- Owner type
- Co-owned, fractional ownership
- Serial number
- 700-0025
- Year built
- 2020
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- February 28, 2020
- Certificate issued
- July 18, 2025
- Expires
- July 31, 2032
- Mode S code
- AAEABA
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 N802QSMatched 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
Investigations on N802QS not matched to an aircraft · 1
They name N802QS, but no registry record covers the date, the aircraft registered then was built later, or the investigation describes another aircraft.
FAA incident reports
No FAA accident or incident reports matched to N802QSMatched 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
Reports on N802QS not matched to an aircraft · 1
They name N802QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
Service difficulty reports · 16
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026032307336Elec Connector · damagedEVACUATION PATH LIGHT UNDER SEAT NR 4 IS NOT ILLUMINATING. REPAIRED POWER WIRE CONNECTOR. OPS CHECK GOOD. IAW SPM 20-30-20SDR DXTA2025102005342Light · malfunctionedWHEN EMER LTS ARE IN ARM AND PAX SAFETY SWITCH IS IN ON POSITION, THE WHITE EXIT LIGHT ABOVE THE FORWARD AIRSHOW SCREEN ON THE CABIN DIVIDER IS NOT ILLUMINATED. THE LIGHT WILL ILLUMINATE NORMALLY WHEN EMER LTS ARE PLACED IN THE ON POSITION. NO OTHER EMER LIGHTSDR DXTA2025082904757Elec Connector · disconnectedEMERGENCY EXIT LIGHT ON RIGHT SIDE OF AIRSTAIRS NOT ILLUMINATING. FOUND LIGHT DISCONNECTED FROM CONNECTOR, CHECK WIRES FOR DAMAGAE, RECONNECTED EMERGENCY LIGHT TO WIRE CONNECTOR. OPS TESTED EMERGENCY LIGHTS. OPS TEST GOOD. NO DEFECTS NOTED AT THIS TIME. REF
See all 16 reportsReports on N802QS not matched to an aircraft · 14
They name N802QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTR20170721Structure · bentSHEETMETAL DAMAGE ON MAIN CABIN DOOR LOWER FOWARD CORNER ON EXTERIOR EDGE. ACCOMPLISHED REPAIR BY AQRD ENGINEERING ERO-900686 INSTRUCTIONSSDR DXTA2014112605937Fuel Control · malfunctionedDESCENDING OUT OF CRUISE ALTITUDE, RT THROTTLE LEVER HAD NO EFFECT ON ENGINE POWER SETTING. RT ENGINE MAINTAINED CRUISE POWER, EVEN WHEN RT THROTTLE WAS BROUGHT TO IDLE. CREW SECURED RT ENGINE AS N2 WAS GOING TO EXCEED TOLERANCE, DECLARED AN EMERGENCY, & LANSDR DXTA2014082805869Motor · unserviceableAFTER LANDING THE LOW RAKE PRESS & ANTI-SKID INOPERATIVE, ANNUNCIATOR ILLUMINATED. NORMAL BRAKES NOT AVAILABLE, USED EMER BRAKES TO STOP THE ACFT. THE POWER BRAKE CIRCUIT BREAKER IS OUT. REMOVED AND REPLACED THE POWER BRAKE MOTOR IAW CE-560 MM 32-42-01. OPS
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