OpenAirDocs.org

N810QS

Open the Markdown

2021 Textron 700 · Honeywell AS907-2-1S

Open in FAA registry

Owner type
Co-owned
Serial number
700-0044
Year built
2021
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
March 29, 2021
Certificate issued
June 25, 2026
Expires
June 30, 2033
Mode S code
AB0ACB
Textron 700Airframe model · 14 seats · 2 engines · 175 registeredTCDS T00015WIAirframe · Textron 700TCDS E00010LAEngine · Honeywell AS907-2-1S

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.

2023In forceSuperseded2026

Information bulletins that may apply

Advisory, not mandatory.

No bulletins matched this aircraft’s models

NTSB investigations

No NTSB investigations matched to N810QSMatched 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
Investigations on N810QS not matched to an aircraft · 1

They name N810QS, but no registry record covers the date, the aircraft registered then was built later, or the investigation describes another aircraft.

NTSB CEN14LA075Accident · No injuriesLimited investigationFinal reportCessna 560 · Walton, INThe inflight separation of the upper and lower right engine cowlings for reasons that could not be determined based on available evidence.Dec 2, 2013 · Substantial damage

FAA incident reports

No FAA accident or incident reports matched to N810QSMatched 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 N810QS not matched to an aircraft · 1

They name N810QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

Accident 20131202023899ACessna 560 · Grissom, INDuring descent the crew felt a slight vibration at 30,000 ft and .73 mach followed by a loud pop and slight yaw of the aircraft. ATC was notified and the aircraft continued to chicago midway airport (mdw). During the post flight walk around of the aircraft…Dec 2, 2013 · Substantial damage

Service difficulty reports · 1

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR DXTA2024120201361Switch · faultedEMERGENCY LIGHTING: AFTER LANDING NOTED ALL EMERGENCY LIGHTS WERE ON. TRIED RESET ON BOTH FRONT SWITCHES, ALL INTERIOR AND EXTERIOR EMERGENCY LIGHTS REMAINED ON. CORRECTIVE ACTION; ARRIVED AT AIRCRAFT AND RESET A.FT EMERGENCY LIGHTING INERTIA SWITCH AND PERFORDec 1, 2024 · N810QS · Textrn TEXTRON700 · Emergency Lighting
Reports on N810QS not matched to an aircraft · 14

They name N810QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

SDR DXTA2014022005659Cowling · departedDURING INITIAL DESCENT, WE NOTICED A SLIGHT VIBRATION. AT APPROXIMATELY 30000 FT & .73 MACH, WE HEARD A LOUD POP & FELT A SLIGHT YAW OF THE ACFT. WE THOUGHT A GEAR DOOR HAD DEPARTED THE ACFT & INFORMED ATC OF THAT. AUTOPILOT STAYED ENGAGED & ALL ENG INSTRUMEDec 2, 2013 · N810QS · Cessna 560CESSNA · Engine Cowling SystemSDR DXTA2013021505288Bulb · burned outDURING GEAR EXTENSION, THE LT MLG LIGHT DID NOT ILLUMINATE GREEN. COMPLETED THE LANDING GEAR WILL NOT EXTEND CHECKLIST INCLUDING THE NITROGEN BLOW DOWN. ALSO PERFORMED ROTARY TEST TO CHECK STATUS OF LT GEAR BULB, CREW DETERMINED THE BULB WAS INOPERATIVE. LAFeb 14, 2013 · N810QS · Cessna 560CESSNA · Landing Gear Position and WarningSDR DXTA2010021503983Outflow Valve · failedLEVEL AT 14,000 FT, CABIN LOST PRESSURIZATION. CABIN WAS CLIMBING AT 3,000 FPM DURING DESCENT. CABIN STAYED AT 2,000 FT UNTIL WE WERE BELOW 8,000 FT OF ALT. CABIN EVENTUALLY CAME DOWN TO FIELD PRESS. R & R PRIMARY OUTFLOW VALVE IAW MM CH 21-32-00. OPERATION Feb 15, 2010 · N810QS · Cessna 560CESSNA · Pressure Regulator/Outflow Valve

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 SystemAeroMech IncorporatedSTC ST04736NYTrue Blue TS28 Emergency Battery Power Supply ReplacementAerospace Design and Compliance LLCSTC ST00415BOInstallation of an NVIS/NVG compatible lighting system and infrared capable exterior lightingATI Engineering Services LLCSTC ST04575ATInstallation of the Rockwell Collins ALT-1000+/ -4000+ with 5G FilteringChippewa Aerospace Inc.STC ST02812LAInstallation of the Honeywell EDG-100 Connected Engine Data Access SystemHoneywell International Inc.STC ST04572CHInstallation of an Airborne Terminal System and a Ka RadomeStandardAero Business Aviation Services LLCSTC ST02746SEInstallation of external aerodynamic modifications, interior furnishings and equipment, including provisions for additional non-essential systemsTextron Aviation Inc.STC ST02694SEGroup Reduced Vertical Separation Minimum (RVSM) airworthiness approvalAeroMech IncorporatedSTC ST04211NYInstallation of of NSM UNIFIS 3000 G2 Flight Inspection SystemAerospace Design & Compliance LLCSTC ST01971WIInstallation of the Garmin G5000 Software Changes & GH-3900 Standby Configuration UpdatesTextron Aviation Inc.STC ST01027DEInstallation of MarathonNorco Aerospace Inc Nickel Cadmium battery in place of existing Nickel Cadmium main aircraft battery/batteriesMarathonNorco Aerospace Inc