- Owner type
- Co-owned, fractional ownership
- Serial number
- 700-0145
- Year built
- 2025
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- August 14, 2025
- Certificate issued
- September 12, 2025
- Expires
- September 30, 2032
- Mode S code
- AC31D7
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 N885QSMatched 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 N885QSMatched 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 · 3
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026061508451Pin · lack of lubeBOTH THE INTERIOR DOOR LATCHING HANDLE AND THE EXTERIOR DOOR HANDLE REQUIRE MORE THAN NORMAL FORCE TO OPERATE (LATCHING CLOSED). THE PROBLEM IS INTERMITTENT. CORRECTIVE ACTION: PERFORMED DOOR PIN LUBRICATION IAW AMM 12-20-25. OPS CHECK GOOD, NO DEFECTS AT THISDR DXTA2025091704988Pin · out of adjustWHEN CLOSING MAIN CABIN DOOR FROM INSIDE HANDLE WILL NOT MOVE DOWN. IT IS STUCK UP. ADJUSTED FORWARD LOWER PIN ROD MECHANISM ALL WORK DONE PER CE 700 AMM 52-10-43 PERFORM SEVERAL OPERATIONAL TESTS OF THE MAIN ENTRY DOOR SUCCESSFULLY ALL WORK DONE PER CE700 AM SDR DXTA2025091604984Handle · seizedMAIN CABIN DOOR HANDLE IS SEIZING WHEN MOVING TO THE CLOSED POSITION (FROM THE INSIDE AND OUTSIDE). DOOR CLOSES COMPLETLEY BUT EXESSIVE FORCE NEEDED TO MOVE HANDLE. DOOR PINS AND PIN HOLES APPEAR NORMAL. ARRIVED ON SITE AND MET WITH CREW TO DEBRIEF. DUPLICATED
Reports on N885QS not matched to an aircraft · 6
They name N885QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA2014052205779Switch · failedDURING CLIMB, NOTICED THAT ACFT WAS NOT PERFORMING NORMALLY IN REGARDS TO DECREASED ROC & AIRSPEED. TROUBLESHOT & FOUND THAT THE SECONDARY GEAR INDICATORS SHOWED THE LT MAIN GEAR TO BE STILL DOWN & LOCKED GREEN. PRIMARY GEAR INDICATORS SHOWED ALL THREE GEAR SDR DXTA200802863Tire · failedBOTH LT MAIN TIRES BLEW UPON LANDING AND DAMAGED LT RIMS. M2B- REMOVED AND REPLACED NR 1 AND NR 2 MLG WHEEL/TIRE ASSEMBLIES AND NR 1 AND NR 2 MLG BRAKE ASSEMBLIES REF AMM 32-40-12 AND 32-40-114. REMOVED AND REPLACED NR 3 AND NR 4 MLG WHEEL/ TIRE ASSEMBLIES AS SDR DXTA200702446Brake Assy · malfunctionedWHEN APPLYING BRAKES, LT BRAKE PRESSURE INDICATES 400 TO 500 PSI HIGHER THAN THE RT BRAKE PRESSURE INDICATION. RT BRAKE FEELS SPONGY AND MORE RT BRAKE TRAVEL IS REQUIRED WHEN BRAKING BOTH PEDALS. AT 80 KNOTS ON LANDING ROLL OUT LT BRAKE INDICATED 1000 PSI AND
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