# N809QS: 2020 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: 700-0036 - Year built: 2020 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 13, 2020 - Certificate issued: March 17, 2026 - Expires: March 31, 2033 - Mode S code: AB04BB - Owner type: Co-owned, fractional ownership - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=809QS - Page: https://openairdocs.org/aircraft/N809QS 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 N809QS. ## FAA accident and incident reports None matched to N809QS. ## Service difficulty reports (8) 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 DXTA2026091409673](https://openairdocs.org/sdr/DXTA2026091409673), Sep 11, 2026: DOOR. FAULTED. MAIN CABIN DOOR IS EXTREMELY DIFFICULT TO LATCH AND LOCK USING EITHER THE INSIDE OR OUTSIDE LEVERS. SERVICED OPS TESTED MAIN CABIN DOOR LATCH AND LOCK WITH NO D - [SDR DXTA2025090204767](https://openairdocs.org/sdr/DXTA2025090204767), Aug 30, 2025: WIRE HARNESS. DAMAGED. AFTER GEAR RETRACTION FROM KCHS WE NOTICED A VIBRATION COMING FROM THE NOSE COMPARTMENT. THEN WE GOT THE FOLLOWING INDICATIONS GEAR CONTROL FAULT, GEAR DOOR OPE - [SDR DXTA2025080804519](https://openairdocs.org/sdr/DXTA2025080804519), Aug 7, 2025: ROD. DIRTY. MAIN DOOR HANDLE IS DIFFICULT TO OPEN FROM INSIDE THE AIRPLANE. RESEARCHED MED DOOR DESCRIPTION AND OPERATION, AND NO HISTORY FOUND CONNECTED TO THIS SQUAWK. AR - [SDR DXTA2025062003957](https://openairdocs.org/sdr/DXTA2025062003957), Jun 18, 2025: HINGE. OUT OF RIG. MAIN CABIN DOOR DID NOT OPEN WHEN LATCH WAS PULLED FROM THE OUTSIDE. PULLED OPEN DOOR MANUALLY AND GAINED ACCESS TO CABIN. CLOSED THE DOOR AND LATCHED IT. ATTEM - [SDR DXTA2025052703640](https://openairdocs.org/sdr/DXTA2025052703640), May 25, 2025: G SWITCH. FAULTED. EMERGENCY LIGHTING: EMER LIGHTS REMAINED ILLUMINATED AFTER SHUT-DOWN WITH SWITCHES IN THE OFF POSITION. COULD NOT RESET WITH THE SWITCH UNDER THE PILOTS SEATS. - [SDR DXTA2024090300386](https://openairdocs.org/sdr/DXTA2024090300386), Aug 30, 2024: LIGHT. INOPERATIVE. FLOOR EMERG EXIT LIGHT: EVACUATION PATH LIGHTING AT SEAT 5 INOP CORRECTIVE ACTION: RE-SEATED SEAT #5 PATH LIGHT ELECTRICAL CONNECTOR, OPS CHECKS NOW GOOD, REF C - [SDR DXTR2023092601](https://openairdocs.org/sdr/DXTR2023092601), Sep 26, 2023: FIRE BOTTLE. FALSE ACTIVATION. LEFT ENGINE FIRE BOTTLE SQUIB ASSEMBLIES FOUND IN OPPOSITE POSTIONS. OUR INVESTIGATATION REVEALLED THAT THE DISCHARGE OUTLET AT THE J1 POSITION CONTAINED THE SQ - [SDR DXTA2022040459630](https://openairdocs.org/sdr/DXTA2022040459630), Apr 3, 2022: NONE. NONE. EMERGENCY LIGHTING: EMER LIGHTS CAN NOT BE TURNED OFF. 5 G SWITCH RESET ATTEMPTED. NO JOY // SIGNOFF// GAINED ACCESS TO AIRCRAFT AND APPLIED APU POWER. VERIFIED ## Service difficulty reports on N809QS not matched to an aircraft (10) They name N809QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DXTA2015004076001](https://openairdocs.org/sdr/DXTA2015004076001), Apr 6, 2015: UNKNOWN. ODOR. BURNING ODOR IN COCKPIT WITH WINDSHIELD HEAT ON. ODOR IS COMING FROM BOTH SIDES. AFTER 15 MIN ENGINE RUN AT VARIOUS SETTINGS & WINDSHIELD HEAT ON HIGH. OPERATED - [SDR DXTR2014090201](https://openairdocs.org/sdr/DXTR2014090201), Sep 2, 2014: VENT LINE. CHAFED. FOUND VENT LINE ASSY TO BE WORN THROUGH AT ELBOW. R & R VENT LINE ASSY IAW SB560-28-16. - [SDR DXTA2013010205225](https://openairdocs.org/sdr/DXTA2013010205225), Dec 31, 2012: LANDING GEAR. ICED. AFTER TAKEOFF AND GEAR RETRACTION, RED GEAR UNLOCK AND HYD PRESS LIGHTS REMAINED ON. GEAR WERE EXTENDED WITH NORMAL INDICATIONS. FOUND BLOCKS OF ICE COVERING MA - [SDR DXTA2013010205226](https://openairdocs.org/sdr/DXTA2013010205226), Dec 31, 2012: INDICATION SYS. ILLUMINATED. AFTER TAKEOFF AND GEAR RETRACTION, RED GEAR UNLOCK AND HYD PRESS LIGHTS REMAINED ON. GEARS WERE EXTENDED WITH NORMAL INDICATIONS. - [SDR DXTA2009120403878](https://openairdocs.org/sdr/DXTA2009120403878), Dec 3, 2009: ACTUATOR. FAULTY. DURING DESCENT FOR LANDING, THE LANDING GEAR WAS EXTENDED AND INDICATED 2 GREEN, 1 RED. THE RT MAIN GEAR SHOWED UNLOCKED. THE "GEAR WILL NOT EXTEND" CHECKLIST W - [SDR 2008FA0000672](https://openairdocs.org/sdr/2008FA0000672), Sep 26, 2008: CHANNEL. MISLOCATED. DURING PHASE 5 INSP, FOUND ELEVATOR TRIM CABLE CONTACTING ELEVATOR SELECTOR DRIVE CHAIN. FOUND THE TRIM CABLE PULLEY CHANNEL BRACKET MIS-LOCATED. ORDERED NEW CH - [SDR DXTA200702637](https://openairdocs.org/sdr/DXTA200702637), Nov 29, 2007: DOWNLOCK SWITCH. INTERMITTENT. GEAR UNSAFE INDICATION ON LT MAIN. RECYCLED GEAR IAW ACP REQUEST STILL UNSAFE. DIVERTED, VISUAL FLY BY INSPECTION INDICATED OK. LANDED WITH NO INCIDENT. COULD N - [SDR DXTA200702621DXTA](https://openairdocs.org/sdr/DXTA200702621DXTA), Nov 20, 2007: CONNECTOR. DIRTY. LEFT MAIN MOUNT DID NOT LOCK DOWN WITH OTHER GEAR. GREEN LIGHT STAYED OFF ADN RED UNSAFE INDICATOR LIGHT ILLUMINATED FOR 15+ SECONDS. JACKED A/C PERFORMED GEAR - [SDR DXTA200702621](https://openairdocs.org/sdr/DXTA200702621), Nov 20, 2007: CONNECTOR. DIRTY. LT MAIN MOUNT DID NOT LOCK DOWN WITH OTHER GEAR. GREEN LIGHT STAYED OFF AND RED UNSAFE INDICATOR LIGHT ILLUMINATED FOR 15+ SECONDS. JACKED A/C PERFORMED GEAR SW - [SDR DXTA200702199](https://openairdocs.org/sdr/DXTA200702199), May 17, 2007: HANDLE. LACK OF LUBE. LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF AS INDICATED BY 3 GREEN, NO RED INDICATION, UPON BRINGING GEAR HANDLE TO UP POSITION. FOUND HANDLE TO BE STIFF. REM ## 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.