- Owner type
- Co-owned, fractional ownership
- Serial number
- 700-0084
- Year built
- 2022
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- December 28, 2022
- Certificate issued
- January 21, 2026
- Expires
- January 31, 2033
- Mode S code
- AB7B38
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 N839QSMatched 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 N839QS not matched to an aircraft · 1
They name N839QS, 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 N839QSMatched 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 N839QS not matched to an aircraft · 1
They name N839QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
Service difficulty reports · 10
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026100610021Flap System · faultedCLIMBING THROUGH 8900FT THE AMBER FLAPS FAIL CAS DISPLAYED MOMENTARILY THEN WENT AWAY. THE MESSAGE CONTINUED TO DISPLAY THEN DISAPEAR UNTIL IT FINALLY REMAINED ON. INFLIGHT THE FLIGHT CONTROL SYNOPTICS PAGE SHOWED THE FLAPS AS AMBER. THE FLAP INDICATOR SHOWED SDR DXTA2025071404176Actuator · faultedAFTER TAKEOFF AND GEAR RETRACTION, HAD A YELLOW X FOR THE NOSE GEAR INDICATION ALONG WITH GEAR DISAGREE N. FOLLOWED QRH WHICH LED TO USING THE EMER GEAR RELEASE HANDLE FOR GEAR EXTENSION. RESULT WAS THREE GREEN INDICATION. PERFORMED FLY-BY AND TOWER CONFIRMSDR DXTA2025061903926Transducer · faultedOUTBOARD SPOILERS FAILED AUTO TEST DURING TAXI. REMOVED AND REPLACED RESSURE TRANSDUCER ON LEFT OUTBOAR ACCUMULATOR MANIFOLD REFERENCED AMM 27-60-33. AND LETTER FP240819 OPS AN LEAK CHECK GOOD.SDR DXTA2025052703625Oil System · leakingODOR OF OIL IN CKPIT & CABIN DURING APU OPS & DURING LOW THRUST ENG OPS. RAN ENGS W/ APU BLD VALVE CLOSED & ODOR IMPROVED, RAN APU & ODOR RETURNED. R & R HEPA FILTER IAW AMM 2 1-70-10. DURING CLOSE UP, FOUND OIL IN MUFFLER DRAIN LINES. REMOVED LOW LIMIT DUSDR DXTA2024122001559Adc · failedON MISSED APPROACH WE LOST OUR STBY ATTITUDE INDICATOR AIRSPEED FOLLOWED BY A RUDDER A & B FAIL. THAT THEN CHANGED TO A RUDDER REV A. REMOVED PART NO: 011-02337-01 REMOVED SERIAL NO: 1U6103649, DUE TO RUDDER MAINTENANCE CAS. INSTALLED CUSTOMER SUPPLIED REPAIRSDR DXTA2024110801080Switch · defectiveCABIN EMERG LIGHT: EMERGENCY LIGHTS WILL NOT TURN OFF. TRIED RESETTING BOTH COCKPIT G SWITCHES MULTIPLE TIMES WITH NO SUCCESS. CORRECTIVE ACTION; REMOVED AND REPLACE FORWARD EMERGENCY LIGHTING INERTIA SWITCH WITH A NEW SWITCH, PERFORMED EMERGENCY LIGHTING OPERSDR DXTA202401100798Actuator · defectiveRIGHT MLG LANDING GEAR EXTENISON: DECENDING BELOW 9000' AT 200KTS GOING INTO KMYL, LOWERED THE LANDING GEAR. RECEIVED A GEAR DISAGREE R AND AND GEAR DOOR OPEN AMBER CAS MESSAGE WITH AMBER HASHED BOX DISPLAYED FOR RIGHT MAIN GEAR. PULLED OUT THE EMERGENCY ABNSDR DXTA2024100100696Fuse · blownAFTER SHUTDOWN/BATTERIES DISCONNECT EMERGENCY LIGHTS DO NOT TURN OFF. RE-OPEN MCD, PROCEEDED TO DO THE 5G RESETS. EMERGENCY LIGHTS DO NOT TURN OFF. RE-CONNECT BATTERIES TO CLOSE MCD. MCD DOESNT CLOSE FROM THE OUTSIDE OR INSIDE. SINCE BATTERIES ARE CONNECTED. TSDR DXTA2024021410899Door · bindingCLOSED MAIN DOOR & HANDLE HAD ALOT OF FRICTION THOUGH HANDLE MOVEMENT. CABIN DOOR OPEN MESSAGE REMAINDED ON. OPENED DOOR & RAN CABIN DOOR OPEN ON GROUND CHKLST. COULD NOT CHECK HANDLE/PUSH TO OVERRIDE LIGHTS TO FLASH IAW CHKLST. TRIED TO CLOSE DOOR AGAIN & STISDR DXTA2024011510623Unknown · unknownEMERGENCY LIGHTS REMAIN ON WITH SWITCH IN OFF POSITION. RESET THE AFT EMERGENGY LIGHTING INERTIA SWITCH, ALL WORK DONE IAW 700 AMM 33-50-00, OPS CHECK GOOD,
Reports on N839QS not matched to an aircraft · 22
They name N839QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA2017040306395Handle · inoperativeLOW BRAKE PRESSURE AND ANTI-SKID INOPERATIVE LIGHTS ILLUMINATED AFTER LANDING WITH TOTAL BRAKE FAILURE. FOUND GEAR HANDLE SWITCH 112B BAD. REMOVED AND REPLACED THE SWITCH IAW MM 32-61-00. OPS CHECKED IAW MM 32-10-00. SATISFACTORY BLED BRAKES AND SERVICEDSDR DXTA2017041306395Brake Sys · failedM2B LOW BRAKE PRESSURE AND ANTI-SKID INOPERATIVE LIGHTS ILLUMINATED WHILE TAXIING TO THE GATE AFTER CLEARING THE RUNWAY WITH TOTAL BRAKE FAILURE. EMERGENCY BRAKING SYSTEM USED TO STOP PLANE.SDR DXTA2016121208337Pressure Switch · failedON SEAR EXTENSION LOW BRAKE PRESSURE AND ANTI-SKID ILLUMINATED. RAN APPROPRIATE CHECKLIST. DIVERTED. LANDING UNEVENTFUL. EMERGENCY BRAKING USED. BRAKE FLUID LEVEL WAS NORMAL. PRESSURE IN THE YELLOW BUT THAT WAS CHECKED AT LEAST 20 MIN AFTER LANDING. PERFORMED
See all 22 unmatched reportsSTCs 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