- Owner type
- Co-owned, fractional ownership
- Serial number
- 680A0323
- Year built
- 2022
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- September 27, 2022
- Certificate issued
- April 2, 2024
- Expires
- April 30, 2031
- Mode S code
- AC920A
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 N909QSMatched 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 N909QSMatched 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
Service difficulty reports · 8
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026022306947Control Module · failedAFTER TAKEOFF LANDING GEAR HANDLE WILL NOT MOVE TO UP POSITION. SUSPECT INTERLOCK SOLENOID FAILED. REMOVED LANDING GEAR HANDLE AND REPLACED WITH CUSTOMER SUPPLIED OVERHAULED LANDING GEAR HANDLE. PERFORMED SYSTEM OPERATIONAL CHECK, NO DEFECTS NOTED. SYSTEM OPESDR DXTA2025070904168Bellcrank · out of adjustTHE DOOR COMES UP, BUT THE LATCHING HANDLE WILL NOT ENGAGE, STUCK IN THE OPEN POSITION CORRECTIVE ACTION: REALIGNED PIN BELL CRANK. IAW CE680A AMM 52-10-04. OPS CHECK GOOD.SDR DXTA2025060603762Engine · faultedIN FLIGHT ENGINE SHUTDOWN. AT APPROXIMATELY FL 330 ON DECENT WE NOTICED A SEVERE RUMBLE FROM THE RIGHT ENGINE, AND LOSS OF THRUST. WE ALSO NOTICED ITT RISE TO 900. THE THRUST WAS ERRATIC AND NOT USABLE. ACCOMPLISHED THE INFLIGHT ENGINE SHUTDOWN QRC AND PROSDR DXTA2025012402061Filter · odorCOCKPIT ODOR: AFTER A FULL PREFLIGHT WITH APU ON WITH BLEED AIR SELECTED ON, ENTRY DOOR WAS CLOSED FOR DEPARTURE. UPON SITTING DOWN IN COCKPIT BOTH PILOT AND COPILOT NOTICED A PROMINENT ELECTRICAL BURNING SMELL. NO VISIBLE SMOKE WAS SEEN. THE SMELL WAS SIMSDR DXTA2024102400925Pin · out of limitsMAIN DOOR: MAIN CABIN DOOR WILL NOT FULLY LATCH CLOSE WITH EITHER THE INTERNAL OR EXTERNAL LATCH HANDLE CORRECTIVE ACTION; ADJUSTED THE DOOR HANDLE STOPS. NOW ALL PINS ARE WITHIN THE MEASUREMENTS GIVEN. OPERATED THE DOOR TEN TIMES WITH NO ISSUES CLOSING FROM ISDR DXTA2024091600541Block · obstructedMAIN DOOR: UPON OPENING DOOR FROM OUTSIDE OR INSIDE OF AIRCRAFT ONCE HANDLE IS RELEASED DOOR OPENS APPROXIMATLY 1 INCH AND STOPS. DOOR MUST BE PHYSICALLY PULLED OR PUSHED TO GET THE DOOR TO OPEN. CORRECTIVE ACTION: FURTHER INVESTIGATION AND TROUBLESHOOTING FOSDR DXTA2023022781360None · noneON DEPARTURE, PASSING THROUGH 10,000' TO 14,000' GOT AMBER CABIN ALT MESSAGE. GOT AS HIGH AS 11,500' BEFORE CLEARANCE BACK TO 10,000'. AT 11,000' RED CABIN ALT MESSAGE ILLUMINATED MOMENTARILY & EXTINGUISHED BACK DOWN TO 10,000'. EMER DESCENT, QRC ACCOMPD W/SDR DXTA2022110273100Pcb · defectiveON GROUND CHECK DOORS AND CABIN DOOR OPEN AMBER CAS MESSAGES DISPLYED. RAN QRH PROCEDURE AND CHECK DOORS WENT OUT BUT CABIN DOOR OPEN REMAINED ON WITH THE CABIN DOOR IN THE CLOSED POSITION, PINS ENGAGED. SIGNOFF // PERFORMED DVI, RESET AND T/S ON CABIN DOOR S
Reports on N909QS not matched to an aircraft · 5
They name N909QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA200601768Metering Valve · failedAFTER TAKEOFF A LOUD BANG CAN BE HEARD AND FELT AS THE GEAR HANDLE IS RAISED. LAST TAKEOFF AT -6C WAS THE MOST PRONOUNCED. REMOVED FAULTY BRAKE METERING VALVE AND INSTALLED NEW UNIT. PERFORMED LEAK AND OPS CHECKED GOOD. IAW MM 32-42-03.SDR DXTA200500799Dmu · malfunctionedAT CRUISE ALTITUDE, HEARD CLICK OR SNAP AND FELT ABRUPT JERK OF NOSE TO LT . RUDDER TRIM RAN AWAY WITH 50 PERCENT DEFLECTION AND STOPPED RETRIMMED RUDDER WITH NO FURTHER INCIDENT. CHECKED RUDDER CABLE TENSIONS AND DMU FOR A PCU FORCE FLIGHT. CONNECTED DMU ANSDR DXTA200500731Rod End · out of adjustDURING FLIGHT, REQUIRED LARGE AMOUNT OF RIGHT AILERON TRIM FOR LEVEL FLIGHT AMOUNT INCREASED TO AT LEAST ONE QUARTER TRIM DEFLECTION (RIGHT WING DOWN TRIM) AT 250 KIAS. DID NOT INCREASE SPEED ABOVE 250 KIAS AS TRIM REQUIRED INCREASED WITH SPEED. REMOVED R/H A
STCs 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