- Owner type
- Co-owned, fractional ownership
- Serial number
- 700-0028
- Year built
- 2020
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- April 29, 2020
- Certificate issued
- February 10, 2026
- Expires
- February 28, 2033
- Mode S code
- AAF5DF
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 N805QSMatched 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 N805QSMatched 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 · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026040907544Downlock · intermittentAFTER DEPARTING KMDW WHEN ATTEMPTING TO RETRACT LANDING GEAR, GEAR HANDLE WAS STUCK IN DOWN POSITION. A FEW SECONDS LATER, WE RECEIVED AN AMBER GROUND DETECT FAULT AMBER CAS MESSAGE. MESSAGE REMAINED ON FOR ENTIRE FLIGHT AND WE DID NOT ATTEMPT ANY MORE GEAR RESDR DXTA2026020906795Wire Harness · defectiveAMBER DOOR CLOSED LED ON MAIN CABIN DOOR INOP. THE AMBER DOOR LED TURNS OFF WHEN THE DOOR IS CLOSED WITH THE DOOR HANDLE IN THE OPEN POSITION. THE AMBER LED TURNS OFF WHEN THE DOOR IS ABOUT HALF WAY UP. CORRECTIVE ACTION: REMOVED HARNESS ASSY CAB DOOR THRESHOSDR DXTR2024072101Thrust Reverser · corrodedLH & RH ENGINE UPPER AND LOWER THRUST REVERSER DOORS HAVE EVIDENCE OF CORROSION.....LH & RH ENGINE UPPER AND LOWER THRUST REVERSER DOORS HAVE EVIDENCE OF CORROSION. LEFT T/R UPPER AND LOWER PIVOT DOORS INNER SURFACE PAINT REMOVED I.A.W. CITATION STANDARD PRACSDR DXTA2024011510615Battery · no testEMERGENCY LIGHTS DO NOT PASS PREFLIGHT TEST. NO LIGHTS COME ON IN THE ARM SWITCH POSITION, BUT THEY DO LIGHT IN THE ON POSITION. REMOVED AND REPLACED THE LT FWD EMERGENCY BATTERY PACK. BEFORE TECH COULD PERFORMED BATTERY CHARGING PROCEDURE ENCOUNTER BATTERYSDR DXTA2023121810346Unknown · unknownNO EMERGENCY LIGHTS ILLUMINATE WITH EMERGENCY LIGHT SWITCH IN ON POSITION. POWERED ON AC AND ALLOWED ALL SYSTEMS BOOT UP AS REQUIRED. PERFORMED OPS CHECK, OPS CHECK FAILED, CONFIRMED DISCREPANCY. ACCESSED #3 & #4 BATTERY PACKS. REPOSITIONED #3 BATTERY POWER SSDR DXTA2023062289060Unknown · unknownMAIN DOOR: REPEAT WRITEUP: AMBER CABIN DOOR OPEN CAS MESSAGE DISPLAYED DURING CRUISE FLIGHT. DOOR PINS VERIFIED TO BE CLOSED. NO NOISE OR CHANGE IN CABIN PRESSURE. ///SIGNOFF/// TECHS FOUND THAT ELECTRICAL CONNECTOR PCOSS TO BE LOOSE AND CAUSING AN INTERMITTENSDR 3J7R2023020600002Not Reported · not reportedPERFORMING THE EMERGENCY LIGHT BATTERY OPS CHECK, FOUND THAT THE EMERGENCY LIGHT SWITCH , WORKS INTERMITTENTLY. REMOVED OVERHEAD CONTROL PANEL AND INSPECTED THE SWITCH AND FOUND EMERGENCY LIGHT SWITCH WIRING CONNECTOR THAT WASNT LOCK DUE TO WORN OUT CLIP.SDR DXTA2022040459580None · defectiveEMERGENCY LIGHTS BATTERY: ON POWER ON CHECKS EMERGENCY LIGHTS DO NOT ILLUMINATE IN ARM OR ON POSITION // SIGNOFF// REMOVED FAILED #3 EMER LIGHT BATTERY P/N: CBS28-1, S/N: 000152 AND REPLACED WITH A CUSTOMER SUPPLIED REPAIRED BATTERY P/N: CBS28-1 1 S/N: 007340.SDR DXTA2022033059260Motor · defectiveMAIN DOOR: CABIN MAIN ENTRY DOOR OPENS NORMALLY THEN PAUSES AFTER 12" OF TRAVEL.. DOOR WILL MANUALLY OPEN REMAINDER OF TRAVEL//CORRECTIVE ACTION//REMOVED THE CABIN DOOR LIFT MOTOR DUE TO DOOR NOT OPENING
SMOOTHLY. INSTALLED A REPAIRED NJA SUPPLIED GEAR MOTOR SDR DXTA2022032258780None · noneCABIN EMERG LIGHT: DURING PREFLIGHT CHECKS, THE EMERGENCY LIGHTS WOULD NOT ILLUMINATE WHEN POWERED BY THE EMERGENCY BATTERIES. // SIGNOFF// PERFORMED EMERGENCY LIGHTS OPERATIONAL CHECK, NO DISCREPANCIES NOTED AT THIS TIME. ALL WORK PERFORM PER CESSNA 700 AMM 3SDR DXTA2022011054940Not Reported · not reportedMAIN DOOR: MAIN CABIN DOOR RESISTS OPENING FROM INSIDE OR OUTSIDE . REQUIRES PHYSICAL FORCE TO OPEN - DOES NOT GRAVITY FALL. // SIGNOFF// OPS CHECK DOOR AND FOUND SATISIACTORY, NO RESISTANCE OPERATING DOOR FROM INSIDE OR OUTSIDE IAW CE 700 MM 52-00-00SDR DXTA2021042641180Flap System · failedFLAPS FAIL AMBEER CAS: AMBER FLAPS FAIL CAS ILLUMINATED INFLIGHT, FLAPS WOULD NOT RESET, LANDED WITH 0 FLAPS. DOWNLOADED ARES DATA AND SENT TO TEXTRON FOR EVALUATION. HAD TO SEND EACH FILE INDUVIAL, WOULD NOT SENT MORE THAN ONE AT A TIME. ASSISTED WITH OPENSDR DXTA202101094575Battery Pack · inoperativeALL EMERGENCY LIGHTS (EXIT SIGNS, LIGHTS OVER SEATS, WING INSPECTION LIGHTS) ARE ILLUMINATED WITH ALL POWER OFF. WE TRIED TO RESET THE SWITCH UNDER PILOT'S SEAT TO NO AVAIL. RESET RT FWD EMERGENCY EXIT BATTERY PACK, LIGHTS EXTINGUISHED APPLIED POWER TO A/C.
Reports on N805QS not matched to an aircraft · 4
They name N805QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA200701870Control Valve · faultyWHEN BRAKING NOTHING HAPPENS UNTIL BRAKE HYD PRESSURE GAUGES READ 200 PSI THEN BRAKES GRAB HARD. SEEMS THE CAPTAINS BRAKE PEDALS ARE BAD, CO-PILOT'S SIDE BRAKES SEEM NORMAL.REMOVED AND REPLACED BRAKE CONTROL VALVE. ALL WORK DONE IAW MM.SDR DXTA200701851Maxaret · inoperativeWHEN BRAKING, NOTHING HAPPENS UNTIL PRESSURE GAUGE READS 200PSI THEN BRAKES GRAB HARD. THIRD WRITEUP. RECEIVED OH MAXARET P/N AC65216 S/N 58268 & NEW MAXARET P/N AC65218 THROUGH NJA SUPPLY. REMOVED AND REPLACED EXISTING MAXARET NR 1 P/N AC65218 S/N 022CJ, NR SDR DXTA200701841Brake · wornBRAKES FEEL MUSHY AFTER LANDING AND DURING TAXI. REPLACED NR 1 AND 2 BRAKE ASSEMBLIES. BLED SYSTEM. OPS CHECKED OK IAW HAWKER 800XP M.M. 32-40-00
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