENDED CORROSION ON AIRCRAFT SKIN. PERFORMED EDDY CURRENT AND ULTRASONIC INSPECTIONS AND REPORTED RESULTS TO ENGINEE - [SDR JGVR20180621001](https://openairdocs.org/sdr/JGVR20180621001), Jun 21, 2018: SKIN. CORRODED. REMOVED AIRCRAFT DATA TAG AND MECHANICALLY BLENDED CORROSION ON AIRCRAFT SKIN. PERFORMED EDDY CURRENT AND ULTRASONIC INSPECTIONS AND REPORTED RESULTS TO ENGINEE - [SDR DXTA2014070705812](https://openairdocs.org/sdr/DXTA2014070705812), Jul 6, 2014: BRAKE ASSY. DIRTY. AFTER A LANDING CYCLE, BRAKES SHUDDER & GRAB WHEN STOPPING ACFT. THIS OCCURS UNDER 3 KTS TO PARK. ACCOMPLISHED BRAKE BLEEDING PROCEDURE IAW MM 32-42-10. CLEANED - [SDR DXTA2014012805627](https://openairdocs.org/sdr/DXTA2014012805627), Jan 27, 2014: WARNING SYSTEM. ACTIVATED. AFTER TAKEOFF NOSE GEAR RED LIGHT REMAINED ILLUMINATED. - [SDR DXTA2013080505468](https://openairdocs.org/sdr/DXTA2013080505468), Aug 4, 2013: ACM. FAILED. WITH ENGINES AND APU RUNNING, AFTER START UP COULD NOT GET TEMPERATURE UNDER CONTROL. WENT TO MANUAL AND STILL COULDN'T CONTROL IT. HAD A STRONG BURNING ELECTRI - [SDR DXTA2013080105462](https://openairdocs.org/sdr/DXTA2013080105462), Jul 31, 2013: LANDING GEAR. MALFUNCTIONED. AFTER TAKEOFF, THE GEAR HANDLE WOULD NOT COME UP. - [SDR CWQR20130528034](https://openairdocs.org/sdr/CWQR20130528034), May 28, 2013: TUBE. CRACKED. DURING A SCHEDULED INSPECTION, FOUND THIS TUBE ASSEMBLY, CRACKED 50 PERCENT AROUND THE FIREWALL BULKHEAD ATTACH FLANGE. CRACK WAS FOUND RIGHT ON THE EDGE OF THE - [SDR DXTA2012101505145](https://openairdocs.org/sdr/DXTA2012101505145), Oct 14, 2012: COALESCER BAG. ODOR. AFTER TAKEOFF, AT ALTITTUDE OF 20,000 MSL BOTH PILOTS OBSERVED SMOKE & FUMES IN THE ACFT. BOTH BLEEDS WERE TURNED OFF AND SMOKE SUBSIDED, AFTER LANDING ACFT TOW - [SDR DXTA2011080204682](https://openairdocs.org/sdr/DXTA2011080204682), Aug 1, 2011: WHEEL. WORN. ABNORMAL GEAR RETRACTION, GEAR UNSAFE LIGHT REMAINED ON FOR APPROX 7-10 SECONDS AFTER ALL GEAR INDICATED UP. HEARD NOSE WHEEL SPINNING ABNORMALLY LONG IN NOSE C - [SDR 2011FA0000134](https://openairdocs.org/sdr/2011FA0000134), Feb 9, 2011: CONNECTOR. DAMAGED. DURING FUEL TANK INSPECTIONS, FINDING ELECTRICAL BLANKING PINS IN WING ROOT OF FUEL TANKS. PINS FALLING OUT OF PLUGS PREVIOUSLY INSTALLED DURING ACFT MFG. - [SDR DXTA2009062503702](https://openairdocs.org/sdr/DXTA2009062503702), Jun 25, 2009: STRUT. DISCHARGED. DURING GEAR RETRACTION, NUMEROUS LOUD BANGING NOISES WERE HEARD FROM THE NOSE GEAR. SOUND AND BUMPS FELT IN THE FLOOR CONTINUED FOR 5 -10 SEC UNTIL THE NOSE GEA ## Other aircraft with N397QS - [Cancelled 2002-11-20](https://openairdocs.org/deregistered/N397QS-2002-11-20): Cessna 560, S/N 560-0531, built 1999. Owner: [Netjets Sales Inc](https://openairdocs.org/faa-owner/NETJETS%20SALES%20INC), [Oklahoma City, OK](https://openairdocs.org/faa-place/OK/Oklahoma%20City) --- 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.