# N385QS: 2006 Cessna 680, registration cancelled 2026-06-01 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 1, 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: 680-0115 - Year built: 2006 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 20, 2006 - Certificate issued: November 8, 2019 - Last registry action: September 15, 2023 - Mode S code: A46F4C - Owner type: Corporation - The mark today: https://openairdocs.org/aircraft/N385QS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=385QS - Page: https://openairdocs.org/deregistered/N385QS-2026-06-01 From the FAA registry file of October 28, 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 (39) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DXTA2026010906472](https://openairdocs.org/sdr/DXTA2026010906472), Jan 7, 2026: PRESSURE VALVE. FAULTED. SHORTLY AFTER TAKEOFF POWER APPLIED, HP VALVE FAIL LT AMBER CAS LIGHT ILLUMINATED. COMPLETED APPROPRIATE QRH. INSPECTED GD001 GROUND. NO DISCREPANCIES. RANG WIR - [SDR JGVR20251119002](https://openairdocs.org/sdr/JGVR20251119002), Nov 19, 2025: SKIN. CORRODED. REPAIRED THE CORRODED AREA ON THE RT SKIN/PANEL OF THE NOSE LANDING GEAR TUNNEL BY BLENDING CORRODED AREA, PERFORMING NDT, REPORTING FOR REPAIR DISPOSITION, FAB - [SDR JGVR20251119001](https://openairdocs.org/sdr/JGVR20251119001), Nov 19, 2025: SKIN. CORRODED. REPAIRED CORRODED AREAS OF THE LOWER AFT TAILCONE SKINS, LOCATED UNDER AND ADJACENT TO THE AFT CHIN FAIRING JOINT, BY BLENDING AREAS, PERFORMING NDT, REPORTING - [SDR JGVR20251118001](https://openairdocs.org/sdr/JGVR20251118001), Nov 18, 2025: SKIN. CORRODED. BLENDED CORRODED AREA ON THE OUTER SKIN OF THE EMERGENCY EXIT DOOR IN THE LOWER AFT CORNER, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, - [SDR JGVR20251017003](https://openairdocs.org/sdr/JGVR20251017003), Oct 17, 2025: SPAR. CORRODED. BLENDED AREA OF CORROSION LOCATED ON THE LT AFT WING SPAR LOWER WEB AT THE EMERGENCY BRAKE CARRY THROUGH FITTING HOLES, LOCATED IN THE LT MAIN LANDING GEAR WHEE - [SDR JGVR20251017002](https://openairdocs.org/sdr/JGVR20251017002), Oct 17, 2025: SPAR CAP. CORRODED. BLENDED AREA OF CORROSION LOCATED INSIDE LH MAIN GEAR WELL BAY ON THE AFT LOWER SPAR CAP, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, A - [SDR JGVR20251017001](https://openairdocs.org/sdr/JGVR20251017001), Oct 17, 2025: SPAR. CORRODED. BLENDED AREA OF CORROSION LOCATED INSIDE RIGHT MAIN GEAR WELL BAY 720DR ON THE LOWER AFT SPAR CAP, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, T - [SDR DXTA2025031002606](https://openairdocs.org/sdr/DXTA2025031002606), Mar 6, 2025: ACM. MALFUNCTIONED. TEMPERATURE CONTROL: DIVERTED DUE TO AMBER EMERGENCY PRESSURIZATION AND ACM O'TEMP CLIMBING THROUGH APROX 37,000 FT THE RIGHT ENGINE ITT BEGAN TO CLIMB RAPIDLY. - [SDR 2023F00224](https://openairdocs.org/sdr/2023F00224), Jul 13, 2023: ANGLE. CORRODED. CORROSION, LH WING, AFT SPAR, WS 28. ACCOMPLISHED TEXTRON AVIATION FIELD REPAIR FR-680-0115-12138 REV-, DATED JULY 11, 2023 AND FAA FORM 8100-9 DATED 7/11/2023; - [SDR 2021FA0000252](https://openairdocs.org/sdr/2021FA0000252), Sep 2, 2021: PANEL. DAMAGED. LH HORIZONTAL WIPER PANEL LOWER AFT SECTION MOUNTING HOLES ARE OVERSIZED AND ELONGATED. REFERENCE TEXTRON AVIATION ENGINEERING MEMO DQ31281M1 REV A DATED 31/AUG - [SDR DXTA2021080246190](https://openairdocs.org/sdr/DXTA2021080246190), Aug 1, 2021: LINE. FAILED. HYDRAULIC LINE: HYDRAULIC PRESSURE LOW L-R AMBER CAS BOTH EMERGENCY GEAR BLOWDOWN AND EMERGENCY BRAKING APPLIED. PERFORMED MULTIPLE GEAR SWINGS WITH THE HYDRAUL - [SDR DXTA2021061643770](https://openairdocs.org/sdr/DXTA2021061643770), Jun 15, 2021: DOOR. BINDING. MAIN DOOR: COULD NOT OPEN MAIN CABIN DOOR USING RED RELEASE BUTTON OR SECONDARY RELEASE. WITH ASSISTANCE OF GROUND PERSONNEL WE WERE OPEN DOOR. "CORRECTIVE ACTI - [SDR 2021F00023](https://openairdocs.org/sdr/2021F00023), Feb 9, 2021: SKIN. DAMAGED. OVERSIZED HOLE CENTER WING UPPER SKIN WS 36.5 AT THE REAR SPAR. ACCOMPLISHED A FIELD REPAIR FR680-0115-8859 REV - DATED 0/4/2021; FIELD REPAIR - HOLE OVERSIZE, - [SDR 2021F00022](https://openairdocs.org/sdr/2021F00022), Feb 9, 2021: SKIN. CORRODED. CORROSION, WING UPPER SKINS, WS37. ACCOMPLISHED TEXTRON AVIATION STANDARD REPAIR SR-680-ATA57-27245 REV - DATED 10/08/2020; STANDARD REPAIR - CORROSION, WING, U - [SDR 2021F00021](https://openairdocs.org/sdr/2021F00021), Feb 9, 2021: SKIN. DAMAGED. OVER SIZED HOLE, UPPER CENTER WING SKIN WS 36.5 AT THE MAIN SPAR. ACCOMPLISHED TEXTRON AVIATION FIELD REPAIR FR-680-0115-8872 REV - DATED 02/08/2021; FIELD REPA - [SDR 2021F00019](https://openairdocs.org/sdr/2021F00019), Feb 8, 2021: PANEL. CORRODED. REPAIR TO HORIZONTAL TRAILING EDGE PANELS. TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ28656M2 DATED FEB. 7, 2021. - [SDR 2021F00018](https://openairdocs.org/sdr/2021F00018), Feb 8, 2021: PICCOLO TUBE. DAMAGED. REPAIR TO ANTI-ICE PICCOLO TUBE FLANGE. TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ28735 DATED JANUARY 30, 2021. - [SDR 2021FA0000035](https://openairdocs.org/sdr/2021FA0000035), Feb 6, 2021: FAIRING. DELAMINATED. LEFT HAND WING TO FUSELAGE MID FAIRING DAMAGED. REPAIRED L/H WING TO FUSELAGE MID FAIRING P/N 6922706-17 I.A.W TEXTRON AVIATION ENGINEERING DQ28747, REF. S-750- - [SDR 2021FA0000034](https://openairdocs.org/sdr/2021FA0000034), Feb 5, 2021: FRAME. CRACKED. NLG WHEEL WELL OVERHEAD STRUCTURE FRAME IS CRACKED-UPPER MID UPPER. REFERENCE AQRD ENGINEERING REPAIR ORDER NO. ERO-104483 REV IR DATED JAN 25 2021 - [SDR DXTA202004213648](https://openairdocs.org/sdr/DXTA202004213648), Apr 20, 2020: LINE. DISCONNECTED. CABIN ALTITUDE AMBER CAS ILLUMINATED - ON CLIMB OUT AT 20000 FEET WE OBSERVED CABIN CLIMBING HIGHER THAN NORMAL AND AT 34000 FEET THE AMBER CAS (8500) LIGHT ILL - [SDR JGVR20190219002](https://openairdocs.org/sdr/JGVR20190219002), Feb 19, 2019: ACCESS PANEL. CORRODED. BLENDED AND TREATED 28 AREAS OF CORROSION ON THE CABIN ENTRY DOOR INNER DOOR SKIN ACCESS PANELS PER REPAIR MEMO. - [SDR JGVR20190219001](https://openairdocs.org/sdr/JGVR20190219001), Feb 19, 2019: SKIN. CORRODED. REPAIRED 22 CORRODED AREAS OF THE DROPPED AISLE FLOOR (INTERIOR FUSELAGE SKIN) BY BLENDING AREAS, PERFORMING ULTRASONIC AND EDDY CURRENT INSPECTIONS, TREATING, - [SDR 2017F00063](https://openairdocs.org/sdr/2017F00063), Mar 1, 2017: FRAME. DAMAGED. ELONGATED & OVERSIZED HOLES AT BS 624 FRAME IN TAILCONE FOR RUDDER BIAS ATTACHMENT. - [SDR 2017F00062](https://openairdocs.org/sdr/2017F00062), Mar 1, 2017: FITTING. CORRODED. AFT LEFT AND RIGHT SIDE SPAR WEB BULKHEAD FITTING CORRODED. - [SDR 2017F00061](https://openairdocs.org/sdr/2017F00061), Mar 1, 2017: SPAR. CORRODED. CENTER SPAR BULKHEAD AND LEFT AND RIGHT WING STATION 37.0 RIB FITTING CORRODED. - [SDR 2017F00060](https://openairdocs.org/sdr/2017F00060), Mar 1, 2017: FITTING. CORRODED. AFT LEFT AND RIGHT SIDE SPAR WEB BULKHEAD FITTING CORRODED. - [SDR DXTA2015071706044](https://openairdocs.org/sdr/DXTA2015071706044), Jul 16, 2015: FAN. FAILED. SMOKE IN THE CABIN ON THE GROUND WITH THE APU RUNNING & BLEED AIR ON. DISCONNECTED BLEED AIR DUCT COUPLING & BORESCOPED APU INLET COMPRESSOR AREA & BLEED AIR PO - [SDR DXTA2015052206021](https://openairdocs.org/sdr/DXTA2015052206021), May 18, 2015: ACTUATOR. FAILED. NO TAKEOFF MSG, DUE TO ROLL SYS. UPON INITIAL OPS CHECKS NOTED NO CAS MSGS. REMOVED THE ACCESS PANEL & INSPECTED THE PROXIMITY SWITCH & TARGET. NOTED THE TARGET - [SDR DXTA2014121505946](https://openairdocs.org/sdr/DXTA2014121505946), Dec 13, 2014: WIRE. CHAFED. DURING GEAR RETRACTION, ALL FOUR GEAR LIGHTS EXTINGUISHED NORMALLY, BUT WITHIN 1-2 SECONDS, RED UPLOCK LIGHT FLICKERED & THEN STAYED ON. GEAR EXTENDED NORMALLY. - [SDR DXTA2013043005366](https://openairdocs.org/sdr/DXTA2013043005366), Apr 30, 2013: DISPLAY. INOPERATIVE. AS THE FLYING PILOT, SMELLED SMOKE AND SAW FLAGS ON THE STNDBY ATTITUDE INDICATOR. MY PARTNER SAW IT AT THE SAME TIME AND TURNED OFF THE STANDYBY INDICATOR. THA - [SDR CWQR20130311018](https://openairdocs.org/sdr/CWQR20130311018), Mar 11, 2013: HEAT EXCHANGER. CRACKED. DURING A SCHEDULED INSPECTION WE WERE PREFORMING A PRODUCT IMPROVEMENT (REPLACEMENT OF DUCT ASSY 6914070-67) WE NOTICED THAT THE HEAT EXCHANGER SIDE PLATE HAD 1 - [SDR CWQR20130305015](https://openairdocs.org/sdr/CWQR20130305015), Mar 5, 2013: HEAT EXCHANGER. CRACKED. DURING A SCHEDULED INSPECTION, NOTICED THE HEAT EXCHANGER SIDE PLATE HAD THREE CRACKS ABOUT .30 INCH LONG. OPPOSITE SIDE OF THE HEAT EXCHANGER WAS CRACKED IN TH - [SDR DXTA2012092105130](https://openairdocs.org/sdr/DXTA2012092105130), Sep 20, 2012: APU. LEAKING. ON PREFLIGHT WITH APU RUNNING AND AC ON, SMELLED OILY ODOR AND SAW LIGHT SMOKE IN CABIN. WITH BLEED AIR OFF, SMOKE WENT AWAY WITH JUST A LITTLE OIL ODOR. REMOVE - [SDR DXTA2012033004934](https://openairdocs.org/sdr/DXTA2012033004934), Mar 29, 2012: WARNING LIGHT. NO INDICATION. RIGHT MLG LIGHT WOULD NOT ILLUMINATE. FOLLOWED THE CHECKLIST PROCEDURE. RESET GEAR SYS IAW MM 32-00-00, BLED SYS. RESERVICED N2 BOTTLE AND SAFETIED. GEAR SWING - [SDR DXTA2012031904923](https://openairdocs.org/sdr/DXTA2012031904923), Mar 16, 2012: SEAL. LEAKING. AFTER TAKEOFF, GEAR WOULD NOT RETRACT. A SHORT TIME LATER WE GOT THE AMBER "WOW MISCOMPRE" CAS MESSAGE. ALL CBS ARE SET. - [SDR DXTA200803254](https://openairdocs.org/sdr/DXTA200803254), Aug 29, 2008: CONTROL UNIT. FAULTY. AFTER TAKEOFF, ATTEMPTED TO RAISE GEAR. HANDLE MOVED TO THE UP POSITION, BUT THE GEAR REMAINED EXTENDED. NO OTHER INDICATIONS PRESENT - NO CAS MESSAGE, NO RED L - [SDR DXTA200803176](https://openairdocs.org/sdr/DXTA200803176), Jul 14, 2008: STRUT. OUT OF ADJUST. LOUD NOISE FROM NOSE WAS HEARD DURING GEAR RETRACTION. NOISE (THUMP) WAS FOLLOWED WITH RED GEAR UNLOCK LIGHT REMAINING ILLUMINATED. GEAR EXTENDED WITH 3 GREEN A - [SDR DXTA200803164](https://openairdocs.org/sdr/DXTA200803164), Jul 8, 2008: SQUAT SWITCH. OUT OF ADJUST. ON GEAR RETRACTION, NOSE GEAR MADE A NOTICEABLE CLUNK AND BANG AND THE RED GEAR UNLOCK LIGHT REMAINED ILLUMINATED. JACKED AIRCRAFT AND CHECKED FOR PLAY IN NLG A - [SDR DXTA20082904](https://openairdocs.org/sdr/DXTA20082904), Feb 28, 2008: STRUT. UNKNOWN. UPON GEAR RETRACTION, A THUMPING NOISE WAS COMING FROM THE NOSEWHEEL COMPARTMENT ALONG WITH A FLASHING RED UNLOCK LIGHT. PERFORMED SEVERAL GEAR RETRACTIONS AND ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20080715842239I](https://openairdocs.org/incident/20080715842239I), Jul 15, 2008: Gulstm 680 (N385QS), Pittsburgh, PA, No damage. (-23) During departure, aircraft retracted gear, crew heard a loud noise and had an associated unsafe gear light. --- 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.