# N338QS: 2004 Cessna 680, registration cancelled 2023-06-21

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 21, 2023
- 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: 680-0011
- Year built: 2004
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 14, 2004
- Certificate issued: December 22, 2020
- Last registry action: April 7, 2023
- Mode S code: A3B4F6
- 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/N338QS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=338QS
- Page: https://openairdocs.org/deregistered/N338QS-2023-06-21

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 (42)

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

- [SDR JGVR20210319002](https://openairdocs.org/sdr/JGVR20210319002), Mar 19, 2021: STRUCTURE. CORRODED. REMOVED THE EXISTING EMERGENCY EXIT DOOR AND FOUND CORROSION ON THE DOOR AROUND THE CONTOUR RINGS. REMOVED THE CONTOUR RINGS FROM THE DOOR AND FOUND ADDITIONAL 
- [SDR JGVR20210319001](https://openairdocs.org/sdr/JGVR20210319001), Mar 19, 2021: SPAR. DAMAGED. REPAIRED THE LH WING REAR SPAR LOWER FORWARD ANGLE, LOCATED IN THE LH MAIN LANDING GEAR WHEEL WELL, BY BLENDING CORRODED AREA PERFORMING NDT AND INSTALLING A RE
- [SDR DXTA2021011804615](https://openairdocs.org/sdr/DXTA2021011804615), Jan 17, 2021: BOLT. FAILED. WHEN THE MAIN CABIN DOOR HANDLE IS OPENED FROM THE INSIDE, THE HANDLE HITS A METAL CYLINDER THAT PROTRUDES FROM THE GROUND. IF THE HANDLE IS FORCED ALL THE WAY 
- [SDR JGVR20200916001](https://openairdocs.org/sdr/JGVR20200916001), Sep 16, 2020: SKIN. CORRODED. REMOVED CORRODED RT UPPER INBOARD BONDED SKIN ASSY, P/N UNKNOWN, AND INSTALLED A NEW BONDED SKIN ASSY P/N 6922680-28 ONTO RT UPPER INBOARD WING. WORK PERFORMED 
- [SDR JGVR20200914002](https://openairdocs.org/sdr/JGVR20200914002), Sep 14, 2020: SKIN. CORRODED. REMOVE AND REPLACE CORRODED RT WING TRAILING EDGE SKIN P/N 6922681-70. REMOVED AND REPLACED CORRODED RT WING TRAILING EDGE SKIN BOND ASSEMBLY WITH NEW P/N 69226
- [SDR JGVR202009141001](https://openairdocs.org/sdr/JGVR202009141001), Sep 14, 2020: SKIN. CORRODED. BLENDED MULTIPLE AREAS OF CORROSION ON LT UPPER WING SKIN AT WS 37 FROM FS 408.46 THRU 482.46. PERFORMED AN EDDY CURRENT INSPECTION AND AN ULTRASONIC THICKNESS 
- [SDR JGVR20200902001](https://openairdocs.org/sdr/JGVR20200902001), Sep 2, 2020: SPAR. CORRODED. LT MLG WHEEL WELL LOWER AFT SPAR HAS 2 AREAS OF VERIFIED CORROSION. REMOVED 3 EACH HI-LOKS FROM LT MLG WHEEL WELL LOWER AFT SPAR FOR ACCESS. BLENDED 2 EACH AREA
- [SDR JGVR20200827002](https://openairdocs.org/sdr/JGVR20200827002), Aug 27, 2020: DRAG ANGLE. CORRODED. RT WING AFT DRAG ANGLE HAS 7 AREAS OF VERIFIED CORROSION ALONG OUTBOARD EDGE AND 6 AREAS OF VERIFIED CORROSION ON MIDDLE DRAG ANGLE OUTBOARD EDGE. REPAIRED DELA
- [SDR JGVR20200827001](https://openairdocs.org/sdr/JGVR20200827001), Aug 27, 2020: HINGE FITTING. CORRODED. RUDDER UPPER HINGE POINT, LOWER BRACKET HAS VERIFIED CORROSION AROUND ATTACH BOLT. HAND SANDED AREA OF CORROSION LOCATED ON UPPER RUDDER HINGE, LOWER PLATE, LT 
- [SDR DXTA2019F00066](https://openairdocs.org/sdr/DXTA2019F00066), Sep 17, 2018: SPAR CAP. CORRODED. VERTICAL STAB AFT SPAR CORROSION. ACCOMPLISHED ENGINEERING LETTER DQ15722M1 DATED SEPTEMBER 13, 2018; 680-0011. VERTICAL STABILIZER AFT SPAR CAP/RIM (P/N 696152
- [SDR DXTA2019F00060](https://openairdocs.org/sdr/DXTA2019F00060), Sep 13, 2018: SPAR CAP. CORRODED. VERTICAL STABILIZER AFT SPAR CAP/RIM DAMAGE (CORROSION). ENGINEERING REPAIR DEFINITION DQ15722M1 DATED 9/13/2017.
- [SDR DXTA2019F00059](https://openairdocs.org/sdr/DXTA2019F00059), Sep 12, 2018: SPAR. CORRODED. REPAIR OF CORROSION ON LT WING REAR SPAR LOWER CAP. REPAIR DEFINITION NR S-680-0011/05RD DATED 9/4/2018 WITH FAA FORM 8100-9 DATED 9/7/2018.
- [SDR DXTA2019F00057](https://openairdocs.org/sdr/DXTA2019F00057), Sep 12, 2018: SPAR. CORRODED. REPAIR OF CORROSION ON LT WING REAR SPAR LOWER CAP. REPAIR DEFINITION S-680-0011/05RD DATED 9/6/2017 WITH FAA FORM 8100-9 DATED 9/7/2018.
- [SDR DXTA2018FA0000361](https://openairdocs.org/sdr/DXTA2018FA0000361), Sep 11, 2018: SPAR WEB. DAMAGED. REPAIR OF RUDDER FWD SPAR LIGHTENING HOLE DAMAGED FLANGE. ENGINEERING REPAIR LETTER DQ1562M1 DATED SEPTEMBER 6, 2018.
- [SDR JGVR20170710002](https://openairdocs.org/sdr/JGVR20170710002), Jul 7, 2017: SKIN. DENTED. DENT ON THE BOTTOM OF THE LEFT WING 44 INCHES OTBD OF THE LT LANDING LIGHT. CONTOURED SKIN IAW SRM 51-00-03, AND 51-10-01. PERFORMED EDDY CURRENT INSPECTION IAW
- [SDR JGVR20170710001](https://openairdocs.org/sdr/JGVR20170710001), Jul 7, 2017: SKIN. DENTED. DENT IN THE RT WING LEADING EDGE CUFF SKIN. PERFORMED PERMANENT REPAIR IAW SRM 51-40-03, 51-00-03, AND MM 57-40-00
- [SDR DXTR2016122704](https://openairdocs.org/sdr/DXTR2016122704), Dec 27, 2016: SKIN. CORRODED. THE LEFT AND RIGHT UPPER AND LOWER HORIZONTAL STABILIZER SKIN HAVE AREAS OF CORROSION, BLENDED AREAS OF CORROSION, AND RETURNED TO SERVICE.
- [SDR DXTR2016122703](https://openairdocs.org/sdr/DXTR2016122703), Dec 27, 2016: SKIN. CORRODED. LEFT ELEVATOR LEADING EDGE AND AFT SKIN HVE AREAS OF CORROSION, BLENDED AREAS OF CORROSION, AND RETURNED TO SERVICE.
- [SDR DXTA2016033106218](https://openairdocs.org/sdr/DXTA2016033106218), Mar 31, 2016: SKIN. DENTED. LEFT WING HAS A DENT ON BOTTOM OF LE FWD OF OVERWING FUEL CAP. RT WING HAS LONG DENT RUNNING ABOUT 3 INCHES ALONG A LINE OF RIVETS ON BOTTOM OF LE FWD OF OVERWI
- [SDR DXTA2015090306075](https://openairdocs.org/sdr/DXTA2015090306075), Sep 2, 2015: UNKNOWN. ODOR. PASSENGERS COMPLAINED OF BOTH EXCESSIVE HEAT & EXHAUST ODOR. AIR FLOWS FROM BOTH COCKPIT & CABIN, WEMACS VERY LOW FROM ENGS ONLY, IMPROVES WITH APU ON LINE. WHE
- [SDR DXTA2015081706060](https://openairdocs.org/sdr/DXTA2015081706060), Aug 16, 2015: TRIM SYSTEM. UNCONTROLLABLE. PRIMARY STAB TRIM RUNAWAY INITIALLY UNCONTROLLABLE, ACFT PITCHED DOWN LOSING 2000 FEET UNTIL ACTUATING RED DISCONNECT BUTTON & TURNING ON SECONDARY TRIM, INDICA
- [SDR DXTA2015031305994](https://openairdocs.org/sdr/DXTA2015031305994), Mar 12, 2015: CONTROL HANDLE. MALFUNCTIONED. LEFT MLG WOULD NOT INDICATE DOWN & LOCKED WHEN LOWERED FOR LANDING. R & R THE LG CONTROL HANDLE ASSEMBLY IAW MM 32-30-10. OPS CHECKED GOOD. COMPLIED WITH HYD SY
- [SDR DXTA2013120905593](https://openairdocs.org/sdr/DXTA2013120905593), Dec 6, 2013: ACTUATOR. MALFUNCTIONED. UPON SELECTING LG DOWN RT MLG INDICATED NOT DOWN. RED UNLOCK LIGHT WAS ILLUMINATED AT THE SAME TIME. BY CHECKING A ROTARY TEST, BOTH RT LDG GEAR LIGHT BULBS WER
- [SDR CWQR20131016046](https://openairdocs.org/sdr/CWQR20131016046), Oct 16, 2013: DOOR FRAME. CRACKED. DURING INSPECTION, FOUND THE OUTER DOOR FRAME CRACKED UNDER THE TELECOPING ROD ATTACH POINT ON THE FWD OUTER CABIN DOOR FRAME. VERFIED CRACK WITH EDDY CURRENT I
- [SDR CWQR20131016045](https://openairdocs.org/sdr/CWQR20131016045), Oct 16, 2013: DOOR FRAME. CRACKED. DURING AN INSPECTION, FOUND OUTER DOOR FRAME CRACKED UNDER THE TELECOPING ROD ATTACH POINT ON THE AFT OUTER CABIN DOOR FRAME. VERFIED CRACK WITH EDDY CURRENT IN
- [SDR CWQR20130501033](https://openairdocs.org/sdr/CWQR20130501033), May 1, 2013: FIREWALL. CRACKED. DURING A SCHEDULED INSPECTION, FOUND THE APU FIREWALL CRACKED 2.75" IN LENGTH. REPLACED WITH NEW FIREWALL. THIS CONDITION AND A PICTURE WAS SENT TO UNDER SCR 65
- [SDR DXTA2013040105343](https://openairdocs.org/sdr/DXTA2013040105343), Mar 30, 2013: BRACKET. LOOSE. FLAPS FAILED IN FLIGHT BETWEEN 15-35 DEGREES. TRIED RESET BUTTON SEVERAL TIMES. AFTER LANDING AND AFTER POWER DOWN FLAPS RETRACTED NORMALLY. FAULT CODES 1 AND 9
- [SDR CWQR20121221053](https://openairdocs.org/sdr/CWQR20121221053), Dec 21, 2012: LINE. CHAFED. DURING A SCHEDULED INSPECTION, THE SHROUDING SCAT DUCT (PN S1053E24T) WAS FOUND TORN IN SEVERAL PLACES. WHEN REPLACING THE SCAT DUCT WE FOUND THE DUCT HAD CHAFE
- [SDR DXTA2012101505144](https://openairdocs.org/sdr/DXTA2012101505144), Oct 12, 2012: STRUT. DISCHARGED. ON GEAR RETRACTION, A VIOLENT, RHYTHMIC, CONTINUOUS THUMPING WAS FELT AND HEARD COMING FROM THE NOSE GEAR. THE RED GEAR UNLOCK LIGHT REMAINED ON ALSO, UNTIL GEA
- [SDR DXTA2011011804415](https://openairdocs.org/sdr/DXTA2011011804415), Jan 15, 2011: SWITCH. INTERMITTENT. NLG TOOK 45 SECONDS TO EXTEND AFTER GEAR HANDLE WAS LOWERED. RED UNLOCK LIGHT WAS ILLUMINATED DURING THAT TIME FRAME. CHECKED SWITCH ADJUSTMENT & FOUND NOSE UPL
- [SDR DXTA2010071204147](https://openairdocs.org/sdr/DXTA2010071204147), Jul 11, 2010: CONNECTOR. DAMAGED. DURING CRUISE & DESCENT, MLG UNLOCK ANNUNCIATOR ILLUMINATED ON & OFF IN TURBULENCE. CYCLED MLG APPLYING FREEZE SPRAY TO UPLOCK SWITCH. NO DEFECTS NOTED. CHECKED
- [SDR DXTA2010051704096](https://openairdocs.org/sdr/DXTA2010051704096), May 13, 2010: UPLOCK SWITCH. OUT OF ADJUST. DURING CRUISE FLIGHT, IN MODERATE TURBULENCE, THE RED GEAR UNSAFE LIGHT FLASHED ON AND OFF FOR AS LONG AS THE TURBULENCE LASTED. IT STOPPED IN SMOOTH AIR. NO PR
- [SDR DXTA2008121503402](https://openairdocs.org/sdr/DXTA2008121503402), Dec 15, 2008: ACTUATOR. INOPERATIVE. UPON LOWERING GEAR HANDLE, NOSE GEAR DID NOT LOCK DOWN. RECYCLED GEAR WITH SAME RESULTS. ON GO AROUND, NOSE GEAR LOCKED DOWN ON ITS OWN. DID NOT RUN CHECKLIST O
- [SDR DXTA2008121603402](https://openairdocs.org/sdr/DXTA2008121603402), Dec 15, 2008: LANDING GEAR. MALFUNCTIONED. UPON LOWERING GEAR HANDLE, NOSE GEAR DID NOT LOCK DOWN. RECYCLED GEAR WITH SAME RESULTS. ON GO-AROUND, NOSE GEAR LOCKED DOWN ON ITS OWN.
- [SDR DXTA200802749](https://openairdocs.org/sdr/DXTA200802749), Jan 5, 2008: ACTUATOR. MALFUNCTIONED. RUDDER BIAS FAULT CAS MESSAGE CAME ON AFTER ROTATION. R & R ACTUATOR NO FAULTS FOUND ON INSPECTION OF RUDDER BIAS COMPONENTS. C/W SATISFACTORY OPERATIONAL CHECK
- [SDR DXTA200702465](https://openairdocs.org/sdr/DXTA200702465), Sep 10, 2007: SERVO. OUT OF ADJUST. AIRCRAFT WILL NOT FLY STRAIGHT WITH A/P AT FL360. AILERON TRIM FULL R. RUDDER TRIM .1250 L, SLIGHT LT TURN, FUEL BALANCED, .79M / FL240 A TRIM FULL R - RUD TRIM
- [SDR DXTA200702466](https://openairdocs.org/sdr/DXTA200702466), Sep 10, 2007: STARTER GEN. TRIPPED. DURING TAKEOFF POWER APPLICATION THE LT GENERATOR HAS TRIPPED OFF LINE. ALL PRE-FLIGHT TESTS AND STARTS SHOW NORMAL OPERATION. REPLACED LT ENGINE STARTER/GEN WI
- [SDR DXTA200702376](https://openairdocs.org/sdr/DXTA200702376), Aug 1, 2007: POSITION SENSOR. MALFUNCTIONED. AMBER CAS (FLAPS FAIL) MESSAGE PUSHED EVENT MARKER, AT FL410, FOLLOWED CHECKLIST FLAP ON NR 2 DISPLAYED MOVED TO 7 DEGREES, WHEN IND = 0 DEGREES. R & R BOTH NR 
- [SDR DXTA200601807](https://openairdocs.org/sdr/DXTA200601807), Dec 19, 2006: UPLOCK SWITCH. OUT OF RIG. AT FL410 RED GEAR UNSAFE LIGHT ILLUMINATED AND EXTHINGUISHED APPROX 5-6 TIMES. NO GEAR HORN OR CAS MESSAGE. PERFORMED CONTINUITY CHECKS OF L, R + NOSE UPLOCK SW
- [SDR DXTA200601735](https://openairdocs.org/sdr/DXTA200601735), Nov 18, 2006: CONNECTOR. ARCED. NOTED ODOR IN COCKPIT FOUND CABIN PRESS CB POPPED. APPROX 30 SEC LATER THE RT ELEC PWR FEED, 3 CB POPPED NOTICED PRESSURE MODE SWITCH LIGHTS INOP. HAD TO USE MA
- [SDR DXTA200601278](https://openairdocs.org/sdr/DXTA200601278), Mar 3, 2006: TIRE. FAILED. ON TOUCH DOWN LEFT MAIN TIRES LOCKED UP AND BLEW OUT ON LANDING ROLL. NO ANTISKID CAS MESSAGE WAS DISPLAYED. - REMOVED & REPLACED LEFT INBOARD & OUTBOARD WHEELS
- [SDR DXTA200501023](https://openairdocs.org/sdr/DXTA200501023), Oct 14, 2005: AIR DATA MODULE. FAILED. AIR SPEED RT PFD FAILED, NO AIRSPEED INDICATION ON TAKEOFF ROLL. LEAK CHECKED COPILOT PITOT STATIC SYSTEM WITH NO DEFECTS NOTED. SYSTEM OPERATED NORMALLY. SWAPP

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