- Owner type
- Co-owned, fractional ownership
- Serial number
- 680A0212
- Year built
- 2019
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- August 25, 2019
- Certificate issued
- March 3, 2026
- Expires
- March 31, 2033
- Mode S code
- A8EFBA
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 3
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2018 | 1 |
|---|---|
| 2023 | 1 |
| 2026 | 1 |
Information bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N675QSMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Textron 680A aircraft
FAA incident reports
No FAA accident or incident reports matched to N675QSMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Textron 680A aircraft
Reports on N675QS not matched to an aircraft · 2
They name N675QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
Incident 20130811014119ICessna 560XL · Mesa, AZWhile climbing though FL 290, heard a pop and left PFD, MFD, and FMS screen went blank. Ahrs aux pwr 1 annunciator was illuminated and cabin pressurization controller went into isobaric mode. All circuit breakers were checked in.Incident 20080413836859ICessna 560XL · Torrance, CA(-23) On April 13, 2008, N675QS was taxiing on taxiway "a" and made a right turn to the transit parking area. The right wing tip impacted the nose cowling of Cessna 9420R. Pilot statement indicated there was no damage note to 675QS. Cessna N9420R received…
Service difficulty reports · 15
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026071508824Door · lack of lubeTHE MAIN CABIN DOOR HANDLE REQUIRES EXCESSIVE FORCE TO LATCH. DURING SEVERAL CLOSURES, THE RESISTANCE VARIED, BUT WHEN IT DID HANG UP, THE INSIDE HANDLE WAS ABOUT IN THE MIDDLE OF THE THROW. CLEANED AND LUBRICATED DOOR STOP. PREFORMED SATISFACTORY OPS CHECK SDR DXTA2026052108172Pin · lack of lubeMAIN CABIN DOOR HANDLE DIFFICULT TO FULLY ENGAGE IN LOCKED POSITION WHEN CLOSING DOOR FROM EITHER INSIDE OR OUTSIDE. HANDLE TRAVELS FREELY WHEN DOOR IS OPEN. OPERATED DOOR/DOOR HANDLE MULTIPLE TIMES FROM BOTH INSIDE AND OUTSIDE WITH DOOR IN THE OPEN AND CLOSSDR MISR2026020306754Module · defectiveON CLIMB OUT FULL NOSE DOWN TRIM REQUIRED. AUTOPILOT KICKED OFF. DECISION MADE TO SLOW THE AIRCRAFT BELOW 200 KTS TO MAINTAIN CONTROL AND LESSEN CONTROL INPUTS. LANDED AIRCRAFT UNDER MAX WEIGHT. CORRECTIVE ACTION: DURING ARES DOWNLOAD ANALYSTS DISCOVERED THESDR DXTA2026020306755Module · defectiveFLAP FAIL AND CAS MESSAGE APPEARED FOR EVERY FLAP SETTING SELECTED. RESET REQUIRED AND QRH RUN FOR EACH FAILURE (FLAPS 1, FLAPS 2, FLAPS FULL SELECTIONS). CORRECTIVE ACTION: DURING ARES DOWNLOAD ANALYSTS DISCOVERED THE GIA#1 FAILED ANDGENERATED ALL ASSOCIATEDSDR DXTA2025120906022Unknown · odorWITH THE APU ON & BLEED AIR SELECTED ON, SMELL AN ELECTRICAL BURNING. TRACKED ODOR BACK TO LT SIDE OVERHEAD HEAT DUCT. WHEN TOUCHED, METAL TRACK WHERE THE HEATER DUCT IS THAT HOUSES AN OVERHEAD LIGHT STRIP, TOO HOT TO TOUCH & HAS A BURNING ODOR. HEAT IS TRASDR 2025F00267Fitting · corrodedAFTER REMOVAL OF NLG ACTUATOR FOUND CORROSION ON THE AFT FITTING ASSEMBLY. REMOVED CORRODED NLG ACTUATOR FITTING AND REPLACED WITH NEW CUSTOMER SUPPLIED NLG FITTING IAW TEXTRON STANDARD REPAIR SR-680A-ATA53-33739 REV. A STANDARD REPAIR - NLG ACTUATOR FITTING RSDR 2025F00268Skin · corrodedFOUND 43 AREAS OF CORROSION UNDER AFT BELLY PANEL 316CBC. MECHANICALLY REMOVED CORROSION WHERE 36 NUTPLATES WERE REMOVED AND 4 ADDITIONAL AREAS IN BAY 316CBC IAW SRM 51-70-03. FOUND CORROSION BLENDS TO BE BEYOND LIMITS IAW SRM 51-70-03 EXCEEDING .002" OF MATERSDR 2025F00261Tunnel Wall · corrodedREPAIRED LEVEL 2 CORROSION ON LH AND RH NLG TUNNEL SKINS PER AQRD ERO-986034 REV.IR, TITLED "N675QS NLG TUNNEL CORROSION" DATED 28OCT25. SUPPORTED BY FAA FORM 8110-3 DATED 10/28/2025.SDR DXTA2025043003245Bushing · damagedMAIN DOOR: TO OPEN MAIN CABIN DOOR A PUSH IS REQUIRED FROM THE INSIDE TO GET THE DOOR TO OPEN. CORRECTIVE ACTION: ACCOMPLISHED FF-1 INFORMATION RECEIVED FROM NETJETS- MED FWD HINGE ADJUSTMENT BUSHING BOLT ARE SEIZED SO THE DOOR CANNOT BE ADJUSTED. REMOVED L/H SDR DXTA2024101400811Latch · out of rigMAIN DOOR: MAIN CABIN DOOR IS VERY HARD TO OPEN FROM THE OUTSIDE OF THE AIRCRAFT. REPEAT WRITE UP. CORRECTIVE ACTION: RIGGED CED LATCH/LOCK SYSTEM IN REF TO CE680A AMM 52-10-04. RIG CHECK GOOD, OPS CHECK OF CED OPENING FROM OUTSIDE GOOD WITH NO BINDING NOTED ASDR DXTA2024100700746Nut · looseMAIN DOOR: WE COULD NOT OPEN THE MAIN ENTRY DOOR FROM OUTSIDE THE AIRCRAFT, THE HANDLE WAS JAMMED, AND WOULD NOT MOVE IN EITHER DIRECTION. WE GAINED ACCESS TO THE AIRCRAFT FROM OUTSIDE THROUGH THE EMERGENCY EXIT. ONCE INSIDE, WITH SOME WIGGLING OF THE MED HSDR DXTA2022022157100Not Reported · not reportedEXIT SIGN LIGHT IN BACK OF CABIN AND EMER LIGHTS ABOVE AND BELOW THE TOILET ARE INOPERATIVE. // SIGNOFF // DUE TOTHE SATISFACTORTY TASK CARD OPS CHECK FROM SQK NUMBER 3,3 MCC REQUESTED SIGN 'OFF AND RELEASE. OPS CHECK GOOD IAW WITH TC-FLT-33-1001 (CESSNA 680 SDR DXTA2022011054850Contactor · abnormalDC GEN AMPS R AMBER CAS: DURING CRUISE AT FL400, AMBER DC GEN AMP R CAME ON STEADY AND QRH P1 WAS DIRECTED AND FOLLOWED. DIVERSION TO MSY WAS NECESSARY. // SIGNOFF// REMOVED AND REPLACED R/H GENERATOR SHUNT AND R/H GENERATOR CONTACTOR SN: CU-74516 WITH NEW SN:SDR 2021F00385Web · crackedNOSE WHEEL WELL WEB (PN: 7413133-10) IS CRACKED ON LH AND RH SIDES AT FS 75. REPAIRED IAW TEXTRON AVIATION STANDARD REPAIR SR-680A-ATA53-25890 DATED 06/01/2020, STANDARD REPAIR - CRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW), FRAME, WEB, AND DOUBLERS, FS 75SDR 2021F00125Cover · corroded#2 ENGINE ACCESSORY GEARBOX REAR COVER HAS MULTIPLE AREAS OF CORROSION. ACCOMPLISH TEMPORARY REPAIR AND PROTECTION OF THE AGB COVER FLANGES FROM MINOR CORROSION IAW P&WC 306D1 MM 72-60-01 REV. 17.
Reports on N675QS not matched to an aircraft · 19
They name N675QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA2015082606064Brake · wornRIGHT BRAKE IS WORN MORE THAN THE LEFT BRAKE. RT BRAKE IS GRABBING & CAUSING ACFT TO DART TO THE RIGHT ON TAXI & LANDING ROLL OUT. JACKED ACFT & REMOVED RT BRAKE. INSTALLED AN OVERHAULED BRAKE. COMPLIED WITH EMERGENCY BRAKE CHECK, BRAKE BLEEDS & ANTI-SKIDSDR DXTA2015082606063Valve · failedAFTER TAKEOFF, EXCESSIVE AMOUNT OF BLEED AIR ALONG WITH A BURNING ODOR. THE ACM OVERHEAT LIGHT ILLUMINATED FOLLOWED BY THE BLEED AIR OVERHEAT LIGHT. MASTER WARNING & MASTER CAUTION BOTH ILLUMINATED. THE THROTTLE WAS REDUCED BELOW CRUISE DETENT & LIGHTS EXTSDR DXTR2015022401Support Angle · crackedCRACK AT FWD DOOR SPRING ON FWD FRAME, PERFORMED EDDY CURRENT INSPECTION OF THE MAIN CABIN DOOR STRUCTURE IAW NDI MANUAL PN 6 20-00-02. VERIFIED EXISTENCE OF CRACK. NDI SERVICES PROVIDED ON W/O B180183. PERFORMED CUTOUT OF DAMADGED AREA. FABRICATED AND MAT
See all 19 unmatched reportsSTCs that may be installed · 16
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Textron 680A
STC ST04765NYUnprepared (Grass/Sod) Runway OperationsSTC ST00885LAInstallation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles.STC ST12344IBReplacement of the Halon Type 1211 portable fire extinguisher with Halotron BrX portable fire extinguisher with Halotron BrX portable fire extinguisher