- Owner type
- Co-owned, fractional ownership
- Serial number
- 700-0082
- Year built
- 2022
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- November 25, 2022
- Certificate issued
- January 2, 2026
- Expires
- January 31, 2033
- Mode S code
- AB73CA
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 N837QSMatched 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 N837QSMatched 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 DXTA2026100509987Wire Harness · defectiveDURING CLIMB OUT WE RECEIVED A GROUND DETECT FAULT SIX TIMES. SHORTEST CAS MESSAGE WAS 5 SEC WHILE THE LONGEST WAS ABOUT 30 SEC. WE RAN THE QRH AND DIVERTED TO AUS FOR A LONGER RUNWAY. MESSAGE CLEARED BEFORE LANDING AND WE HAD NO ISSUES WITH LANDING, ROLL OUT SDR DXTA2025100305157Sensor · faultedRECURRING MALFUNCTION. ORIGINAL DISCOVERY T2PL6D00D5PN2 09/27/25 CLOSED WO T2PL6D00D5PN5 09/30/25. THIS FLIGHT, 09/30/25, AGAIN OBSERVED CAS MESSAGE "FUEL SCAV FAIL-R" (A) DURING DESCENT. QRH PROCEDURE EXTINGUISHED CAS MESSAGE. CORRECTIVE ACTION: REMOVED SUSPSDR DXTA2025093005121Sensor · faultedDURING DESCENT, THE FUEL SCAV FAIL-R AMBER CAS MESSAGE ILLUMINATED. THE CHECKLIST WAS RUN AND TURNING ON BOTH FUEL PUMPS PER THE CHECKLIST RESULTED IN THE AMBER MESSAGE BEING EXTINGUISHED. REMOVED RIGHT LOW LEVEL FUEL SENSING UNIT #2 (SR003) PART NO: 722888-2SDR DXTA2025082504707Light · dimEMERGENCY LIGHTS IN ARM POSITION WITH PAX SAFTEY BUTTON ON, INTERIOR MAIN CABIN DOOR EXIT, BUKHEAD EXIT, AND OVERWING EXIT LIGHTS ARE DIM AND FLICKER. EXTERIOR EMERGENCY LIGHTS ARE INOPERATIVE IN SAME SWITCH POSTION. WITH EMERGENCY LIGHT SWING IN ON, ALL LISDR DXTA2025012902106Apu · odorWHEN THE APU WAS STARTED AND BLEED AIR IS ON THERE IS AN OILY MUSTY SMELL COMING FROM THE BLEED AIR. TURN BLEED AIR OFF AND IT DISIPATES. CAN NOTICE A VERY SLIGHT HAZE IN THE COCKPIT AS WELL AS THE SMELL. REPLACED APU. OPS CHECK GOOD. IAW CE-700 AMM 49-10-00SDR DXTA2024111401128Striker · looseMAIN DOOR: MAIN CABIN DOOR HANDLE DIFFICULT TO OPEN AND CLOSE. DOOR HANDLE BINDS MIDWAY WHEN OPENING AND CLOSING THE DOOR FROM INSIDE AND OUTSIDE THE AIRCRAFT. CORRECTIVE ACTION; FOUND AFT UPPER AND MIDDLE CABIN DOOR LATCH STRIKER PLATE ECCENTRICS LOOSE CAUSISDR DXTA2024111101104Unknown · odorAPU BLEED AIR: WITH APU RUNNING - MUSTY, OILY SMELL IS NOTICEABLE IN CABIN. SMELL DISSIPATES WITH APU OFF. CORRECTIVE ACTION; INSPECTED ALL THE DUCTING AROUND THE APU AND ACMS AND WAS NOT ABLE TO FIND ANY OIL LEAKS OR ANYTHING RUBBING THAT WOULD CAUSE THE CABISDR DXTA2024091900575Pcb · failedENGINE FIRE L RED CAS: AT FL310 RED L ENG FIRE LIGHT BEGAN TO FLICKER THEN FLASH AND THEN SOLID FOLLOWED BY ENG FIRE L CAS. AFTERWARS RECEIVED AMBER FIRE DETECT FAIL L CAS. THE SEQUENCE REPEATED AT LEAST TWICE THEN CLEARED AS WE DESCENDED. CORRECTIVE ACTION: SDR DXTA2024091700550Pcb · defectiveENGINE FIRE L RED CAS: THROUGH APPROX FL 280 WE ENCOUNTERED A FLICKERING (NOT FLASHING) RED ENGINE FIRE L. SHORTLY AFTERWARDS IT EXATINQUISHED AND WE GOT A YELLOW FIRE DETECT FAIL CAS MESSAGE . THE CYCLE REPEATED ITSELF 3 -4 TIMES CORRECTIVE ACTION: REMOVED PCSDR DXTA2024020910838Battery · defectiveEMERGENCY LIGHTS DURING POWER ON CHECKLIST DO NOT WORK. REMOVED AND REPLACED FWD #1 EMERGENCY LIGHT PACK. OPS CHECICS GOOD, REF CE-700 AMM 33-50-07. BATTERY PN OFF/ON: CBS28-1 SN OFF: 008669 SN ON: 5917M, CLOSED UP ACCESS,SDR DXTA2024020610812G Switch · defectiveEMERGENCY LIGHTING: EMERGENCY LIGHT BATTERIES NOT HOLDING THEIR CHARGE. NOT WORKING ON ON OR ARM. REMOVED AFT BAGGAGE WALL TO ACCESS AFT SWITCHES/BATTERYS. R&R R/H AFT G-SWITCH G-SWITCH OPS TEST GOOD. REMOVED R/H AFT EMER BATTERY , INSTALLED A REPAIRED EMER
Reports on N837QS not matched to an aircraft · 27
They name N837QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA2017073106431Engine · overheatedDURING TAKE OFF, RIGHT ITT WENT TO APPROXIMATELY 740 DEGREES FOR ABOUT 2 SECONDS SOON AFTER LIFT OFF. IMMEDIATELY REDUCED THRUST ON RIGHT ENGINE AND ITT RETURNED TO NORMAL.SDR EBVR20170608001Wire · burnedWHEN PRESSURIZATION, THE KNOB WAS SELECTED TO ANY POSITION OTHER THAN NORMAL, THE NORMAL AND EMERGENCY PRESSURIZATION CIRCUIT BREAKERS TRIPPED. FOUND DURING POST RUN CHECKS. VERIFIED THE DAMAGED AREA ON WIRE APT022-JPA002(20) AT CONNECTOR PT022, RT BLEED AIR SDR EBVR20170606001Bracket · corrodedCORRODED AILERON QUADRANT BRACKET. REPLACED THE CORRODED AILERON QUADRANT BRACKET IAW EO ERO-896682. REV IR.
See all 27 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