# N305QS: 2006 Cessna 680, registration cancelled 2026-02-18 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 18, 2026 - Status when cancelled: Sale reported - 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: 680-0088 - Year built: 2006 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: July 19, 2006 - Last registry action: February 18, 2026 - Mode S code: A33354 - Location: [Bangor, ME](https://openairdocs.org/faa-place/ME/Bangor) - Owner type: Individual - Owner's area on the map: 44.8485° N, 68.8504° W: Placed by OpenAirDocs at the center of ZIP code 04401, within about 6 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N305QS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=305QS - Page: https://openairdocs.org/deregistered/N305QS-2026-02-18 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 (70, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DXTA2025111105628](https://openairdocs.org/sdr/DXTA2025111105628), Nov 9, 2025: SWITCH. OUT OF POSITION. IAW PREFLIGHT CHECKS THE EMERGENCY LIGHT SWITCH WAS PLACED TO ON POSITION. NONE OF THE EMERGENCY LIGHT ILLUMINATED. PER DISCUSSION WITH MAINTENANCE A 30 MINUTE - [SDR DXTA2025110705559](https://openairdocs.org/sdr/DXTA2025110705559), Nov 3, 2025: BATTERY PACK. DEFECTIVE. TWO FORWARD RIGHT EXTERIOR , ONE MAIN CABIN ENTRY, THREE MAIN CABIN OVERHEAD EMER LIGHTS REMAINED INOP AFTER 2 30 MINUTE CHARGE CYCLES. REPLACED BATTERY PACKS. - [SDR DXTA2025082704732](https://openairdocs.org/sdr/DXTA2025082704732), Aug 26, 2025: WARNING MESSAGE. FALSE ACTIVATION. MED WAS CLOSED WITH THE KEYLOCK IN THE LOCKED POSITION. THE CABIN DOOR CAS MESSAGE ILLUMINATED. COULD NOT DUPLICATE. MAINTENANCE PERFORMED IAW 52-10-00 AND 52-2 - [SDR DXTA2025052203567](https://openairdocs.org/sdr/DXTA2025052203567), May 20, 2025: LIGHT. UNKNOWN. EMERGENCY EXIT LIGHT ON LAV SEAT DOES NOT ILLUMINATE(PRE-FLIGHT) COMPLETED OPS CHECK OF THE EMERGENCY LIGHTING SYSTEM IAW MM 33-50-00. OPS CHECK GOOD AT THIS TI - [SDR JGVR20250517001](https://openairdocs.org/sdr/JGVR20250517001), May 17, 2025: HINGE FITTING. CORRODED. BLENDED CORRODED AREAS ON THE UPPER AND LOWER BRACKETS OF THE UPPER RUDDER HINGE AT THE BONDING STRAP BOLT HOLE, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITI - [SDR JGVR20250515001](https://openairdocs.org/sdr/JGVR20250515001), May 15, 2025: FRAME. CRACKED. FOUND CRACK IN THE MID FRAME OF THE NOSE LANDING GEAR WHEEL WELL, CUT OUT CRACKED AREA, PERFORMED NDT, FABRICATED AND INSTALLED REPAIR DOUBLER AND SHIMS PER NET - [SDR JGVR20250512001](https://openairdocs.org/sdr/JGVR20250512001), May 12, 2025: SKIN. DAMAGED. BLENDED CORRODED AREAS LOCATED ON THE UPPER SURFACE OF THE UPPER WING SKINS LOCATED UNDER AND ADJACENT TO THE LH WING AFT DRAG ANGLE (WING-TO-FUSELAGE FAIRING S - [SDR JGVR20250506001](https://openairdocs.org/sdr/JGVR20250506001), May 6, 2025: SKIN. CORRODED. REPAIRED THE CORRODED FUSELAGE SKIN AT THE LOWER TCAS ANTENNA CABLE FEED-THROUGH BY BLENDING CORRODED AREAS, PERFORMING NDT AND REPORTING FOR REPAIR DISPOSITION - [SDR JGVR20250429001](https://openairdocs.org/sdr/JGVR20250429001), Apr 29, 2025: ATTACH BOLT. CORRODED. MECHANICALLY REMOVED AREAS OF CORROSION LOCATED ON LH ELEVATOR CABLE PULLEY ATTACHMENT BRACKET LOCATED INSIDE BELLY PANEL BAY 154AC AND EXTENDING FORWARD SEVERA - [SDR JGVR202504007006](https://openairdocs.org/sdr/JGVR202504007006), Apr 7, 2025: PANEL. CORRODED. MECHANICALLY REMOVED 2 AREAS OF CORROSION FROM LH WING TRAILING EDGE PANEL 532GB, PERFORMED NDT, REPORTED FOR REPAIR DISPOSITION, CLEANED, TREATED, AND, PRIMED - [SDR JGVR202504007005](https://openairdocs.org/sdr/JGVR202504007005), Apr 7, 2025: BULKHEAD. CORRODED. MECHANICALLY REMOVED CORROSION LOCATED IN RH MLG WHEEL WELL AT MIDDLE EMERGENCY BRAKE LINE CARRY THRU ON WS 52.00 INBOARD SIDE, PERFORMED NDT, REPORTED FOR REPA - [SDR JGVR202504007004](https://openairdocs.org/sdr/JGVR202504007004), Apr 7, 2025: BULKHEAD. CORRODED. MECHANICALLY REMOVED CORROSION LOCATED IN LH MLG WHEEL WELL AT MIDDLE EMERGENCY BRAKE LINE CARRY THRU ON WS 52.00 INBOARD SIDE, PERFORMED NDT, REPORTED FOR REPA - [SDR JGVR202504007003](https://openairdocs.org/sdr/JGVR202504007003), Apr 7, 2025: HINGE BRACKET. CORRODED. REMOVED 3 AREAS OF CORROSION LOCATED ON LH #1 SPOILER OUTBOARD HINGE BRACKET, PERFORMED NDT, REPORTED FOR REPAIR DISPOSITION, CLEANED, TREATED, AND, PRIMED PER - [SDR JGVR202504007001](https://openairdocs.org/sdr/JGVR202504007001), Apr 7, 2025: ATTACH FITTING. CHAFED. MECHANICALLY REMOVED CHAFFING MARKS ON RH MIDDLE WING ATTACHMENT FITTING, PERFORMED NDT, REPORTED FOR REPAIR DISPOSITION, CLEANED, TREATED, AND, PRIMED PER NETJ - [SDR JGVR20250402004](https://openairdocs.org/sdr/JGVR20250402004), Apr 2, 2025: STRUCTURE. CORRODED. REPAIRED CORRODED AREAS OF THE AFT TAILCONE SKINS LOCATED UNDER AND ADJACENT TO THE AFT CHIN FAIRINGS, BY R&R THE FAIRINGS, BLENDING CORRODED AREAS, PERFORMING - [SDR JGVR20250402003](https://openairdocs.org/sdr/JGVR20250402003), Apr 2, 2025: PULLEY BRACKET. CORRODED. MECHANICALLY REMOVED 1 AREA OF CORROSION FROM LH ELEVATOR CABLE PULLEY BRACKET LOCATED INSIDE LOWER TAIL ACCESS BAY 323AC, PERFORMED NDT, REPORTED FOR REPAIR DI - [SDR JGVR20250402002](https://openairdocs.org/sdr/JGVR20250402002), Apr 2, 2025: FITTING. CORRODED. MECHANICALLY REMOVED CORROSION LOCATED ON LH AND RH MLG WHEEL WELL WS 37.00 FWD END, EMERGENCY BRAKE LINE CARRY THRU FITTINGS, PERFORMED NDT AND REPORTED FOR RE - [SDR JGVR20250402001](https://openairdocs.org/sdr/JGVR20250402001), Apr 2, 2025: SPAR. CORRODED. REPAIRED CORRODED AREA IN THE LH MLG WHEEL WELL ON THE AFT WING SPAR LOWER CLIP IN BAY 730DL, PERFORMED NDT, REPORTED FOR REPAIR DISPOSITION, CLEANED, TREATED, - [SDR JGVR20250331003](https://openairdocs.org/sdr/JGVR20250331003), Mar 31, 2025: SPAR. CORRODED. REPAIRED TWO CORRODED AREAS IN THE RH MLG WHEEL WELL ON THE AFT WING SPAR LOWER CLIP, PERFORMED NDT, REPORTED FOR REPAIR DISPOSITION, CLEANED, TREATED, AND PRIM - [SDR JGVR20250331002](https://openairdocs.org/sdr/JGVR20250331002), Mar 31, 2025: SPAR WEB. CORRODED. REPAIRED CORRODED AREAS AT OF THE LH WING AFT SPAR WEB AFT FACE AT THE #4 SPEED BRAKE PANEL HYDRAULIC LINE CARRY-THRU FITTINGS, PERFORMED NDT, REPORTED FOR REPA - [SDR JGVR20250331001](https://openairdocs.org/sdr/JGVR20250331001), Mar 31, 2025: SKIN. CORRODED. REPAIRED CORRODED AREA OF THE RIGHT WING LOWER SKIN JUST OUTBOARD OF THE MAIN JACKPOINT BY BLENDING AREA, PERFORMING NDT, REPORTING FOR REPAIR DISPOSITION, CLEA - [SDR JGVR20250317003](https://openairdocs.org/sdr/JGVR20250317003), Mar 17, 2025: SKIN. CORRODED. BLENDED AREA OF CORROSION FROM FUSELAGE SKIN LOCATED AFT OF E-EXIT DOOR OPENING, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS BY CLEANING, - [SDR JGVR20250317002](https://openairdocs.org/sdr/JGVR20250317002), Mar 17, 2025: SKIN. CORRODED. MECHANICALLY REMOVED 2 AREAS OF CORROSION FROM LH LOWER WING SKIN TRAILING EDGE JUST INBD OF FLAP ISLAND, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REP - [SDR JGVR20250317001](https://openairdocs.org/sdr/JGVR20250317001), Mar 17, 2025: DOOR. CORRODED. BLENDED MULTIPLE AREAS OF CORROSION ON THE EMERGENCY EXIT DOOR, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS BY CLEANING, TREATING AND PRIM - [SDR DXTA2024040811427](https://openairdocs.org/sdr/DXTA2024040811427), Apr 6, 2024: CABLE. READS HIGH. DOOR MECHANISM NOT BALANCED. VERY DIFFICULT TO OPEN AND CLOSES VIOLENTLY. ADJUSTED CABIN DOOR CABLES FORWARD AND AFT AFTER FINDING TENSIONS TO BE EXTREMELY HIGH - [SDR 2024F00079](https://openairdocs.org/sdr/2024F00079), Mar 17, 2024: SPAR CAP. CORRODED. CORROSION, LH/RH WING, LOWER FORWARD REAR SPAR CAP, W.S. 17-46. - [SDR 2024FA0000229](https://openairdocs.org/sdr/2024FA0000229), Mar 17, 2024: FAIRING. CORRODED. R/H ELEVATOR WEDGE FAIRING SKIN CORROSION BLEND-OUT. - [SDR 2023FA0000475](https://openairdocs.org/sdr/2023FA0000475), Aug 29, 2023: SPAR WEB. CORRODED. CORROSION AROUND AFT SPAR GEAR EXTEND AND RETRACT FEED-THROUGHS RH WHEEL WELL. ACCOMPLISHED TEXTRON AVIATION FIELD REPAIR S-680-ATA-57/03RD. - [SDR 2023FA0000474](https://openairdocs.org/sdr/2023FA0000474), Aug 29, 2023: SPAR WEB. CORRODED. CORROSION AROUND AFT SPAR EMERGENCY EXTENSION AND EMERGENCY BRAKE FEED-THROUGHS LH WHEEL WELL. ACCOMPLISHED TEXTRON AVIATION FIELD REPAIR S-680-ATA-57/03RD. - [SDR 2023F00259](https://openairdocs.org/sdr/2023F00259), Aug 29, 2023: SPAR WEB. CORRODED. CORROSION AROUND AFT SPAR GEAR EXTEND AND RETRACT FEED-THROUGHS RH WHEEL WELL. ACCOMPLISHED TEXTRON AVIATION FIELD REPAIR S-680-ATA-57/03RD. - [SDR 2023F00258](https://openairdocs.org/sdr/2023F00258), Aug 29, 2023: DOOR. DAMAGED. TWO FASTENERS (1EA SCREW AND 1EA 1/4 TURN) HAVE GOUGED THE STRUCTURE ABOVE THE EMERGENCY EXIT DOOR P/N 6711141-30. - [SDR DXTA2023071090550](https://openairdocs.org/sdr/DXTA2023071090550), Jul 7, 2023: UNKNOWN. UNKNOWN. CABIN EMERG LIGHT: THE EMERGENCY LIGHTS ON BATTERY PACK NUMBER 1 ARE NOT FUNCTIONING PROPERLY. //SIGNOFF// REMOVED WORN CABIN EMERGENCY LIGHT BATTERY PACK P/N: - [SDR DXTA2023061288360](https://openairdocs.org/sdr/DXTA2023061288360), Jun 12, 2023: UNKNOWN. UNKNOWN. EMERG LIGHT SWITCH: NO INTERIOR OR EXTERIOR EMERGENCY EXIT LIGHTS ILLUMINATE WITH THE EMERGENCY LIGHT SWITCH IN THE ARMED POSITION AND BATTERY SWITCHES OFF. EME - [SDR DXTA2023033183450](https://openairdocs.org/sdr/DXTA2023033183450), Mar 31, 2023: UNKNOWN. UNKNOWN. RIGHT SIDE TELESCOPING ROD IS BENT AND THE DOOR WILL NOT CLOSE. GAINED ACCESS TO THE RIGHT SIDE TELESCOPING ROD AND REMOVED AND REPLACED TELESCOPING ROD. IAW CE - [SDR DXTA2022081868320](https://openairdocs.org/sdr/DXTA2022081868320), Sep 8, 2022: ENGINE. DEFECTIVE. RIGHT ENGINE ENGINE VIBRATION INDICATION: WHILE IN CRUISE FLIGHT (FL330). RIGHT ENGINE BEGIN TO VIBRATE, ACCOMPANIED BY MOMENTARY "ENGINE SHUDOWN" CAS MESSAGE I - [SDR DXTA2021121353430](https://openairdocs.org/sdr/DXTA2021121353430), Dec 12, 2021: BATTERY. DEFECTIVE. CABIN EMERG LIGHT: WHEN PERFORMING THE EMER LTS TEST, THE SEAT NUMBER 8 CABIN EMERGENCY LIGHT/READING LIGHT DID NOT ILLUMINATE WHEN THE MAIN BATTERY SWITCHES WE - [SDR DXTA2021101750410](https://openairdocs.org/sdr/DXTA2021101750410), Oct 16, 2021: NONE. NONE. MAIN DOOR HANDLE: WHEN THE MAIN DOOR IS CLOSED AND LATCHED IN NORMAL CLOSED POSITION, THE RED BUTTON CAN NOT BE DEPRESSED TO OPEN MAIN CABIN DOOR. THE CREW MADE - [SDR DXTA2021101750390](https://openairdocs.org/sdr/DXTA2021101750390), Oct 16, 2021: HANDLE. NOT REPORTED. MAIN DOOR HANDLE: WHEN THE MAIN DOOR IS CLOSED AND LATCHED IN NORMAL CLOSED POSITION, THE RED BUTTON CAN NOT BE DEPRESSED TO OPEN MAIN CABIN DOOR. THE CREW MADE - [SDR DXTA2021013104657](https://openairdocs.org/sdr/DXTA2021013104657), Jan 29, 2021: DOOR. OUT OF BALANCE. MAIN CABIN DOOR NEEDS ADJUSTING. THE DOOR LOWERS VERY QUICKLY WITH VERY LITTLE COUNTERBALANCE WEIGHT HOLDING DOOR IN THE CLOSED POSITION. THE CONDITION MAY HAVE - [SDR DXTA2019073102693](https://openairdocs.org/sdr/DXTA2019073102693), Jul 31, 2019: WINDSHIELD. FAILED. FIRST OFFICER COCKPIT WINDOW - PASSING FL 220 RIGHT COCKPIT SIDE WINDSHIELD BEGAN TO CRACK. QRH WAS RUN AND WINDOW CONTINUED TO SLOWLY CRACK UNTIL 3000FT. ALL S - [SDR DXTA201904230188](https://openairdocs.org/sdr/DXTA201904230188), Apr 23, 2019: TRUSS. CORRODED. APU TRUSS MOUNT (FLANGE) CORROSION. REFERENCE TEXTRON AVIATION ENGINEERING MEMO DQ19152M1 DATED APRIL 12, 2019. - [SDR DXTA201904230187](https://openairdocs.org/sdr/DXTA201904230187), Apr 23, 2019: DRAG ANGLE. CRACKED. VERTICAL FIN DRAG ANGLE DAMAGE. REFERENCE TEXTRON AVIATION ENGINEERING MEMO DQ19155M1 DATED APRIL 15, 2019. - [SDR DXTA201904230186](https://openairdocs.org/sdr/DXTA201904230186), Apr 23, 2019: SPAR CAP. CORRODED. VERTICAL STAB. AFT SPAR CAP DAMAGE (CORROSION). REFERENCE TEXTRON AVIATION ENGINEERING MEMO DQ19154M1 DATED APRIL 12, 2019. - [SDR DXTA201904230185](https://openairdocs.org/sdr/DXTA201904230185), Apr 23, 2019: TRUSS. CORRODED. APU TRUSS MOUNT (FLANGE) CORROSION. REFERENCE ENGINEERING MEMO DQ19152M1. - [SDR DXTA201904230184](https://openairdocs.org/sdr/DXTA201904230184), Apr 23, 2019: DRAG ANGLE. CRACKED. VERTICAL FIN DRAG ANGLE DAMAGE. REFERENCE TEXTRON AVIATION ENGINEERING MEMO DQ19155M1 DATED APRIL 15, 2019. - [SDR DXTA201904230183](https://openairdocs.org/sdr/DXTA201904230183), Apr 23, 2019: SPAR CAP. CORRODED. VERTICAL STAB. AFT SPAR CAP DAMAGE (CORROSION). REFERENCE TEXTRON AVIATION ENGINEERING MEMO DQ19154M1 DATED APRIL 12, 2019. - [SDR DXTA201902051975](https://openairdocs.org/sdr/DXTA201902051975), Feb 1, 2019: SWITCH. DEFECTIVE. ALL LANDING GEAR RETRACTION DID NOT RETRACT - GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE HANDLE WAS LOCKED OUT AND COULD NOT BE MOVED. A SHORT TIME LATER WE RECE - [SDR JGVR2018110200001](https://openairdocs.org/sdr/JGVR2018110200001), Nov 2, 2018: INLET. CORRODED. BLENDED THREE AREA OF CORROSION ON THE APU INLET DEFLECTOR SCOOP. FOUND INLET/DEFLECTOR SCOOP NOT REPAIRABLE AND REPLACED WITH NEW. - [SDR DXTA2018022300633](https://openairdocs.org/sdr/DXTA2018022300633), Feb 23, 2018: WATER SEPARATOR. ODOR. DURING THE FINAL STAGES OF A HIGH ALTITUDE 3 HOUR FLIGHT WHILE MANEUVERING BELOW 10,000 FEET WITH THE THROTTLES PULLED BACK NEAR IDLE TO DESCEND AND SLOW DOWN A - [SDR JGVR20171219002](https://openairdocs.org/sdr/JGVR20171219002), Dec 19, 2017: SKIN. CORRODED. RIGHT WING UPPER WING SKIN OTBD OF MIDDLE DRAG ANGLE AFT END UNDERNEATH PAINT AND SEALANT HAS 4 AREAS OF SUSPECTED CORROSION. MECHANICALLY BLENDED LEVEL 1 CORRO All 70: https://openairdocs.org/deregistered/N305QS-2026-02-18/reports.md --- 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.