- Owner type
- Co-owned
- Serial number
- 700-0055
- Year built
- 2021
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- September 1, 2021
- Certificate issued
- October 15, 2026
- Expires
- October 31, 2033
- Mode S code
- AB2883
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 N818QSMatched 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 N818QSMatched 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 · 15
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026073109069Proximity Sensor · faultedCLIMBING THROUGH 31,000 RECEIVED AMBER "CHECK DOORS" AND "CABIN DOOR OPEN" CAS MESSAGE. COMPLETED QRH AND CONTINUED TO DESTINATION. "CORRECTIVE ACTION" REMOVED DOOR PROXIMITY SWITCH (SC002) P/N: S2800-1257, S/N: N/A, DUE TO FAULTY SWITCH CAUSING "CHECK DOORS" SDR DXTA2026062908597Door · lack of lubeVERY DIFFICULT TO SECURE FORWARD CABIN DOOR. MUST USE A LOT OF FORCE TO SECURE MAIN CABIN DOOR. VERIFIED DISCREPANCY ON MAIN CABIN DOOR; DOOR PINS FOUND DRY AND CONTAMINATED. CLEANED DOOR LATCH PINS AND PERFORMED INITIAL OPS CHECK WITH SATISFACTORY RESULTS, TSDR DXTA2026020906820Light · no discrepancyNO EMER LIGHTS ARE ILLUMINATED WHEN SWITCH IN ON POSITION. C/W MULTIPLE OPS OF THE EMERGENCY LIGHTS. OPS CHECKS ARE GOOD AT THIS TIME IAW CE-700 AMM 33-50-00SDR DXTA2025102205387Fuse · blownSEAT NR 4 EMERGENCY PATH LIGHT INOPERATIVE. REMOVED FAULTY SEAT NR 4 PATH LIGHT FUSE AND REPLACED WITH A CUSTOMER SUPPLIED NEW UNIT, OPS CHECKS.ARE GOOD AT THIS TIME. ALL WORK DONE IAW AMM 33-50-15.SDR DXTA2025011601956Wheel · looseEXCESSIVE VIBRATION/SHUDDER WHILE BRAKING DURING LANDING. IT BECAME WORSE WHILE DECELERATING, THEN LET UP WHEN RELEASING THE BRAKES. RETORQUED #1 AND BOTH NOSE WHEELS. OPS CHECK GOOD. IAW MM 32-40-05. ORIGINAL SUBMISSION DATE: 1/16/2025SDR DXTA2024043011647Striker · out of adjustMAIN DOOR HANDLE: REPEAT WRITE UP. WHEN CLOSING THE MAIN CABIN DOOR FROM INSIDE THE CABIN THE HANDLE BINDS MIDWAY WHEN LOWERING THE HANDLE TO THE CLOSED POSITION. ADJUSTED ECCENTRIC STRIKERS AS REQUIRED. VERIFIED DOOR GAPS WAS WITHIN LIMITS. VERIFIED DOOR SDR DXTA2024042211579Bolt · defectiveMAIN DOOR HANDLE: MAIN CABIN DOOR HANDLE DOES NOT WORK CORRECTLY. WHEN CLOSING DOOR AND PULLING HANDLE DOWN INTO THE LOCKED POSITION THE HANDLE BINDS UP HALF WAY THROUGH ITS NORMAL FULL TRAVEL. EVIDENCE OF METAL ON METAL RUBBING LOCATED NEAR MIDDLE RIGHT LOCKSDR DXTA2024042211558Handle · out of adjustMAIN CABIN DOOR HANDLE WILL NOT CLOSE ALL THE WAY TO SECURE THE DOOR. HANDLE TRAVELS HALF WAY THEN BINDS UP. ADJUSTED AND SERVICED LATCH DOOR IS OPERATIONAL WITH NO DEFECTS TO NOTE CURRENTLY REF CESSNA 700 AMM 12-20-15MAIN DOOR HANDLESDR DXTA2024040511396Warning Message · false activationAFTER TAKEOFF AND CLIMBING THROUGH 3,000' AMBER CAS MSGS CHECK DOORS AND CABIN DOOR OPEN LIGHTS CAME ON. NO PRESSURE LOSS WAS NOTICED AND RETURNED TO DEPARTURE AIRPORT. WHILE TAXIING BACK TO THE RAMP THE AMBER CAS MSG AUTO TEST FAIL ILLUMINATED. PERFORMED A ASDR DXTA2024040211375Wire Harness · faultedAT 3 OR 4 THOUSAND FEET CHECK DOORS AND CABIN DOOR OPEN CAS MESSAGES WERE DISPLAYED. WE RAN THE QRH CHECK AND RETUNED TO SCOTTSDALE. NO CABIN PRESSURE LOSS. REMOVED THE MAIN CABIN STAIRS TO GAIN ACCESS TO THE SC007 PROXIMITY SWITCH TO CHECK THE RIGGING AND ALSSDR DXTA2024032611311Proximity Switch · out of adjustMAIN DOOR: AFTER T/O THE CABIN DOOR OPEN AMBER CAS AND CHECK DOORS AMBER CAS MESSAGE CAME ON. CHECK LIST WAS RUN AND DOOR VERIFIED CLOSED. ELECTED TO RETURN TO DEPARTURE AIRPORT. ADJUSTED DOOR HANDLE PROX SWITCH. OPS CHECK GOOD. IAW CE-700 AMM 52-10-05SDR DXTA2024030811135Bayonet · contaminatedMAIN DOOR: MAIN DOOR WHEN CLOSING FROM INSIDE DOOR HANDLE IS NOT SMOTH CLOSING HANDLE DOWN. IT BINDS AT THE MIDDLE WHEN CLOSING IT. PLEASE EVALUATE THE DOOR. ALSO, (THERE'S A VIDEO ATTACHED TO IT.). TROUBLE SHOT DOOR FOR PROPER OPERATION AND CLEANED BULIT SDR DXTA2023063089900Unknown · unknownCAPTAIN COCKPIT SLIDING WINDOW: CAPTAIN COCKPIT SIDE WINDOW CRACKED WHILE DESCENDING THROUGH 16,000'. REMOVED CRACKED L,H COCKPIT SIDE WINDOW AND INSTALLED NEW WINDOW IAW AMM CH56-10-10SDR DXTA2022103172990Pcb · intermittentAT ALTITUDE THE FLAPS FAIL AMBER CAS MESSAGE ILLUMINATED. QRH & QRC WERE REVIEWED &COMPLETED. FLAPS 0 LANDING PREFORMED. ACCESSED ARES DATA, FOUND FLAP CONTROL WENT OFFLINE CAUSING ARINC DATA TO STOP BEING TRANSMITTED TO GSD 1 WHICH SET THE FLAP FAIL CAS MESSSDR DXTA2022011054960Not Reported · not reportedMAIN DOOR: SHORTLY AFTER TAKEOFF FROM KFLL, CABIN DOOR OPEN AND CHECK DOORS EICAS WAS DISPLAYED, CABIN ALSO STOPPED PRESSURIZING. //SIGNOFF //POWERED AIRCRAFT AND WAS ABLE TO DUPLICATE SQUAWK, GAINED ACCES
TO CMC AND VERIFIED SWITCHES OPERATION AND VENT DOOR
Reports on N818QS not matched to an aircraft · 14
They name N818QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA2018012400506Fitting · leakingENGINE CONTROL FAULT L CAS, LEFT ENGINE CONTROL FAULT CAME ON DURING FINAL APPROACH. RAN THE CHECKLIST AND WILL NOT RESET. ENGINE STUCK AT 67 PERCENT N1 AND WILL NOT IDLE ON FLARE, HAD TO SHUT DOWN ENGINE. PERFORMED LEFT ENGINE DOWNLOAD AND SENT FOR REVIEW. SDR JGVR20170517001Link · corrodedLT TRAILING LINK INNER BORE HAS LARGE AREA OF CORROSION AND AXLE IS HEAVILY CORRODED. FOUND WHILE PERFORMING TASK 32-11-02-210 MAIN LANDING GEAR INSP AND TASK 32-30-00-210 MLG TRAILING LINK INTERNAL BORE INSP. AS PART OF THE PHASE 5 INSPECTION. REMOVED AND REPSDR DXTA2014040405714Brake Assy · malfunctionedBRAKES CATCH & GRIND DURING ROLLOUT & COMING TO A STOP. BRAKES CATCH & GRIND DURING ROLLOUT & COMING TO A STOP. TAXI CHECKED AND VERIFIED DISCREPANCY. PERFORMED COMPLETE ANTI-SKID BRAKE SYSTEM BLEED, PERFORMED TAXI CHECK AND OPS AND LEAK CHECKED GOOD. BRAK
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