# N818QS: 2021 Textron 700 - Status: Valid registration - Airframe: [Textron 700](https://openairdocs.org/model/textron-700) (registry code 2076819, 14 seats) - Engine: [Honeywell AS907-2-1S](https://openairdocs.org/engine/honeywell-as907-2-1s) (registry code 33403) - Data sheets: [TCDS T00015WI](https://openairdocs.org/tcds/T00015WI) (Textron Aviation Inc.), [TCDS E00010LA](https://openairdocs.org/tcds/E00010LA) (Honeywell Aerospace US LLC) (OpenAirDocs) - Serial number: 700-0055 - Year built: 2021 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 1, 2021 - Certificate issued: October 15, 2026 - Expires: October 31, 2033 - Mode S code: AB2883 - Owner type: Co-owned - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=818QS - Page: https://openairdocs.org/aircraft/N818QS From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. ## ADs that may apply (OpenAirDocs): 2 in force ### Matched by airframe (Textron 700) - [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026 - [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023 ### Matched by engine (Honeywell AS907-2-1S) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N818QS. ## FAA accident and incident reports None matched to N818QS. ## Service difficulty reports (15) As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DXTA2026073109069](https://openairdocs.org/sdr/DXTA2026073109069), Jul 30, 2026: PROXIMITY SENSOR. FAULTED. CLIMBING THROUGH 31,000 RECEIVED AMBER "CHECK DOORS" AND "CABIN DOOR OPEN" CAS MESSAGE. COMPLETED QRH AND CONTINUED TO DESTINATION. "CORRECTIVE ACTION" REMOVED - [SDR DXTA2026062908597](https://openairdocs.org/sdr/DXTA2026062908597), Jun 26, 2026: DOOR. LACK OF LUBE. VERY 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 - [SDR DXTA2026020906820](https://openairdocs.org/sdr/DXTA2026020906820), Feb 8, 2026: LIGHT. NO DISCREPANCY. NO 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 33-50-00 - [SDR DXTA2025102205387](https://openairdocs.org/sdr/DXTA2025102205387), Oct 20, 2025: FUSE. BLOWN. SEAT 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 - [SDR DXTA2025011601956](https://openairdocs.org/sdr/DXTA2025011601956), Jan 13, 2025: WHEEL. LOOSE. EXCESSIVE VIBRATION/SHUDDER WHILE BRAKING DURING LANDING. IT BECAME WORSE WHILE DECELERATING, THEN LET UP WHEN RELEASING THE BRAKES. RETORQUED #1 AND BOTH NOSE - [SDR DXTA2024043011647](https://openairdocs.org/sdr/DXTA2024043011647), Apr 29, 2024: STRIKER. OUT OF ADJUST. MAIN 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 POSITIO - [SDR DXTA2024042211579](https://openairdocs.org/sdr/DXTA2024042211579), Apr 22, 2024: BOLT. DEFECTIVE. MAIN 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 WA - [SDR DXTA2024042211558](https://openairdocs.org/sdr/DXTA2024042211558), Apr 20, 2024: HANDLE. OUT OF ADJUST. MAIN 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 WIT - [SDR DXTA2024040511396](https://openairdocs.org/sdr/DXTA2024040511396), Apr 3, 2024: WARNING MESSAGE. FALSE ACTIVATION. AFTER 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 - [SDR DXTA2024040211375](https://openairdocs.org/sdr/DXTA2024040211375), Mar 31, 2024: WIRE HARNESS. FAULTED. AT 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. REM - [SDR DXTA2024032611311](https://openairdocs.org/sdr/DXTA2024032611311), Mar 25, 2024: PROXIMITY SWITCH. OUT OF ADJUST. MAIN 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 - [SDR DXTA2024030811135](https://openairdocs.org/sdr/DXTA2024030811135), Mar 7, 2024: BAYONET. CONTAMINATED. MAIN 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. AL - [SDR DXTA2023063089900](https://openairdocs.org/sdr/DXTA2023063089900), Jun 30, 2023: UNKNOWN. UNKNOWN. CAPTAIN COCKPIT SLIDING WINDOW: CAPTAIN COCKPIT SIDE WINDOW CRACKED WHILE DESCENDING THROUGH 16,000'. REMOVED CRACKED L,H COCKPIT SIDE WINDOW AND INSTALLED NEW - [SDR DXTA2022103172990](https://openairdocs.org/sdr/DXTA2022103172990), Oct 29, 2022: PCB. INTERMITTENT. AT ALTITUDE THE FLAPS FAIL AMBER CAS MESSAGE ILLUMINATED. QRH & QRC WERE REVIEWED &COMPLETED. FLAPS 0 LANDING PREFORMED. ACCESSED ARES DATA, FOUND FLAP CONTROL - [SDR DXTA2022011054960](https://openairdocs.org/sdr/DXTA2022011054960), Jan 9, 2022: NOT REPORTED. NOT REPORTED. MAIN DOOR: SHORTLY AFTER TAKEOFF FROM KFLL, CABIN DOOR OPEN AND CHECK DOORS EICAS WAS DISPLAYED, CABIN ALSO STOPPED PRESSURIZING. //SIGNOFF //POWERED AIRCRAFT A ## Service difficulty 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 DXTA2018012400506](https://openairdocs.org/sdr/DXTA2018012400506), Jan 23, 2018: FITTING. LEAKING. ENGINE 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 WIL - [SDR JGVR20170517001](https://openairdocs.org/sdr/JGVR20170517001), May 17, 2017: LINK. CORRODED. LT 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 3 - [SDR DXTA2014040405714](https://openairdocs.org/sdr/DXTA2014040405714), Apr 3, 2014: BRAKE ASSY. MALFUNCTIONED. BRAKES CATCH & GRIND DURING ROLLOUT & COMING TO A STOP. BRAKES CATCH & GRIND DURING ROLLOUT & COMING TO A STOP. TAXI CHECKED AND VERIFIED DISCREPANCY. PERFORMED - [SDR DXTA2012121105205](https://openairdocs.org/sdr/DXTA2012121105205), Dec 11, 2012: UNKNOWN. ODOR. AT 41,000FT, A SLIGHT ELECTRICAL ODOR WAS NOTICED. WALKING TOWARDS THE BACK OF THE PLANE, THE ODOR WAS NOTICEABLY MUCH STRONGER STARTING AT THE CABIN DOOR AND M - [SDR DXTA2012031304918](https://openairdocs.org/sdr/DXTA2012031304918), Mar 12, 2012: MOTOR. INOPERATIVE. FREON AIR CONDITIONER WAS WORKING ON PREVIOUS FLIGHT. WHILE INVESTIGATING A ELETRICAL BURNING ODOR ON GROUND, DISCOVERED THE FREON AIR CONDITIONER TO BE INOPERA - [SDR DXTA2011100304740](https://openairdocs.org/sdr/DXTA2011100304740), Sep 30, 2011: BULB. INOPERATIVE. ON APPROACH EXTENDED GEAR. RECEIVED TWO GREEN AND NO RT GEAR INDICATIONS & NO RED LIGHTS. PERFORMED "LANDING GEAR WILL NOT EXTEND" CHECKLIST WHICH REQUIRES GEAR - [SDR DXTA20111004740](https://openairdocs.org/sdr/DXTA20111004740), Sep 30, 2011: INDICATION SYS. MALFUNCTIONED. GEAR EXTENDED ON APPROACH. GOT 2 GREEN AND NO RT MAIN GEAR INDICATOR BUT NO RED LIGHT. PERFORMED "LANDING GEAR WILL NOT EXTEND" CHECKLIST WHICH REQUIRES GEAR BL - [SDR DXTA2011042604563](https://openairdocs.org/sdr/DXTA2011042604563), Apr 25, 2011: INDICATOR. INACCURATE. AUTOPILOT TRANSFERRED COPILOT, PILOTS SIDE ATTITUDE INDICATOR SHOWS DISCREPANCY WITH COPILOTS SIDE. INDICATES 2.5 DEGREES LOW IN CLIMB, 1 DEGREE LOW LEVEL FLIGH - [SDR DXTA2011010304389](https://openairdocs.org/sdr/DXTA2011010304389), Jan 1, 2011: GYRO. MALFUNCTIONED. STBY GYRO DISPLAYED "EXT MANUV" ANNUNCIATOR AND SHOWED A 10 DEGREE RT BANK AND HEADING PRECESS OF MORE THAN 180 DEGREES. HEADING PRECESS ABOUT 10 DEGREES EVERY - [SDR DXTA2010091504236](https://openairdocs.org/sdr/DXTA2010091504236), Sep 14, 2010: INDICATOR. MALFUNCTIONED. AT FL410 STBY, GYRO SHOWED 6 DEGREE LT BANK, AND HEADING MISCOMPARE OF APPROX 120 DEGREES. (HEADING OF 330 THEN SLOWY MOVED TO 030). PLANE HEADING WAS 084. ALSO - [SDR DXTA2010072604172](https://openairdocs.org/sdr/DXTA2010072604172), Jul 25, 2010: SWITCH. INOPERATIVE. UPON TAXING OUT GOT LOW BRAKE PRESS/ANTISKID INOP ANNUCIATOR WITH THE POWER BRAKES CIRCUIT BREAKER POPPED. RESET, 20 SECONDS LATER THE POWER BRAKES CIRCUIT BREA - [SDR DXTA2009041403602](https://openairdocs.org/sdr/DXTA2009041403602), Apr 13, 2009: NONE. NONE. ON CLIMBOUT AND AT A FLAPS SETTING OF 7 DEGREES, A NEAR MISS CAUSED A FLAP OVERSPEED OF APPROX 40 KNOTS. COMPLIED WITH CESSNA 'OVERSPEED CHECK'. NO DEFECTS NOTE - [SDR DXTA200803139](https://openairdocs.org/sdr/DXTA200803139), Jun 23, 2008: LANDING GEAR. MALFUNCTIONED. AFTER TAKE OFF THE LANDING GEAR WOULD NOT RETRACT. THE GEAR DID NOT EVEN COME OUT OF THE LOCKS, WE HAD 3 GREEN THE ENTIRE TIME. WE CHECKED THE CB'S AND NONE WER - [SDR DXTA200803059](https://openairdocs.org/sdr/DXTA200803059), May 14, 2008: LAMP. INOPERATIVE. ON ARRIVAL, THE "LT" GEAR DOWN INDICATION LIGHT DID NOT ILLUMINATE. JACKED ACFT, RESET EMERGENCY BLOW-DOWN BOTTLE. REMOVED AIR FROM SYSTEM. FOUND ROTARY KNOB WO ## STCs that may be installed (OpenAirDocs) (11) Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do. ### Approved for the airframe (Textron 700) - [STC ST12145SE](https://openairdocs.org/stc/ST12145SE): Installation of Starlink Aviation System. AeroMech Incorporated - [STC ST04736NY](https://openairdocs.org/stc/ST04736NY): True Blue TS28 Emergency Battery Power Supply Replacement. Aerospace Design and Compliance LLC - [STC ST00415BO](https://openairdocs.org/stc/ST00415BO): Installation of an NVIS/NVG compatible lighting system and infrared capable exterior lighting. ATI Engineering Services LLC - [STC ST04575AT](https://openairdocs.org/stc/ST04575AT): Installation of the Rockwell Collins ALT-1000+/ -4000+ with 5G Filtering. Chippewa Aerospace Inc - [STC ST02812LA](https://openairdocs.org/stc/ST02812LA): Installation of the Honeywell EDG-100 Connected Engine Data Access System. Honeywell International Inc - [STC ST04572CH](https://openairdocs.org/stc/ST04572CH): Installation of an Airborne Terminal System and a Ka Radome. StandardAero Business Aviation Services LLC - [STC ST02746SE](https://openairdocs.org/stc/ST02746SE): Installation of external aerodynamic modifications, interior furnishings and equipment, including provisions for additional non-essential systems. Textron Aviation Inc - [STC ST02694SE](https://openairdocs.org/stc/ST02694SE): Group Reduced Vertical Separation Minimum (RVSM) airworthiness approval. AeroMech Incorporated - [STC ST04211NY](https://openairdocs.org/stc/ST04211NY): Installation of of NSM UNIFIS 3000 G2 Flight Inspection System. Aerospace Design & Compliance LLC - [STC ST01971WI](https://openairdocs.org/stc/ST01971WI): Installation of the Garmin G5000 Software Changes & GH-3900 Standby Configuration Updates. Textron Aviation Inc - [STC ST01027DE](https://openairdocs.org/stc/ST01027DE): Installation of MarathonNorco Aerospace Inc Nickel Cadmium battery in place of existing Nickel Cadmium main aircraft battery/batteries. MarathonNorco Aerospace Inc ## Related - Other Textron 700 aircraft: https://openairdocs.org/model/textron-700/aircraft.md - The Honeywell AS907-2-1S engine: https://openairdocs.org/engine/honeywell-as907-2-1s.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.