- Owner type
- Co-owned, fractional ownership
- Serial number
- 700-0102
- Year built
- 2023
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- September 1, 2023
- Certificate issued
- October 8, 2026
- Expires
- October 31, 2033
- Mode S code
- ABB035
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 N852QSMatched 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 N852QSMatched 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 DXTA2026083109495Stop Fitting · out of adjustTHE MAIN CABIN DOOR HANDLE IS DIFFICULT TO MOVE TO THE CLOSED POSITION WHEN CLOSING THE CABIN DOOR FROM INSIDE. WHEN CLOSING THE DOOR ON THE PREVIOUS FLIGHT, WE RECEIVED AN AMBER CHECK DOORS CAS MESSAGE. FOLLOWED THE CHECKLIST RESET PROCEDURE AND THIS CLEARSDR DXTA2026081809308Pin · out of alignmentUNABLE TO LATCH MAIN CABIN DOOR CLOSED. ONE OF THE PINS IS RECESSED INTO THE DOOR AND IS NO LONGER ALIGNED WITH ITS HOLE. REMOVED THE AIRSTAIRS AND COVER PLATE. FOUND THE FWD MID DOOR PIN OUT OF ITS SOCKET, WE CORRECTED THE EFFECTED DOOR PIN REFERENCING AMM 5SDR DXTA2026081709282Pin · damagedWHEN THE CREW ARRIVED AT THE AIRCRAFT, THE MAIN CABIN DOOR WAS OPEN. THE SERVICE HUB CLEANERS HAVE BEEN ON BOARD AND WE'RE NOT ABLE TO CLOSE THE MAIN CABIN DOOR, THIS WAS CONFIRMED BY DOUG AT CMH MAINTENANCE THAT THE MAINTENANCE TECH AT TEB COULD NOT CLOSE THESDR DXTA2025100205149Control Valve · defectiveWHILE TAXING OUT AND APPLYING THE BRAKES THE AMBER "BRAKE 50% DEGRADED" CAS MESSAGE DISPLAYED EVERY TIME WE APPLIED THE BRAKES. IT WOULD DISAPPEAR WHEN BRAKES WERE RELEASED. ALL BRAKE PAD PINS ARE STICKING OUT PLENTY. CORRECTIVE ACTION: REPLACED AFT BRAKE CONTSDR 2025F00095Thrust Reverser · corrodedLH AND RH THRUST REVERSER INNER AIR WASHED SURFACES HAVE CORROSION. ACCOMPLISHED CORROSION REMOVAL AND REPAIR TO LH AND RH THRUST REVERSER BEAMS AND PIVOT DOORS INNER AIR WASHED SURFACES IAW SAFRAN NACELLES REPAIR SCHEME NO 907-623 REV B DATED 01/03/2024;REPAISDR 2025FA0000257Fuel Cell · fodWHILE ACCOMPLISHING SL 700-28-02, A RAG WAS FOUND IN THE RIGHT WING FUEL BAY NUMBER 13 FLAPPER. THIS WAS THE FIRST INSPECTION OF THE FUEL STORAGE SYSTEM SINCE PRODUCTION.SDR DXTA2025040202865Battery Pack · faultedEMERGENCY LIGHTING: EMER LIGHTS DO NOT ILLUMINATE WHEN POWER IS OFF AND SWITCH IS IN ON POSITION. ARM POSITION FUNCTIONS CORRECTLY. CORRECTIVE ACTION: EMERGENCY LIGHT DID NOTILLUMINATE WHEN POWER WAS OFF AND SWITCH WAS TURNED ON. SWAPPED EMERGENCY BATTERY PACSDR DXTA2025022702520Rub Block · looseDOOR STICKS HARD TO OPEN INSIDE AND OUT. GAINED ACCESS TO AIRCRAFT AND FOUND CABIN DOOR RUB BLOCK LOOSE. AJUSTED RUB BLOCK AND PERFORMED OPS CHECK. OPS CHECK GOOD. IAW CE-700 AMM 52-10-15. NO DEFECTS NOTED.SDR DXTA2024010210482Sensor · faultedBRAKE 50% DEGRADE CAS MESAGE. CYCLED GEAR , MESSAGE WENT AWAY. CYCLED AGAIN AND CAME BACK. LANDED WITHOUT OUTBOARD BRAKES. TAXING IN BRAKES BEGAN WORKING. IAW .ARES DOWNLOAD REVIEW OF 50 % BRAKE DEGRADE CAS MSG, R & R PRESSURE SENSOR AND ACCOMPLISHED SATISFACSDR DXTA2023121410329Unknown · unknownMAIN CABIN DOOR WILL NOT LATCH, DOOR OPERATES BUT WILL NOT LATCH. FOUND UPPER FORWARD MCD STRIKER LATCH TO BE OUT OF ADJUSTMENT. PERFORMED MCD STRIKER LATCH RIGGING IAW CE-700 MM 52-10-00. DURING RIGGING PROCEDURE FOUND ALL MCD STRIKER LATCH ECCENTRIC BOLTS TOSDR DXTA2023120410219Unknown · unknownMAIN CABIN DOOR CABIN DOOR OPEN AMBER CAS WILL NOT EXTINGUISH. TRIED TO CLOSE DOOR SEVERAL TIMES. RAN CHECKLIST LIGHT IS STILL ILLUMINATED.
Reports on N852QS not matched to an aircraft · 11
They name N852QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA2015070806041Oil System · low pressureINFLIGHT ENGINE SHUTDOWN, DUE TO A HIGH OIL PRESSURE INDICATION. PERFORMED A VISUAL INSPECTION OF RT ENGINE WITH NO ISSUES. PERFORMED A GROUND RUN TO CONFIRM HIGH OIL PRESSURE & DID NOT FIND OIL PRESSURE HIGH, FOUND OIL PRESSURE LOW, SHOWING 34 PSI AT IDLESDR DXTA2015050806016Strut · unserviceableZERO RUDDER TRAVEL IN FLIGHT DESPITE NORMAL CHECKS ON GND. SUSPECT RUDDER BIAS ISSUE. PREFORMED FUNCTIONAL TEST OF RUDDER BIAS SYS, TESTED SATISFACTORY. PERFORMED RUDDER CONTROL CIRCUIT FRICTION CHECK, CHECKED SATISFACTORY. FOUND THAT AFTER RUNNING ENGS ATSDR DXTA2015050506015Unknown · malfunctionedZERO RUDDER TRAVEL IN FLIGHT DESPITE NORMAL CHECKS ON GND.
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