- Owner type
- Co-owned
- Serial number
- 700-0052
- Year built
- 2021
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- July 29, 2021
- Certificate issued
- June 25, 2026
- Expires
- June 30, 2033
- Mode S code
- AB24CC
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 N817QSMatched 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 N817QSMatched 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 N817QS not matched to an aircraft · 1
They name N817QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
Service difficulty reports · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026082809442Light · faultyTHE PATHWAY EMERGENCY LIGHT ON THE BASE OF SEAT 9 IS INOP. REMOVED CABIN LIGHT ASSY, INSTALLED NEW CABIN LIGHT ASSY. OPS CHECK GOOD. WORK PERFORMED IAW IMM 25-20-00SDR 2023FA0000460Thrust Reverser · corrodedPROCEDURE TO REPAIR CORROSION DAMAGE AND RESTORING SURFACE PROTECTION ON THE BEAM INNER SKIN. REPAIR SCHEME NO. RS907-623 REV. ASDR DXTA2023062289110Battery · defectiveWITH MAIN BATTERIES CONNECTED AND BATTERIES OFF, EMER LIGHTS - ARM DOES NOT ILLUMINATE ANY EMERGENCY LIGHTS. WITH EMER LIGHTS - ON, ALL LIGHTS ILLUMINATE WITH THE EXCEPTION OF RIGHT WING INSPECTION LIGHT//CORRECTIVE ACTION//REMOVED AND REPLACED #1AND #2 EMERGESDR DXTA2023060888170Unknown · unknownEMERG EXIT SIGN/LIGHT: WITH BATTERIES OFF AND EMER SWITCH IN ARMED THERE ARE NO LIGHTS COMING ON. WHEN THE EMER SWITCH IS FLIPPED TO THE ON POSITION THE LIGHTS ILLUMINATE AS PRESCRIBED. PERFORMED EMERGENCY LIGHTING POWER SUPPLY BATTERY EXCERCISE PROCEDURE IASDR DXTA2023032082790Harness · damagedEXTENSION / RETRACTION: AFTER TAKEOFF LANDING GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. AT APPROXIMATELY 400' AMBER GROUND DETECT FAULT CAS ILLUMINATED FOLLOWED BY WHITE ENG CTRL FAULT L/R. PERFORMED QRH PROCEDURES FOR GROUND DETECT FAULT AND LANDING GEASDR DXTA2022050661330Hinge · brokenMAIN DOOR: MAIN CABIN DOOR TOP MOST STEP IS ELEVATED ABOUT 1 INCH ABOVE FLUSH. DEFINITE TRIP HAZARD. PICS ATTACHED. INSPECTED STEP RISER HINGES AND NOTED ALL THREE ARE BROKEN. REPLACED STEP HINGES PER CESSNA CE700 MM 52-10-05. DOOR OPS CHECK GOOD.
Reports on N817QS not matched to an aircraft · 12
They name N817QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA2011022804480Check Valve · failedACFT FAILED TO PRESSURIZE EVENLY; ALT WARNING HORN SOUNDED AND MASKED FELL AS WE CLIMBED THOUGH FL200. AFTER EMERGENCY DESCENT, APU WAS REENGAGED BUT EVEN THEN ALT WARNING HORN STAYED ON UNTIL BELOW 8000FT; AND BOTH CREW CONFIRMED ONGOING PRESSURE FLUCTUATIONSSDR DXTA2010090904228Transducer · fluctuatesNR 2 ENG SHUTDOWN IN FLT DUE TO FLUCTUATION OF N1, N2, & FUEL FLOW. FLUCTUATIONS INCREASED AS POWER DECREASED. PRIOR TO SHUTDOWN, ENG FLUCTATED 75-95 % N1. A SMALL FLUCTUATION OBSERVED AFTER DEPARTURE. ENG NORMAL TO FL 400. INSPECTED INLET & EXHAUST FOUND NO DSDR DXTA2010030104009Computer · failedELECTRIC PITCH TRIM WENT FULL NOSE DOWN WHEN LEVEL AT 38000. ELECTRIC PITCH TRIM CIRCUIT BREAKER WAS PULLED. ELECTRIC PITCH MOTOR CONTINUED TO RUN WITH CIRCUIT BREAKER PULLED. WERE ABLE TO OVER-POWER THE MOTOR AND MAINTAIN CONTROL OF THE ACFT. DESCENDING T
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