# N365QS: 2005 Cessna 680, registration cancelled 2025-06-02 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 2, 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: 680-0057 - Year built: 2005 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: November 9, 2005 - Certificate issued: April 9, 2019 - Last registry action: August 16, 2023 - Mode S code: A4204E - 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/N365QS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=365QS - Page: https://openairdocs.org/deregistered/N365QS-2025-06-02 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 (24) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DXTA2023110910008](https://openairdocs.org/sdr/DXTA2023110910008), Nov 8, 2023: BATTERY. INOPERATIVE. WHEN CONDUCTING POWER ON CHECKLIST, EMER LIGHTS - CHECK (EMER LIGHTS - SWITCH TO ON), ONLY ONE OF THE THREE AIRCRAFT RIGHT EXTERIOR EMERGENCY LIGHTS ILLUMINATE. - [SDR DXTA2023102698860](https://openairdocs.org/sdr/DXTA2023102698860), Oct 25, 2023: BATTERY. INOPERATIVE. EMERGENCY LIGHTING: ALL EMER LIGHTS INOP WITH EMER SWITCH IN THE ON POSITION AND BATTERIES OFF //SIGNOFF// FOUND #4 EMERGENCY LIGHT BATTERY TO BE INOP. REMOVED - [SDR DXTA2023100296900](https://openairdocs.org/sdr/DXTA2023100296900), Oct 2, 2023: CHARGER. DAMAGED. CABIN EMERG LIGHT: REPEAT WRITE UP. CABIN EMERGENCY LIGHT OVER THE GALLEY ONLY ILLUMATES WITH AIRCRAFT POWER ON. WITH AIRCRAFT POWER OFF LIGHT IS EITHER OFF OR - [SDR DXTA2023092996850](https://openairdocs.org/sdr/DXTA2023092996850), Sep 29, 2023: UNKNOWN. UNKNOWN. EMERGENCY LIGHT OVER GALLEY COUNTERTOP WHICH ILLUMINATES THE MAIN CABIN DOOR INOP DURING PREFLIGHT CHECKS. WITH CREW ONBOARD, VERIFIED GALLEY EMERGENCY LIGHT TU - [SDR DXTA2023090594470](https://openairdocs.org/sdr/DXTA2023090594470), Sep 3, 2023: UNKNOWN. UNKNOWN. AVIONICS ACCESS DOOR: RIGHT AFT NOSE DOOR MECHANICAL LATCH OPENED AT ABOUT 7000 FEET DURING CLIMB //SIGNOFF// REMOVED COVER FOR WIRING HARNESS AND FOUND BROKEN - [SDR DXTA2022061563940](https://openairdocs.org/sdr/DXTA2022061563940), Jun 14, 2022: PIN. LOOSE. EMERG EXIT SIGN/LIGHT: FORWARD FACING EMERGENCY EXIT SIGN LIGHT ON BULKHEAD ABOVE SEAT 9 HEADREST IS INOPERATIVE.// SIGNOFF// UPON INSPECTION, FOUND THE PIN ON - [SDR DXTA2022020856390](https://openairdocs.org/sdr/DXTA2022020856390), Feb 7, 2022: NOT REPORTED. NOT REPORTED. NLG LANDING GEAR UNLOCK LIGHT: ON GEAR EXTENSION WE HAD 3 GREEN DOWN AND LOCKED INDICATIONS BUT ALSO HAD THE GEAR UNSAFE HORN. WE ELECTED TO GO AROUND. ON RETRA - [SDR DXTA2021102150620](https://openairdocs.org/sdr/DXTA2021102150620), Oct 20, 2021: NONE. NONE. LEFT SIDE INTERIOR, EXTERIOR MAIN CABIN DOOR ENTRANCE, AND RIGHT WING LANDING EMERGENCY LIGHTS ARE INOPERATIVE. THE LIGHTS DO NOT EVEN ILLUMINATE WHEN THE MAIN - [SDR JGVR20200911001](https://openairdocs.org/sdr/JGVR20200911001), Sep 11, 2020: SPAR. DAMAGED. A) REPAIRED BLENDED AREAS ON LT WING LOWER REAR SPAR ANGLE AT LWS 27 AND LWS 40 PER AQRD ERO-966905 TITLED "LT WING REAR SPAR ANGLE REPAIR" DATED 09/11/2020 AND - [SDR 2TJR20200124320](https://openairdocs.org/sdr/2TJR20200124320), Jan 23, 2020: SPAR CAP. CORRODED. CORROSION DAMAGE ON LH WING WHEEL WELL, LH AFT SPAR PN 6922431-3, LOWER CAP AT LWS 32.00 - [SDR EBVR20190321001](https://openairdocs.org/sdr/EBVR20190321001), Mar 21, 2019: SHROUD. CRACKED. DURING INCOMING INSPECTION FOUND THE CO-PILOT SEAT IB SHROUD CRACKED. REPAIR WAS PERFORMED IAW AQRD REPAIR ERO-954897 REV.IR, APPROVED BY FORM FAA 8110-3, DATED - [SDR DXTA2018FA0000409](https://openairdocs.org/sdr/DXTA2018FA0000409), Oct 8, 2018: SPAR CAP. CORRODED. CORROSION, CENTER WING, LOWER SKIN C/T REAR SPAR WS 18 - WS 23. ACCOMPLISHED FAA FORM 8100-9, FIELD REPAIR FR-680-0057-4639 REV-. - [SDR 2018FA0000399](https://openairdocs.org/sdr/2018FA0000399), Oct 2, 2018: COWLING. DAMAGED. RIGHT UPPER COWL OUTBOARD AREA HAS HOLE THROUGH INNER LAYERS OF COMPOSITE INTO CORE MATERIAL AND MINOR CHAFFING MARKS ADJACENT TO THE PUNCTURE. - [SDR DXTA2013092605521](https://openairdocs.org/sdr/DXTA2013092605521), Sep 26, 2013: DISPLAY. FAILED. PRIOR TO ENGINE START, NR 2 DISPLAY UNIT STARTED FLASHING ON AND OFF RAPIDLY. AFTER ABOUT 20 SECONDS A STRONG ELECTRICAL BURNING ODOR WAS APPARENT IN COCKPIT. O - [SDR DXTA201304170556](https://openairdocs.org/sdr/DXTA201304170556), Apr 16, 2013: ACM. SEIZED. UNABLE TO CONTROL ENVIRONMENTAL TEMPS IN ANY CONFIGURATION. HOLDING FOR TAKEOFF, CABIN & COCKPIT BECAME WARM. SELECTED MANUAL DID NOT ALLOW TEMP TO BE CONTROLLE - [SDR DXTA2013032505331](https://openairdocs.org/sdr/DXTA2013032505331), Mar 23, 2013: LAMP. INOPERATIVE. ON APPROACH, GEAR SELECTED DOWN AND NO LEFT MAIN GEAR GREEN LIIGHT OBSERVED. COMPLETED M1 GEAR NOT IN LANDING POSITION CHECKLIST. GEAR HORN OBSERVED, ROTARY TES - [SDR DXTA2013020605276](https://openairdocs.org/sdr/DXTA2013020605276), Jan 29, 2013: ALTERNATOR. BURNED. STREAM OF WHITE SMOKE WAS SEEN EMANATING FROM UNDERSIDE OF RT ENGINE AFTER START. NO FIRE INDICATION. R & R RT ALTERNATOR IAW MM 24-20-10 ALTERNATOR OPS CHECK G - [SDR DXTA2013010705231](https://openairdocs.org/sdr/DXTA2013010705231), Jan 4, 2013: WARNING HORN. FALSE ACTIVATION. ON APPROACH, GEAR APPEARED TO EXTEND NORMALLY, DISPLAYING 3 GREEN LIGHTS. ATTEMPTED TO EXTEND FLAPS TO 35, GEAR UNSAFE HORN SOUNDED. RETRACTED FLAPS TO 15 AND H - [SDR DXTA2012012004849](https://openairdocs.org/sdr/DXTA2012012004849), Jan 18, 2012: OIL SYSTEM. OVERSERVICED. WHILE ON THE GROUND, ACFT FILLED WITH SMOKE WHEN APU BLEED WAS SELECTED ON. SMOKE APPEARED TO COME THROUGH ENVIRONMENTAL SYSTEM. FOUND APU OIL OVER SERVICED. SE - [SDR DXTA2011070804653](https://openairdocs.org/sdr/DXTA2011070804653), Jul 8, 2011: SWITCH. MALFUNCTIONED. AMBER FLAPS FAIL CAS MESSAGE. FLAPS WOULD NOT RESET. FLAPS INDICATING AT 7 DEGREES. R & R SWITCH OPS CHECKED GOOD RESTORED PEDESTAL AND OPS CHECKED. ALL WORK IA - [SDR DXTA2010090804225](https://openairdocs.org/sdr/DXTA2010090804225), Sep 7, 2010: ACTUATOR. FAILED. LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. WHEN GEAR WAS SELCTED UP NOSE GEAR REMAINED DOWN WITH GREEN NOSE GEAR LIGHT AND RED UNLOCKED LIGHT ILLUMINATED. R - [SDR 2010FA0000334](https://openairdocs.org/sdr/2010FA0000334), Apr 9, 2010: STIFFENER. CORRODED. DURING REPLACEMENT OF RUDDER HINGE BRACKETS ON VERTICAL STABILIZERS REAR SPAR, EXFOLIATION CORROSION WAS FOUND ON THE LOWER BRACKET (P/N: 6931050-10) OF THE UPP - [SDR DXTA200702676](https://openairdocs.org/sdr/DXTA200702676), Dec 13, 2007: WARNING SYSTEM. FALSE INDICATION. AMBER (ROLL SYSTEM CONTROL FAULT) APPEARED SEVERAL TIMES ON DESCENT, WITH AUTOPILOT ON AND OFF. TESTED SEVERAL TIMES WITHOUT DUPLICATING THE DISCREPANCY. VIEWED - [SDR DXTA200701923](https://openairdocs.org/sdr/DXTA200701923), Feb 8, 2007: BRAKE ASSY. HOT. UPON APPLIED BRAKES A/C PULL TO THE LT. AT SHUTDOWN, LT INSIDE BRAKE WAS SMOKING AND VERY HOT. TAXI TIME WAS GREATER THAN 5 MIN. BRAKES DID NOT PULL AT TAXI SPE --- 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.