- Owner type
- Co-owned, fractional ownership
- Serial number
- 700-0050
- Year built
- 2021
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- June 28, 2021
- Certificate issued
- July 29, 2023
- Expires
- July 31, 2030
- Mode S code
- AB1D5E
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 N815QSMatched 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 N815QSMatched 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 · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026050607946Wire Harness · unsecureEMERGENCY EXIT LIGHT MOUNTED ON LEFT GALLEY/PASSENGER BULKHEAD IS NOT ILLUMINATED WITH THE EMERGENCY LIGHTS SWITCH IN EITHER THE ON OR ARMED POSITION. REMOVED THE EMERGENCY EXIT LIGHT MOUNTED ON THE LEFT BULKHEAD AND FOUND THE CONNECTORS DISCONNECTED. REMOVESDR DXTA2026032407354Gps · faultedAT 45,000 FEET WE LOST GPS 2 FOR ABOUT 10 MIN. AFTER ABOUT 10 MIN WE LOST GPS 1 AND HAD CASCADING FAILURES. WE LOST THE SHAKER, PUSHER, AUTO PILOT FAILURE, AUTO THROTTLE FAILURE, TERRAIN FAILURE, AND OTHERS. ON LANDING WE HAD AUTO THROTTLE HOLD FAILURE CORRSDR DXTA2026030407101Wire Splice · damagedWHILE CLOSING THE MAIN CABIN DOOR, THE HANDLE MOVES FREELY DOESN'T FEEL LIKE THE CAMS ARE ENGAGING. THE HANDLE ALSO WILL MOVE TO THE OPEN POSITION WITHOUT PRESSING THE RED BUTTON. AND THE DOOR OPEN LIGHT WILL NOT EXTINGUISH. REMOVED AND REPLACED FAULTY MED CLSDR 2026FA0000147Thrust Reverser · corrodedR/H ENGINE UPPER TR BUCKET, LOWER TR BUCKET, AND INBD TR SIDE BRACE HAS VISIBLE CORROSION. LEVEL 2 CORROSION FOUND. ACCOMPLISHED SAFRAN REPAIR SCHEME NO. 907-623 REV. B DATED: 01/03/2024.SDR 2026F00017Brace · corrodedLEFT ENGINE UPPER THRUST REVERSER BUCKET. LOWER THRUST REVERSER BUCKET, AND OTBD THRUST REVERSER SIDE BRACE HAD VISIBLE CORROSION. LEVEL 2 CORROSION FOUND. ACCOMPLISHED REPAIR SCHEME NR 907-623 REV. B .SDR DXTA2026013006692Antenna · defectiveWHILE DESCENDING FROM 9000 TO 8000 THE GEAR WARNING HORN AND THE RED CAS LANDING GEAR AND RED MASTER WARNING FLASHED AND THE GEAR INDICATIONS WERE RED. THIS CONTINUED UNTIL WE WERE LEVEL AT 8000 AT WHICH POINT IT SAID "10".. FURTHER DESCENT TO 6000 IT STARTED SDR DXTA2026012106619Light Sys · malfunctionedFORWARD CABIN EMERGENCY EXIT LIGHT NOT ILLUMINATING IN THE AUTO POSITION. PERFORMED EMERGENCY LIGHTING ADUSTMENT/TEST IAW MM 33-50-00. ALL EMERGENCY LIGHTS OPERATING NORMALLY.SDR DXTA2025112405789Monitoring Unit · unserviceableAFTER TAXING IN AND SHUTTING DOWN THE ENGINES, WITH THE APU ONLINE. WE COULD NOT OPEN THE MAIN CABIN DOOR. THE AIRCRAFT WAS NOT PRESSURIZED AND NO DOOR STATUS LIGHTS WERE ILLUMINATED. THE INTERIOR DOOR HANDLE COULD NOT BE MOVED FROM THE LOCKED POSITION. WE HADSDR DXTA2024082900370Sign · inoperativeEMERG EXIT SIGN/LIGHT: WITH EMER LTS SWITCH IN THE ARM POSITION AND THE PAX SAFETY SWITCH ON, THE EXIT SIGN LIGHT ON THE LEFT FORWARD CABIN BULKHEAD DOES NOT ILLUMINATE. WITH THE EMER LTS SWITCH IN THE ON POSITION, THE SAME EXIT SIGN LIGHT DOES ILLUMINATE. COSDR DXTA2024070812287Battery Pack · no testEMERGENCY LIGHTS FAIL PREFLIGHT TEST. BATTERY WILL CHARGE AFTER ACCOMPLISHING QRH PROCEDURE BUT IS DEAD THE NEXT DAY AFTER AIRCRAFT IS PARKED OVERNIGHT. DUE TO THE EMERGENCY LIGHTS FAILING PREFLIGHT TEST ALL FOUR EMERGENCY LLGHT POWER SUPPLIES WERE REMOVED SDR DXTA2024030711123Striker · out of rigMAIN ENTRY DOOR HANDLE IS DIFFICULT TO MOVE INTO THE DOOR CLOSED POSITION FROM INSIDE THE CABIN. OPERATIONAL CHECK WAS NOT SATISFACTORY THE TECH INSPECT THE DOOR WITH SATISFACTORY RESULT THE TECH NOTED THE DOOR LATCH STRIKERS NEED RJGGING, THE TECH RIGGED AS
Reports on N815QS not matched to an aircraft · 13
They name N815QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA2014041605732Deec · malfunctionedDURING INITIAL CLIMB, CREW FELT LATERAL YAW, NOTICED RT N1 SURGING 3 OR 4 PERCENT. DIMINISHED AT MID POWER SETTING BUT STILL SLIGHTLY NOTICEABLE. CREW DECLARED AN EMERGENCY & RETURNED TO DEPARTURE. ENGINE INDICATIONS ONLY, NO ANNUNCIATOR LIGHTS ILLUMINATEDSDR DXTA2013053105405Aileron Sys · lack of lubeDURING GROUND FLIGHT CONTROL CHECK, AIRLERON MOVEMENT APPEARED STIFF BETWEEN MID TO FULL TRAVEL. INFLIGHT, THE STIFFNESS INCREASED SPECIFICALLY WHEN ROLLING TO THE RT. PROBLEM DETECTED WHILE AUTOPILOT WAS SELECTED OFF. INSPECTED AND LUBED AILERON PULLEYS ASDR DXTA2012120705202Reservoir · underservicedACFT NORMAL BRAKING SYSTEM INOPERATIVE. DURING TAXI OUT BRAKES WERE VERY MUSHY AND HAD MINUMAL PRESSURE. WITH EITHER THE CAPT BRAKES APPLIED OR THE CO-PILOTS BRAKES APPLIED THE PEDDLES WOULD GO TO THE STOPS AND ONLY HAVE APPROX 400 PSI MAX PRESSURE. AUX BRAKI
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