- Owner type
- Co-owned, fractional ownership
- Serial number
- 700-0073
- Year built
- 2022
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- June 13, 2022
- Certificate issued
- February 5, 2026
- Expires
- February 28, 2033
- Mode S code
- AB59C9
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 2
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 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 N830QSMatched 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 700 aircraft
FAA incident reports
No FAA accident or incident reports matched to N830QSMatched 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 700 aircraft
Service difficulty reports · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2025102105362Pcb · faultyDURING DESCENT YELLOW CAS MESSAGE, "ELEC EMER L," DISPLAYED. SEVERAL MINUTES LATER YELLOW CAS MESSAGE, "BATTERY DISCHARGE L," ALSO DISPLAYED. FOLLOWED QRH PROCEDURES TO INCLUDE AN EMERGENCY GEAR EXTENSION. REMOVED FAILED ELE SYS MON PCB NZ107 AND INSTALLED NESDR DXTR2025072901Cap Seal · fracturedWHILE ACCOMPLISHING LT MLG LUBRICATION TASK CARD AMM 12-20-10-612, AND WHILE LUBRICATING INBOARD END OF LT MLG ACTUATOR, FOUND THE END CAP ASSY P/N: 7441511-20 TO BE FRACTURED. THIS END CAP IS DESIGNED TO NOT ONLY RETAIN THE GREASE BUT ALSO CAPTURES THE PIN - SDR DXTA2025040903018Handle · out of adjustWHEN CLOSING MAIN DOOR FROM INSIDE CABIN DOOR OPEN CAS AND AMBER DOOR OPEN LIGHT DOESN'T EXTINGUISH UNLESS DOOR HANDLE IS PUSHED DOWN. WHEN OPENING DOOR FROM INSIDE, PUSHING RED THUMB BUTTON DOESN'T ACTIVATE THE HANDLE UNLESS HANDLE IS 1ST PUSHED DOWN. CORRECTSDR DXTA2025031802737Battery Pack · defectiveEMERGENCY LIGHTING: EMERGENCY LIGHTS FAIL THE PREFLIGHT TEST. NO EMERGENCY LIGHTS WORK WITH SWITCH IN THE ARM POSITION. ALL LIGHTS WORK WITH THE SWITCH IN THE ON POSITION. CREW RAN QRH PROCEDURE FOR ONE HOUR WITH NO CHANGE. CORRECTIVE ACTION; REPLACED THE #I ESDR DXTA2024092600659Door · unknownWHEN CLOSING MAIN CABIN DOOR, AMBER DOOR OPEN LIGHT AND CAS REMAIN ILLUMINATED. POWER CYCLE WORKED TO CLEAR MALFUNCTION, BUT REOCCURED 2 LEGS LATER. PERFORMED MED OPS CHECK PER CE-700 AMM 52-10-00 MULTIPLE TIMES. PERFORMED MED WARNING SYSTEM OPS CHECK PER AMSDR DXTR2024062502Structure · corrodedLEFT THRUST REVERSER UPPER BUCKET, LOCATED ON O/B SIDE NEEDS PAINT TOUCH-UP. REPAIR OF PAINT & CORROSION PER AQRD EWO-5998 REV. IR. & AQRD 912781 REV. A. REPAIRED C/W ON 8130-3, UNDER WO 32221130, CRS 9AQR662C.SDR DXTR20224062501Frame · corrodedR/H T/R I/B FRAME BETWEEN BUCKETS NEEDS PAINT TOUCH-UP. REPAIR OF PAINT & CORROSSION PER AQRD EWO-5999 REV. IR. & AQRD 912781 REV. A. REPAIRED C/W ON 8130-3 UNDER WO 32221130, CRS 9AQR662C.SDR DXTA2024021210872Gdu · faultedDURING DECENT GSD FAIL 1,2 AND 3 DISPLAYED ALONE WITH MULTIPLE CORRESPONDING SYSTEM, FAILURE MESSAGES. AVIONICS INTEGRATION (IAC, NIC PROC, MAU, GEA, IAPS): DURING A GSD FAILURE WE GOT A GTC MESSAGE OF L PFD CARD3 ERROR AND ALSO L PFD CARD3 REM REMOVED "SUSPESDR DXTA2023081793310Unknown · unknownMAIN DOOR: MAIN CABIN DOOR HANDLE WILL NOT MOVE FROM THE OPEN POSITION. IT IS MECHANICALLY JAMMED. DOOR CANNOT BE LATCHED CLOSED. ARRIVED AT AIRCRAFT IN HANGAR NOTING MED LEFT OPEN. TECHS ATTEMPTED TO MOVE INNER DOOR HANDLE TO THE LATCHED POSITION AND CONFIRMSDR 2023F00066Arm · gougedCOPILOTS RUDDER PEDAL ADJUSTMENT ARM GOUGED. ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ38345M1 DATED FEBRUARY 22, 2023; 700-0073 COPILOTS RUDDER PEDAL ADJUSTMENT ARM GOUGE.SDR DXTA2022102472710Wire Harness · damagedMAIN DOOR: "CABIN DOOR OPEN" ILLUMINATED INFLIGHT. LIGHT WAS INTERMITTENT IN TURBULENCE. REMOVED AND REPLACED CABIN THRESHOLD WIRING HARNESS PN: 8250171-1 NSN. OPS CHECK GOOD NO DEFECTS AT THIS TIME. RETURNED ALL REMOVED COMPONENTS FOR ACCESS BACK TO ORIGINAL
Reports on N830QS not matched to an aircraft · 12
They name N830QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA2018052501003Seal · wornPRESSURIZATION FAILURE AT FL410. SOUND OF AN AIR LEAK. NOISE QUICKLY GOT LOUDER, BECAME WHISTLING FOLLOWED BY LOUDER WHISTLING AND AIRFLOW. CABIN RATE HELD MOMENTARILY AT START OF NOISE, BUT QUICKLY LET GO AND BECAME A RAPID DECOMPRESSION. WHILE RUNNING EMERGSDR DXTA2017062506417Downlock Switch · unserviceableAFTER TAKEOFF, TRIED TO RETRACT THE GEAR. ALL GEAR WOULD COME UP. AND LIGHTS EXTINGUISH. AFTER ABOUT 10 SECONDS THE GEAR UNSAFE AND GREEN NOSE GEAR LIGHT WOULD ILLUMINATE. TRIED RECYCLING TWICE BUT DID NOT FIX THE PROBLEM. SOUNDED LIKE NOSE GEAR WOULD RETRACTSDR DXTA2015012105967Unknown · odorAFTER DEPARTURE WITH THROTTLES IN CLIMB DETENT, HAD STRONG ELECTRICAL BURNING ODOR THROUGHOUT CABIN. OVERHEAD FAN WAS OFF & FREON A/C WAS OFF. THERE WAS A LIGHT HAZE LOOKING BACK INTO THE CABIN. RAN ENGINES AT HIGH POWER WHILE TESTING EACH ACFT SYS INDIVI
STCs that may be installed · 11
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Textron 700
STC ST12145SEInstallation of Starlink Aviation SystemSTC ST04736NYTrue Blue TS28 Emergency Battery Power Supply ReplacementSTC ST00415BOInstallation of an NVIS/NVG compatible lighting system and infrared capable exterior lightingSTC ST04575ATInstallation of the Rockwell Collins ALT-1000+/ -4000+ with 5G FilteringSTC ST02812LAInstallation of the Honeywell EDG-100 Connected Engine Data Access SystemSTC ST04572CHInstallation of an Airborne Terminal System and a Ka RadomeSTC ST02746SEInstallation of external aerodynamic modifications, interior furnishings and equipment, including provisions for additional non-essential systemsSTC ST02694SEGroup Reduced Vertical Separation Minimum (RVSM) airworthiness approvalSTC ST04211NYInstallation of of NSM UNIFIS 3000 G2 Flight Inspection SystemSTC ST01971WIInstallation of the Garmin G5000 Software Changes & GH-3900 Standby Configuration UpdatesSTC ST01027DEInstallation of MarathonNorco Aerospace Inc Nickel Cadmium battery in place of existing Nickel Cadmium main aircraft battery/batteries