- Owner type
- Co-owned, fractional ownership
- Serial number
- 700-0113
- Year built
- 2024
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- March 15, 2024
- Certificate issued
- April 24, 2024
- Expires
- April 30, 2031
- Mode S code
- ABD046
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 N860QSMatched 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 N860QSMatched 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 · 8
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2025100105130Structure · ground damageAIRCRAFT REPORTED DAMAGED FROM LOWERING THE AIRCRAFT WITH THE TAIL-STAND IN PLACE. AIRCRAFT REPORTED DAMAGED FROM LOWERING THE AIRCRAFT WITH THE TAIL-STAND IN PLACE. R & R FLOOR STIFFENER IAW DWG 7412694 AND SRM 51-40-05. R & R STRINGER IAW DWG 7412531 AND SDR DXTA2025093005123Handle · bindingMAIN CABIN DOOR HANDLE IS BINDING CAUSING IT TO REQUIRE EXTRA FORCE TO CLOSE FROM INSIDE CABIN. ABLE TO DUPLICATE FAULT & REMOVED THE STAIRS FROM ACFT TO GAIN ACCESS TO DOOR HANDLE INNER LINKAGES: PERFORMED A GVI THE DOOR LATCH STRIKERS FOUND THAT LT MIDDLE DSDR DXTA2025090804830Window · crackedCOCKPIT SIDE VIEW WINDOW ON CAPTAIN SIDE CRACKED DURING DESCENT AT 13,000' WITH A CABIN PSID OF 5.4. QRH 10C ACCOMPLISHED. REMOVED DAMAGED LT SIDEVIEW WINDOW. INSTALLED NEW WINDOW AND APPLIED SEALANT. APPLIED POWER TO ACFT AND ALLOWED SYSTEMS TO BOOT UP. PESDR DXTA2025082904756G Switch · trippedON LANDING IN HYA EMERGENCY LIGHTS WERE ILLUMINATED. RESET BOTH 5G SWITCHES UNDER PILOT AND COPILOT SEATS, THE EMERGENCY LIGHTS STAYED ON AND WOULD NOT EXTINGUISH UNTIL THE EMERGENCY LIGHT BATTERIES WERE DEPLETED. FOUND AFT INERTIA SWITCHES TRIPPED. GAINED ASDR DXTA2025051903503Filter · dirtyCOCKPIT ODOR: HAD A MUSTY FAINT SMELL IN THE COCKPIT WITH THE VENT OPEN ON THE LEFT PILOT SIDE. ALSO AFTER ENGINES STOPPED BACK IN THE CABIN SIMILAR SMELL LIKE A MUSTY/ HUMIDITY SMELL. CORRECTIVE ACTION; REPLACED HEPA FILTER REF. CE 700 AMM 21-70-10. NO FURTHSDR DXTA2025050903419Unknown · odorCOCKPIT ODOR: STRONG OIL TYPE ODOR IN COCKPIT AND CABIN AFTER RIGHT ENGINE START/WHEN RIGHT ENGINE RUNNING. CORRECTIVE ACTION: RAN APU AND DUPLICATED THE ISSUE. THE OIL OOOR DIMINISHED WHEN APU WAS RUNNING FOR FEW MIN BUT INITIAL WAS STRONGER. RAN RH ENGINE ASDR DXTA2025011301931Pin · dirtyAFTER CLOSING MAIN CABIN DOOR, ABNORMALLY HIGH FORCE IS REQUIRED TO MOVE THE HANDLE TO THE LOCKED POSITION. CORRECTIVE ACTION: CLEANED AND LUBED DOOR PINS. OPS CHECKS GOOD. IAW CE-700 MM 52-10-00 & 52-10-05.SDR DXTA2024112601256Handle · out of adjustCABIN DOOR OPEN CAS DOES NOT EXTINGUISH AFTER CLOSING MAIN CABIN DOOR. PERFORMED RESET PROCEDURE AND STARTUP ANOMALY CHECKLIST WITH NO EFFECT. MAIN CABIN DOOR WILL CLOSE AND THE AFTER SELECTING THE HANDLE DOWN, THE SOLENOID "CLICK" IS HEARD BUT THE AMBER LIGH
Reports on N860QS not matched to an aircraft · 6
They name N860QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA2016052006241Oil Cap · looseNR 1 ENG SHUTDOWN IN FLIGHT DUE TO LOW OIL PRESS. CLEANED RESIDUAL OIL FROM ENG & COWLING. FOUND OTBD OIL SERVICE CAP LOOSE. SERVICED ENG WITH 4 QTS MOBIL 254 OIL. RE-INSTALLED & SERVICED OIL CAP, RAN ENG. LEAK & OPERATIONS CHECKED GOOD. ALL WORK IAW AMMSDR DXTA2014091505883Uplock Switch · out of adjustABOVE 10,000 FT & ACCELERATING THRU 280 KIAS, THE LT MAIN GEAR UNSAFE RED LIGHT ILLUMINATED. SLOWING BELOW 275 KIAS THE LIGHT EXTINGUISHED. ADJUSTED DOOR LATCH ECCENTRIC BOLT TO ALLOW DOOR TO BE FULLY FAIRED WHEN IN UP AND LOCKED POSITION AND ADJUSTED UPLOCKSDR DXTR2014011301Cam · misinstalledAIRCRAFT PULLS TO THE RIGHT ON FLAT SURFACES AT ALL SPEEDS NO BRAKING. FOUND NOSE STRUT ASSEMBLED INCORRECTLY, NOSE WHEEL CENTERING CAM IS 90 DEGRESS OFF POSITION AND WOULD NOT AUTO-CENTER WHEN ACFT WAS ON JACKS. RE-ASSEMBLED LOWER STRUT IAW CMM 32-20-35.
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