- Owner type
- Co-owned, fractional ownership
- Serial number
- 700-0088
- Year built
- 2023
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- March 1, 2023
- Certificate issued
- April 20, 2026
- Expires
- April 30, 2033
- Mode S code
- AB84FF
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 N841QSMatched 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 N841QSMatched 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 DXTA2026081409273Squat Switch · out of rigON DEPARTURE NOSE WHEEL GEAR WOULD NOT RETRACT . FOLLOWED THE QRH AND MANUALLY DEPLOYED THE GEAR. RIGGED SG014 SQUAT SWITCH AND TIGHTENED UPLOCK SWITCH AND PROPERLY RIGGED. SENT TIMED GEAR RETRACTION VIDEO TO MCC, OKAY WITH SIGN OFF. ALL OPS CHECKS GOOD - HSDR DXTA2026071008729Squat Switch · faultedON DEPARTURE, SELECTED GEAR UP AND RECEIVED 4-5 AMBER CAS MSGS, INCLUDING GEAR DISAGREE L N R. GEAR SHOWED AMBER DN ON NOSE, AND YELLOW HASHING ON LEFT AND RIGHT GEAR. RAN PROCEDURE AND GEAR INDICATED THREE GREEN. ONLY REMAINING CAS MESSAGE IS AMBER GROUND DETSDR 2025FA0000353Thrust Reverser · corrodedCORROSION ON THE INSIDE SURFACE OF LH AND RH ENGINE THRUST REVERSER PIVOT DOORS AND BEAMS. REMOVED CORROSION AND VERIFIED REMAINING MATERIAL THICKNESS TO BE WITHIN TOLERANCE USING ULTRASONIC TESTING. APPLIED TREATMENT, PRIMER, AND TOP COAT AS REQUIRED BY THE MSDR DXTA2025020502204Brake Assy · malfunctionedMLG BRAKE PRESSURE: EXCESSIVE FORCE MUST BE APPLIED TO BRAKE PEDALS TO STOP AIRCRAFT AFTER LANDING. BRAKES FEEL LIKE THERE IS RESISTANCE OR BACK PRESSURE. NO DIFFERENCE FROM EITHER PILOT OR CO PILOT SIDE. BEGAN TROUBLESHOOTING FAULT. POWERED A/C AND CYCLED BRASDR DXTA2024091200507Battery Pack · no testEMERGENCY LIGHTING: ALL EMERGENCY LIGHTS INTERIOR, AND EXTERIOR DO NOT COME ON DURING FIRST FLIGHT OF THE DAY TEST IN THE ON POSITION CORRECTIVE ACTION: REMOVED LH AFT EMER BATT INSTALLED REPAIRED CUSTOMER SUPPLIED EMER BATT IAW MODEL 700 AMM 33-50-05. OPS CHSDR DXTA2024070812291Battery Pack · no testEMERGENCY LIGHTS DO NOT OPERATE IN THE ARM POSITION. THE EMEGENCY LIGHTS OPERATE IN THE ON POSITION. ACCOMPLISHED THE PROCEDURE EMERGENCY LIGHTS FAIL PREFLIGHT TEST IN THE QRH. AFTER PERFORMING TC WE CALLED TEAM700 FOR INFORMATION. THEY SUGGESTED SWAPPING FWDSDR DXTA2024032211273Latch · stiffMAIN CABIN DOOR LATCH IS STIFF & DIFFICULT TO LATCH CLOSED & UNLATCH, WHETHER OPENING/CLOSING DOOR FROM INSIDE OR OUTSIDE THE ACFT. PERFORMED DOOR OPEN & CLOSE PROCEDURES & CONFIRMED MED OPEN & CLOSE IS DIFFICULT IAW AMM 52-10-00. WHILE PERFORMING A GVI TECHSSDR DXTA2024030711116Door · obstructedCABIN BEGAN DEPRESSURIZING AT APPROX 14,000' WHILE TO 17,000' . LOUD AIR SOUND LT SIDE OF ACFT DURING DEPRESSURIZATION. AMBER FOLLOWED BE RED CABIN ALT CAS. SHORTLY AFTER AMBER CHECK DOORS & MAIN CABIN DOOR CAS. AFTER LANDING, INSPECTED DOOR PINS & HANDLE POS
Reports on N841QS not matched to an aircraft · 15
They name N841QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA2015082706067Brake · odorON DEPARTURE BURNING ODOR NOTICED IN THE COCKPIT. ON LANDING, BURNING ODOR APPEARED TO BE COMING FROM RT WHEEL BRAKE. REMOVED RT MLG WHEEL ASSEMBLY, VISUALLY INSPECTED WHEEL & BRAKE ASSEMBLY IAW AMM 32-41-01-211, NO DEFECTS FOUND. PER REQUEST OF MCC PERFORMSDR DXTA2013080505465Relay · failedAFTER LANDING AND TAXIING TO RAMP, POWER BRAKES CIRCUIT BREAKER TRIPPED. RECEIVED A LOW BRAKE PRESSURE AND ANTI-SKID INOPERATIVE ILLUMINATED. NORMAL BRAKE FAILED. USED EMERGENCY BRAKE PULL TO STOP AIRCRAFT. R & R RELAY WITH A NEW UNIT. PERFORMED FUNCTION SDR DXTA2013071205443Bulb · inoperativeRIGHT SIDE LANDING LIGHT INOPERATIVE. FOUND CIRCUIT BREAKER HT008 TRIPPED. FOUND BULB BAD. R & R WITH NEW BULB IAW MM 33-42-01. OPS CHECKED NORMAL.
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