- Owner type
- Co-owned, fractional ownership
- Serial number
- 700-0075
- Year built
- 2022
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- August 10, 2022
- Certificate issued
- September 17, 2026
- Expires
- September 30, 2033
- Mode S code
- AB5D80
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 N831QSMatched 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 N831QSMatched 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 · 12
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026082709424Wire Harness · faultedON THE DESCENT WE HAD A WHITE ENG CTRL FAULT L CAS MESSAGE THAT REVERTED TO AMBER ENG CTRL FAULT L UPON LANDING. REMOVED LT ENG W6 WIRE HARNESS AND REPLACED WITH NEW HARNESS IAW LMM 76-10-01. OPS CHECKED GOOD.SDR 2025FA0000833Thrust Reverser · corrodedCORROSION ON THE INSIDE SURFACE OF LH AND RH ENGINE THRUST REVERSER PIVOT DOORS AND BEAMS. REMOVED CORROSION AND VERIFIED REMAINING MATERIAL THICKNESS TO BE WITHIN TOLERANCE USING ULTRASONIC TESTING. APPLIED TREATMENT, PRIMER, AND TOP COAT AS REQUIRED BY THE MSDR DXTA2025021102281Air Filter · defectiveSMELLS IN CABIN/COCKPIT: BOTH THE CABIN AND THE COCKPIT HAVE A MUSTY SMELL ANYTIME THE APU OR ENGINES ARE RUNNING. CORRECTIVE ACTION: REPLACED HEPA FILTER. OPS CHECK GOOD. IAW CE-700 AMM 21-70-10.SDR DXTA2023121310321Unknown · unknownEMERGENCY LIGHTS DO NOT ILLUMINATE DURING POWER ON CHECK PER AOM 2.12.2.1. R & R BATTERY PACKS.SDR DXTA2023121110290Battery · inoperativeEMERGENCY EXIT LIGHTS WILL NOT TEST. NONE OF THE LIGHTS WILL ILLUMINATE UNDER THEIR OWN BATTERY POWER. COMPLIED WITH OPS CHECK OF BATTERIES IAW MM 33-50-00. OPS CHECK GOOD. FOUND DURING OPS CHECK THE LIGHTS ARE NOT TURNED IN THE SEQUENCE REMOVED COCKPIT OVERSDR DXTA2023090594380Module · defectiveL AMBER CAS: GEAR DISAGREE AMBER LRN CASS MESSAGE DISPLAYED AFTER TAKE OFF AND DURING GEAR RETRACTION. RAN QRH FOR GEAR DISAGREE CAS MESSAGE WHICH RESULTED IN PULLING EMER GEAR RELEASE HANDLE. LANDED SAFELY UNDER MAX LANDING WEIGHT. //SIGNOFF// ARES WAS UPLOADSDR DXTA2023041784380Unknown · unknownMAIN DOOR: MAIN DOOR HANDLE DIFFICULT TO LATCH. MAY REQUIRE 2 HANDS TO PULL. // SIGNOFF // GAINED ACCESS TO MED HANDLE MECHANISM AND VERIFY DISCREPANCY. DOOR HANDLE HAAD TO OPEN. REMOVE BOTH SIDE DOOR PANEL AND STEP COVER ASSY. PERFORMED DETAILED MED HANDLE ISDR DXTA2023031082360Unknown · unknownNOSE LANDING GEAR WOULD NOT RETRACT. COULD HEAR BINDING OF NOSE GEAR/ DOORS IN COCKPIT. VIBRATION FELT IN YOKE CONTROL. PERFORMED THE NOSE LANDING GEAR SQUAT SWITCH RIGGING IAW MM 32-60-00, IT WAS NOTED THAT THE SWITCH WAS 2 FULL TURNS OUT OF RIG. TECHS NOTSDR DXTA2023022781310None · noneCABIN EMERG LIGHT: EMER LIGHTS WILL NOT EXTINGUISH. *** CORRECTIVE ACTION *** RESET ALL G-SWITCHES, CHARGED EMERGENCY BATTERIES AND PERFORMED OPS CHECKS IAW CESSNA 700 AMM 33-50-00. OPS CHECKS SATISFACTORYSDR DXTA2022121976460Door · out of adjustDURING ARRIVAL INSPECTION, FOUND MCD DOES NOT DROP DOWN WHEN OPENING (FOUND BY MX) // SIGNOFF// FOUND DURING ARRIVAL INSPECTION. ADJUSTED MAIN CABIN DOOR FORWARD FRAME RUB BLOCK IA W CESSNA 700 M/M CHAPTER 52-10-15. MAIN CABIN DOOR WHEN RELEASED LATCH DROPS ANSDR DXTA2022092270900Wire · shortedCABIN DOOR OPEN AMBER CAS: WHEN CLOSING MAIN CANIN DOOR, YELLOW DOOR HANDLE LOCK LIGHT WOULD NOT EXTINGUISH. ALSO AMBER CAS CABIN DOOR OPEN WAS ILUMINATED. FOLLOWED QRH PROCEEDURE WITH NO LUCK. CHECKED WIRING AND FOUND SOLENOID INTERMITTENT. REMOVED SPLICE ANSDR 2022F00338None · chippedLH MAIN LANDING GEAR DOOR DAMAGED. ACCOMPLISHED TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ36249M1 DATED: 09/08/2022, LEFT MAIN LANDING GEAR DOOR DAMAGE (CHIPPED CORNER).
Reports on N831QS not matched to an aircraft · 14
They name N831QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR JGVR20170808001Skin · corrodedFOUND CORROSION ON EXTERNAL AREA OF THE UPPER SKIN NEAR LWS 121 AND AFT SPAR OF THE LEFT WING. REPAIRED BY BLENDING, EDDY CURRENT AND ULTRASOUND INSPECTIONS, AND INSTALLING AN EXTERNAL REPAIR DOUBLER IAW REPAIR DEFINITION S-560-0792/04RD.SDR DXTA2017010306353Brake Sys · malfunctionedDURING LANDING, RECEIVED A LOW BRAKE PRESSURE AND ANTI-SKID FAILURE LIGHTS WITH THE MASTER CAUTION LIGHT. AT FIRST HAD BRAKES THEN THEY FAILED. USED THE EMERGENCY BRAKE TO STOP. THERE WAS NO HYDRAULIC FLUID LEAKING AND NO CIRCUIT BREAKER TRIPPED. REMOVED ANSDR DXTA2016050706237Spar Cap · corrodedCORROSION ALONG RT WING UPPER SPAR CAP SURFACES. IDENTIFIED ALL CORRODED AREAS ON THE RT UPPER WING SPAR CAP & REMOVED ALL CORROSION. PERFORMED A FLUORESCENT DYE PENETRANT INSPECTION OF THE BLENDED AREAS ON RT WING UPPER SPAR CAP, FOR REMAINING CORROSION & C
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