- Owner type
- Co-owned, fractional ownership
- Serial number
- 700-0029
- Year built
- 2020
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- May 22, 2020
- Certificate issued
- September 4, 2025
- Expires
- September 30, 2032
- Mode S code
- AAF996
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 N806QSMatched 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 N806QSMatched 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 · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026042107701Proximity Switch · out of adjustAT FL410, RECEIVED A MASTER CAUTION CAS, EMERGENCY EXIT OPEN. RAN THE QRH 25C AND NOTED NO ABNORMAL INDICATIONS THROUGH THROUGH THE SYNOPTIC PAGES OR ON THE EXIT DOOR ITSELF. PROCEED TO DESTINATION WITH NO ABNORMAL INDICATIONS. THE CAS REMAINED THROUGH OUT THSDR DXTA2026030607119Smoke Detector · dirtyON GROUND GOT RED BAGGAGE FIRE LIGHT CAS MESSAGE. POWERED UP ACFT & ABLE TO DUPLICATE DISCREPANCY, WENT THRU FAULT HISTORY & FOUND ALERT ID 593. THIS FAULT IS TRIGGERED WHEN AFT CARGO SMOKE DETECTOR INPUT TO GSD2 INDICATES SMOKE DETECTED. IAW TROUBLE SHOOTISDR DXTA2026020206727Oxygen Bottle · leakingOXYGEN BOTTLES LOST PRESSURE WHILE IN FLIGHT. BOTH OXYGEN BOTTLES WERE AT 1500-1600 ON PREFLIGHT.SDR DXTA2025120205921Battery Pack · no testCABIN EMERGENCY LIGHTING IS NOT WORKING PROPERLY. WITH BATTERIES OFF & FOLLOWING A 30 MIN CHARGE WITH APU ON, EMERGENCY LIGHTS WILL ILLUMINATE IN ON, BUT FAIL TO ILLUMINATE IN ARM. FAILURE DISCOVERED DURING PREFLT WHEN INTERIOR & EXTERIOR EMERGENCY LIGHTS WOUSDR DXTA2024122301590Diode · inoperativeFLOOR LIGHTING UNDER SEATS 5, 9, AND LAV ARE INOP. CABIN EMERG LIGHT: FLOOR LIGHTING UNDER SEATS 5, 9, AND LAV ARE INOP. REMOVED SEAT 5 SHROUD AND INSPECTED CONNECTOR PC2043. FOUND PIN 1 RECESSED IN CONNECTOR, REMOVED AND INSTALLED NEW 43031-0009 PIN AND INSESDR DXTA2024120201329Light · inoperativeEMERG EXIT SIGN/LIGHT: CABIN FORWARD BULKHEAD EXIT SIGN ABOVE SEAT 3 INTERMITTENT. APPEARS TO WORK WITH EMER LIGHTS ON, BUT DOES NOT WORK WITH EMER LIGHTS ARMED AND PAX SAFETY ON. CORRECTIVE ACTION; GAINED ACCESS TD A/C. POWERED UP NC VIA GPU. PERFORMED OPS CHSDR DXTA2024050711697Battery Pack · failedEMERGENCY LIGHTING WILL NOT WORK UNDER OWN POWER. THEY DO WORK WITH SHIPS POWER ON. R & R BATTERY PACKS DUE TO INTERNAL FAILURE IAW AMM 33-50-05.SDR DXTA2023112910172Fuse · faultedLOWER LAV EMER LIGHT DOES NOT ILLUMINATE WITH POWER ON CHECKLIST PER AOM. INSPECTED ALL LIGHT CONNECTIONS & WIRING ASSOCIATED WITH EMER TOILET PATH WIRING . REF WDM 33-50-01. NO DEFECTS NOTED. NOTICED FUSE H0007 HAD MIGRATED OUT SLIGHTLY. PUSHED FUSE BACK IN SDR DXTA2023062889750Unknown · unknownEMERGENCY LIGHT SING ON THE FORWARD BULKHEAD IS OUT WHEN IN THE ARMED POSITION. CREW HAS GIVEN MCC PERMISSION TO SIGN OFF AS EIE.SDR 2023FA0000318Thrust Reverser · corrodedL/H THRUST REVERSER I/B AND O/B BEAMS HAS AREAS OF MINOR CORROSION.SDR DXTA2022092370950Battery Pack · abnormalEMERG EXIT SIGN/LIGHT: EMER LIGHTS WORKED ON INITIAL POWER UP PRE FLIGHT BUT ARE FAILING TO ILLUMINATE ON SHUT DOWN. // SIGNOFF// REMOVED AND REPLACED EMERGENCY LIGHT RELAY KF125 PERFORMED OPERATIONAL CHECKS OPS CHECKS FAILED REF CE-700 AMM 24-60 45 REMOVED ANSDR DXTA2022021056500Not Reported · not reportedCABIN EMERG LIGHT: EMER LIGHTS WILL NOT ILLUMINATE IN THE "ON" POSITION, BUT THEY DO ILLUMINATE IN THE "ARM" POSITION. WE RAN THE APU FOR 20 MINUTES AND THEN SHUT DOWN AND ATTEMPTED TO TEST AGAIN AND SAME ISSUE. AFTER FURTHER CONFERRING WITH MCC WE RAN THE ASDR DXTA2020082304018Sensor · out of positionAFTER TAKEOFF AND SELECTING LANDING GEAR UP, NOSE GEAR CAME UP, BUT BOTH MAIN GEAR INDICATIONS WERE AMBER. GEAR MISCOMPARE AND GEAR DOOR OPEN CAS MESSAGES APPEARED. AFTER SELECTING LANDING GEAR HANDLE DOWN, NOTHING HAPPENED FOR APPROXIMATELY 90 SECONDS. THE
Reports on N806QS not matched to an aircraft · 13
They name N806QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA2014033005704Brake Assy · malfunctionedRIGHT BRAKE DRAGGED SEVERELY DURING EXITING RUNWAY. SIGNIFICANT VIBRATION & YAWING WERE EXPERIENCED. AFTER SETTING & RELEASING THE PARKING BRAKE & WAITED 5 MINUTES, THE TAXI IN WAS NORMAL. JACKED RT MLG, INSPECTED BRAKE, NO DEFECTS WERE NOTED. WHEEL FREELYSDR DXTA2010091704241Flap System · frozenDURING FLAP EXTENSION ON APPROACH, THE FLAPS FROZE BETWEEN THE 7 DEGREE DETENT AND THE 15 DEGREE DETENT. RAN FLAPS THUR ALL POSITIONS VARIOUS TIMES - NO DEFECTS NOTED. PLACED LOAD ON FLAPS AND RAN NO DEFECTS. OPEN RT PEDESTAL PANEL. EXAMINED SWITCHES WHILE RSDR DXTA2009010103452Pitot System · contaminatedVISUAL DISCREPANCY OBSERVED DURING TAKEOFF CROSS CHECKS. NO FLAGS OR ANNUNCIATORS WITNESSED. PILOTSIDE AIRSPEED STAYED STEADY AT 53 KTS. COPILOTS AIRSPEED WAS INCREASING AT A NORMAL RATE. ABORTED TAKEOFF AT 86 KTS. PURGED CAPT PITOT SYS IAW MM 34-11-10 PAG
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