# N380QS: 2006 Cessna 680, registration cancelled 2026-02-10

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 10, 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: 680-0089
- Year built: 2006
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 26, 2006
- Certificate issued: May 5, 2020
- Last registry action: January 22, 2023
- Mode S code: A45CB9
- 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/N380QS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=380QS
- Page: https://openairdocs.org/deregistered/N380QS-2026-02-10

From the FAA registry file of November 7, 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 (53, newest 50)

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

- [SDR 2025F00128](https://openairdocs.org/sdr/2025F00128), May 20, 2025: SPAR CAP. CORRODED. EXFOLIATION CORROSION ON LH AFT SPAR LOWER CAP BEHIND PANEL 720DL. MECHANICALLY REMOVED AREA OF CORROSION FROM LH WING AFT SPAR IAW C680 SRM 51-70-02. FOUND COR
- [SDR 2025F00129](https://openairdocs.org/sdr/2025F00129), May 20, 2025: FITTING. CORRODED. RH MLG WS 37.00 SUPPORT BEAM IN GEARWELL, FWD AREAS, HAVE HYD LINE CARRY THRU FITTINGS WITH CORROSION AROUND THEM. MECHANICALLY BLENDED CORROSION IN ACCORDANCE 
- [SDR DXTA2025040202907](https://openairdocs.org/sdr/DXTA2025040202907), Apr 1, 2025: WARNING MESSAGE. ILLUMINATED. BLEED AIR O'TEMP R AMBER CAS: ON THE PRIOR FLIGHT BLEED AIR OVER TEMP RIGHT AMBER CAST ILLUMINATED. COMPLIED WITH CHECKLIST AND TURNED OFF RIGHT SIDE PRESSURE F
- [SDR DXTA2025013002121](https://openairdocs.org/sdr/DXTA2025013002121), Jan 26, 2025: ACTUATOR. FAULTED. FLAP: AFTER TAKEOFF WHEN BRINGING FLAPS FROM 7 TO 0, WE GOT A FLAPS FAIL, WE RAN ALL THE CHECKLIST AND DID AN EMERGENCY RETURN. CORRECTIVE ACTION: REPLACED FLAP
- [SDR DXTA2024112501227](https://openairdocs.org/sdr/DXTA2024112501227), Nov 21, 2024: G SWITCH. DAMAGED. EMERGENCY LIGHTING: REPEAT WRITE UP. EMERGENCY LIGHTING: WITH EMER LTS SWITCH IN THE OFF POSITION, THE FOLLOWING LIGHTS REMAINED ILLUMINATED AND COULD NOT BE EX
- [SDR 2024F00172](https://openairdocs.org/sdr/2024F00172), Jul 23, 2024: TORQUE TUBE. CORRODED. DURING RUDDER UPPER TORQUE TUBE DETAILED INSPECTION FOUND CORROSION TO EXTEND BETWEEN 0.1 AND 0.2 INCH FROM THE TORQUE TUBE. REMOVED CORRODED RUDDER TORQUE TUBE
- [SDR 2024FA0000511](https://openairdocs.org/sdr/2024FA0000511), Jul 23, 2024: SPAR. CORRODED. MECHANICALLY REMOVED 2 EA AREAS OF CORROSION ON LH WING AFT SPAR, LOWER CLIP INBD SIDE OF WS 37.00 IAW C680 SRM 51-70-02. EVALUATED AND FOUND BLENDED AREAS TO B
- [SDR DXTA2021102250750](https://openairdocs.org/sdr/DXTA2021102250750), Oct 22, 2021: ECS. CONTAMINATED. WHEN WE STARTED THE BLEED AIR THE AIRPLANE FILLED UP WITH THICK SMOKE. BOTH THE CABIN AND THE COCKPIT. ACCOMPLISHED APU GROUND RUN. VERIFIED OIL SMELL PRESENT I
- [SDR DXTA2020083104036](https://openairdocs.org/sdr/DXTA2020083104036), Aug 31, 2020: SEAL. DAMAGED. LANDING GEAR WOULD NOT RETRACT AFTER TAKE OFF. COMPLIED WITH QRH AND RETURNED FOR LANDING WITH NORMAL PROCEDURES. NO UNSAFE MESSAGES NOTED. THE AMBER WOW MISCOM
- [SDR 2019FA0000200](https://openairdocs.org/sdr/2019FA0000200), Jun 26, 2019: TRUSS. CORRODED. APU TRUSS CORRODED. ACCOMPLISHED REPAIR TO APU TRUSS IAW ENGINEERING MEMO DQ21989RR1
- [SDR 2019F00228](https://openairdocs.org/sdr/2019F00228), Jun 25, 2019: COWLING. CHAFED. LH ENGINE UPPER COWL CHAFE. REFERENCE MANUFACTURER DOCUMENT S-750-ATA51/01RD REV. A. AND ENGINEERING MEMO DQW21934M1
- [SDR JGVR20180711002](https://openairdocs.org/sdr/JGVR20180711002), Jul 11, 2018: FRAME. CORRODED. BLENDED CORRODED AREAS ON UPPER FRAME IN THE NOSE WHEEL WELL AT FS 77 LOCATED UNDER AND AROUND HYDRAULIC FEED THROUGH FITTINGS, PERFORMED EDDY CURRENT AND ULTRA
- [SDR JGVR20180711001](https://openairdocs.org/sdr/JGVR20180711001), Jul 11, 2018: SPAR. CORRODED. BLENDED CORRODED AREA ON THE RT WING CENTER SPAR INBRD WEB FORWARD FACE AT HYDRAULIC LINE FEED THROUGH RWS 40.62, PERFORMED ULTRASONIC AND EDDY CURRENT INSPECTI
- [SDR EBVR201707060001](https://openairdocs.org/sdr/EBVR201707060001), Jul 6, 2017: SKIN. CORRODED. CORROSION NOTED ON THE LT UPPER AND LOWER BUCKETS AS WELL AS THE RT UPPER. ALL AREAS WERE ON THE OUTER SKINS. AREA BLENDED AND NDT PERFORMED CONFIRMING ALL CORR
- [SDR DXTR20170424017](https://openairdocs.org/sdr/DXTR20170424017), Apr 17, 2017: SKIN. CORRODED. LEFT ELEVATOR HAS CORROSION ON UPPER SIDE. REMOVED CORROSION AND POLISHED IAW SRM 51-10-01. ACCOMPLISHED EDDY CURRENT INSPECTION OF THE RT ELEVATOR AFTER BLENDI
- [SDR DXTR20170424016](https://openairdocs.org/sdr/DXTR20170424016), Apr 17, 2017: SKIN. CORRODED. RIGHT UPPER WING AT WS 54 HAS CORROSION. REMOVED PAINT IAW MM 20-31-00. REMOVED CORROSION AND POLISHED IAW SRM 51-10-01. ACCOMPLISHED EDDY CURRENT INSPECTION AF
- [SDR DXTR20170424013](https://openairdocs.org/sdr/DXTR20170424013), Apr 17, 2017: SKIN. CORRODED. LEFT ELEVATOR HAS CORROSION ON BOTTOM SIDE. REMOVED CORROSION AND POLISHED IAW SRM 51-10-01. ACCOMPLISHED EDDY CURRENT INSPECTION OF MULTIPLE AREAS AFTER BLENDI
- [SDR DXTR20170424012](https://openairdocs.org/sdr/DXTR20170424012), Apr 17, 2017: SKIN. CORRODED. PANEL 352AB HAS CORROSION. ACCOMPLISHED EDDY CURRENT INSPECTION OF MULTIPLE AREAS ON PANELS AFTER BLENDING IAW NDI MANUAL PART 6-20-00-02. NO DEFECTS NOTED AT T
- [SDR DXTR20170424011](https://openairdocs.org/sdr/DXTR20170424011), Apr 17, 2017: SKIN. CORRODED. PANEL 352AC HAS CORROSION. ACCOMPLISHED EDDY CURRENT INSPECTION OF MULTIPLE AREAS ON PANELS AFTER BLENDING IAW NDI MANUAL PART 6-20-00-02. NO DEFECTS NOTED AT T
- [SDR DXTR20170424010](https://openairdocs.org/sdr/DXTR20170424010), Apr 17, 2017: SKIN. CORRODED. PANEL 351AC HAS CORROSION. ACCOMPLISHED EDDY CURRENT INSPECTION OF MULTIPLE AREAS ON PANELS AFTER BLENDING IAW CE-680 NDI MANUAL PART 6-20-00-02. NO DEFECTS NOT
- [SDR DXTR2017042406](https://openairdocs.org/sdr/DXTR2017042406), Apr 17, 2017: THRUST REVERSER. CORRODED. LEFT ENGINE THRUST REVERSER HAS CORROSION AT THE 6 O'CLOCK POSITION. ACCOMPLISHED AN EDDY CURRENT INSPECTION IAW NDI MANUAL PART 6-20-00-02. NO DEFECTS NOTED.
- [SDR DXTR2017042405](https://openairdocs.org/sdr/DXTR2017042405), Apr 17, 2017: THRUST REVERSER. CORRODED. LEFT ENGINE THRUST REVERSER HAS CORROSION AT THE 11 O'CLOCK POSITION. ACCOMPLISHED EDDY CURRENT INSPECTION OF MULTIPLE AREAS IAW NDI MANUAL PART 6-20-00-02. NO 
- [SDR DXTR2017042404](https://openairdocs.org/sdr/DXTR2017042404), Apr 17, 2017: THRUST REVERSER. CORRODED. RIGHT ENGINE THRUST REVERSER HAS CORROSION AT THE 9 O'CLOCK POSITION. ACCOMPLISHED EDDY CURRENT INSPECTION OF MULTIPLE AREAS ON THE RT T/R AFTER BLENDING IAW ND
- [SDR DXTR2017042402](https://openairdocs.org/sdr/DXTR2017042402), Apr 17, 2017: THRUST REVERSER. CORRODED. RIGHT ENGINE T/R HAS CORROSION AT THE 2 O'CLOCK POSITION. ACCOMPLISHED EDDY CURRENT INSPECTION OF MULTIPLE AREAS ON THE RT T/R AFTER BLENDING IAW 0 NDI MANUAL P
- [SDR DXTR2017042401](https://openairdocs.org/sdr/DXTR2017042401), Apr 17, 2017: THRUST REVERSER. CORRODED. RIGHT ENGINE THRUST REVERSER HAS CORROSION AT THE 1 O'CLOCK POSITION. ACCOMPLISHED EDDY CURRENT INSPECTION OF MULTIPLE AREAS ON THE RT THRUST REVERSER AFTER BLE
- [SDR DXTR2017042112](https://openairdocs.org/sdr/DXTR2017042112), Apr 17, 2017: TAIL CONE. CORRODED. APU EXHAUST TAIL CONE HAS CORROSION AT ZONE 331. REMOVED THE CORROSION AND POLISHED IAW SRM 51-10-01. ACCOMPLISHED EDDY CURRENT INSPECTION OF MULTIPLE AREAS ON 
- [SDR DXTR2017042111](https://openairdocs.org/sdr/DXTR2017042111), Apr 17, 2017: TAIL CONE. CORRODED. APU EXHAUST TAIL CONE HAS CORROSION . REMOVED CORROSION AND POLISHED IAW SRM 51-10-01. ACCOMPLISHED EDDY CURRENT INSPECTION OF MULTIPLE AREAS ON THE APU TAILCON
- [SDR DXTR2017042110](https://openairdocs.org/sdr/DXTR2017042110), Apr 17, 2017: LATCH. CORRODED. CARGO DOOR UPPER AFT LATCH HAS CORROSION. REMOVED CORROSION AND POLISHED IAW SRM 51-10-01. ACCOMPLISHED EDDY CURRENT INSPECTION.680 NDI MANUAL PART 6-20-00-02. 
- [SDR DXTR2017042109](https://openairdocs.org/sdr/DXTR2017042109), Apr 17, 2017: SKIN. CORRODED. LEFT WING WS 78 IN ZONE 522 HAS CORROSION. REMOVED PAINT IAW MM 20-31-00. REMOVED CORROSION AND POLISHED IAW SRM 51-10-01. ACCOMPLISHED EDDY CURRENT INSPECTION 
- [SDR DXTR2017042108](https://openairdocs.org/sdr/DXTR2017042108), Apr 17, 2017: SKIN. CORRODED. LEFT WING WS 75 IN ZONE 522 HAS CORROSION. REMOVED CORROSION AND POLISHED IAW CE-680 SRM 51-10-01.
- [SDR DXTR2017042107](https://openairdocs.org/sdr/DXTR2017042107), Apr 17, 2017: SKIN. CORRODED. LEFT WING WS 72 HAS CORROSION. REMOVED PAINT IAW MM 20-31-00. REMOVED CORROSION AND POLISHED IAW SRM 51-10-01.ACCOMPLISHED EDDY CURRENT INSPECTION OF MULTIPLE A
- [SDR DXTR2017042106](https://openairdocs.org/sdr/DXTR2017042106), Apr 17, 2017: SKIN. CORRODED. LEFT WING WS 53 HAS CORROSION. REMOVED PAINT IAW MM 20-31-00. ACCOMPLISHED EDDY CURRENT INSPECTION OF MULTIPLE AREAS AFTER BLENDING IAW NDI MANUAL PART 6-20-00-
- [SDR DXTR2017042105](https://openairdocs.org/sdr/DXTR2017042105), Apr 17, 2017: SKIN. CORRODED. LEFT WING WS 49 HAS CORROSION. REMOVED PAINT IAW MM 20-31-00. ACCOMPLISHED EDDY CURRENT INSPECTION OF MULTIPLE AREAS AFTER BLENDING IAW NDI MANUAL PART 6-20-00-
- [SDR DXTR2017042104](https://openairdocs.org/sdr/DXTR2017042104), Apr 17, 2017: SKIN. CORRODED. LEFT WING WS 43 IN ZONE 512 HAS CORROSION. REMOVED PAINT IAW MM 20-31-00. REMOVED CORROSION AND POLISHED IAW SRM 51-10-01. ACCOMPLISHED EDDY CURRENT INSPECTION 
- [SDR DXTR2017042103](https://openairdocs.org/sdr/DXTR2017042103), Apr 17, 2017: SKIN. CORRODED. LEFT WING WS 27 IN ZONE 512 HAS CORROSION. REMOVED PAINT IAW MM 20-31-00. ACCOMPLISHED EDDY CURRENT INSPECTION OF MULTIPLE AREAS AFTER BLENDING IAW NDI MANUAL P
- [SDR DXTR2017042102](https://openairdocs.org/sdr/DXTR2017042102), Apr 17, 2017: SKIN. CORRODED. RIGHT UPPER WING AT WS 57 ZONE 612 HAS CORROSION. REMOVED PAINT IAW MM 20-31-00. REMOVED CORROSION AND POLISHED IAW SRM 51-10-01. ACCOMPLISHED EDDY CURRENT INSP
- [SDR DXTR2017042101](https://openairdocs.org/sdr/DXTR2017042101), Apr 17, 2017: SKIN. CORRODED. RIGHT UPPER WING AT WS 44.5 HAS CORROSION. ACCOMPLISHED EDDY CURRENT INSPECTION OF MULTIPLE AREAS AFTER BLENDING IAW NDI MANUAL PART 6-20-00-02. NO DEFECTS NOTE
- [SDR DXTR2017041201](https://openairdocs.org/sdr/DXTR2017041201), Apr 12, 2017: THRUST REVERSER. CORRODED. LT & RT TR HAS MULTIPLE AREAS OF CORROSION, REPAIRED IAW AQRD ERO-890952. THIS REPAIR IS VALID FOR THE NOTED AMOUNT OF HOURS (500 HOURS), AFTER WHICH THE COMPON
- [SDR DXTA2016F00178](https://openairdocs.org/sdr/DXTA2016F00178), Sep 1, 2016: TRUNNION. WORN. REPAIR OF OVERSIZED DOOR ROD PIN HOLE IN MLG TRUNNION. REPORT NR S-680-ATA32/02RD, DATED FEB 28, 2014 WITH FAA FORM 8100-9 DATED 3/7/2014.
- [SDR DXTA2015031205993](https://openairdocs.org/sdr/DXTA2015031205993), Mar 11, 2015: WHEEL. CONTAMINATED. HEAVY SMOKE FROM RT BRAKE ASSEMBLY OBSERVED. NO PERFORMANCE ISSUES NOTED. NO FLUID VISIBLE ON DECK. INSPECTED RT MLG WW FOR LEAKS & RT INBD & OTBD BRAKE FUSES, 
- [SDR DXTA2015021905983](https://openairdocs.org/sdr/DXTA2015021905983), Feb 18, 2015: PRESSURE SWITCH. FAILED. RED ENGINE LOW OIL PRESSURE CAS MESSAGE. OCCURRED DURING CLIMB AT APPROX 37,000 FEET. OIL PRESSURE GAUGE IN THE GREEN BAND. REMOVED LOW OIL PRESSURE SWITCH. INS
- [SDR DXTA2013011705247](https://openairdocs.org/sdr/DXTA2013011705247), Jan 16, 2013: HOSE. LEAKING. UPON GEAR EXTENSION, HYD VOLUME LOW CAS MESSAGE POSTED. CYCLED ON AND OFF UNTIL TOUCHDOW. HYD FLUID IS VISIBLE FROM THE NOSE AND TRAILS THE ENTIRE LENGTH OF THE
- [SDR DXTR2011122900001](https://openairdocs.org/sdr/DXTR2011122900001), Dec 29, 2011: CABLE. DAMAGED. DURING NOSE WHEEL STEERING CHECK, THE TILLER WILL ONLY MOVE HALF WAY TO THE LEFT. IF YOU CONTINUE TO APPLY PRESSURE THERE IS A POP IN THE TILLER AND IT CONTINUE
- [SDR DXTA2011080804692](https://openairdocs.org/sdr/DXTA2011080804692), Aug 5, 2011: CONTROL HANDLE. FAILED. AFTER TAKEOFF, LANDING GEAR HANDLE WAS STUCK IN DOWN POSITION WITH 3 GREEN & NO RED. MADE AN UNEVENTFUL LANDING. MX ATTEMPTED TO RAISE GEAR. GEAR HANDLE WOULD N
- [SDR DXTA2011071904661](https://openairdocs.org/sdr/DXTA2011071904661), Jul 18, 2011: HOSE. LEAKING. DURING CLIMB, AMBER HYD PRESSURE LOW LT & RT AND HYD VOLUME LOW LIGHTS ILLUMINATED. ON POST FLIGHT, HYD FLUID PRESENT IN NOSE GEAR WELL AND ALONG BELLY OF ACFT.
- [SDR DXTA2011063004638](https://openairdocs.org/sdr/DXTA2011063004638), Jun 29, 2011: ACM. FAILED. ON TAXI OUT, GREY/WHITE SMOKE WAS NOTICED IN COCKPIT ALONG WITH A ODOR OF HOT METAL. APU WAS RUNNING AND APU BLEED VALVE AND ENGINE BLEED VALVES WERE OPEN. REMO
- [SDR DXTA2011062004624](https://openairdocs.org/sdr/DXTA2011062004624), Jun 19, 2011: O-RING. CUT. TAXIED OUT FROM FBO, WITH APU RUNNING, WITH BLEED AIR ON. GOT TO THE END OF RUNWAY, NEXT FOR TAKEOFF WHEN A LIGHT BLUE COLORED SMOKE STARTED TO FILL THE COCKPIT
- [SDR DXTA2010041904069](https://openairdocs.org/sdr/DXTA2010041904069), Apr 18, 2010: LANDING GEAR. MALFUNCTIONED. UPON TAKEOFF, LANDING GEAR WOULD NOT RETRACT. SHORTLY AFTER, HAD A WOW MISCOMPARE AMBER CAS. GEAR HANDLE WOULD NOT RAISE. JACKED ACFT AND FOUND NOSE GEAR NOT FU
- [SDR DXTA2010040704062](https://openairdocs.org/sdr/DXTA2010040704062), Apr 6, 2010: TRIM SYSTEM. FAILED. IMMEDIATELY AFTER TAKEOFF, WERE UNABLE TO TRIM THE ACFT NOSE DOWN. AFTER A FEW MOMENTS WE RECEIVED THE "PRIMARY STAB TRIM FAIL" CAS MESSAGE. SECONDARY TRIM FUNC
- [SDR DXTA2009090403772](https://openairdocs.org/sdr/DXTA2009090403772), Sep 3, 2009: BRACKET. DAMAGED. AUTOPILOT/YAW DAMPER DISENGAGED ON IT'S OWN IN FLIGHT AND COULD NOT RE-ENGAGE. YAW DAMP WAS ABLE TO RE-ENGAGE INTERMITTENTLY ON 'B' CHANNEL ONLY. REMOVED AND RE

All 53: https://openairdocs.org/deregistered/N380QS-2026-02-10/reports.md

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