# N807QS: 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: 700-0032 - Year built: 2020 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 1, 2020 - Certificate issued: December 29, 2025 - Expires: December 31, 2032 - Mode S code: AAFD4D - Owner type: Co-owned, fractional ownership - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=807QS - Page: https://openairdocs.org/aircraft/N807QS 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 N807QS. ## FAA accident and incident reports None matched to N807QS. ## Service difficulty reports (12) 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 DXTA2026031307207](https://openairdocs.org/sdr/DXTA2026031307207), Mar 10, 2026: STRUT. STUCK. ON DEPARTURE GEAR RETRACTION HANDLE WOULD NOT MOVE TO GEAR UP POSITION. ON THIRD TRY HANDLE MOVED TO GEAR UP POSITION BUT AMBER CAS MESSAGES BEGAN TO POPULATE O - [SDR DXTA2025080804502](https://openairdocs.org/sdr/DXTA2025080804502), Aug 6, 2025: DOOR. NO DISCREPANCY. MAIN CABIN DOOR BECOMING VERY DIFFICULT TO LATCH CLOSED. ARRIVED TO THE A/C IN ATTEMPT TO DUPLICATE THE FAULT, CONNECTED THE A/C BATTERIES, CLOSED THE MED FROM - [SDR DXTA2025071104202](https://openairdocs.org/sdr/DXTA2025071104202), Jul 10, 2025: PCB. FAULTED. AFTER LANDING AND SHUTTING ENGINES OFF, MAIN CABIN DOOR WOULD NOT OPEN. NOTHING HAPPENED WHEN PUSHING THE RED BUTTON. WE ENDED UP TURNING THE BATTERIES TO OFF A - [SDR DXTA2025041503100](https://openairdocs.org/sdr/DXTA2025041503100), Apr 14, 2025: BATTERY. DEFECTIVE. WHEN TESTING EMERGENCY LIGHTS IN ARM POSITION, LIGHTS DO NOT ILLUMINATE. ACCOMPLISHED QRH 25X PROCEDURE TO CHARGE THE BATTERY PACK AND LIGHTS OPERATED NORMALLY - [SDR DXTA2024021210854](https://openairdocs.org/sdr/DXTA2024021210854), Feb 9, 2024: BATTERY. DEFECTIVE. CABIN EMERG LIGHT: EMER LTS NOT HOLDING CHARGED. CHARGE AMD STILL NOT HOLDING CHARGE. //SIGNOFF// WE PERFORMED THE EMERGENCY BATTERY EXERCISE PROCEDURE AND FOUN - [SDR DXTA2023071991280](https://openairdocs.org/sdr/DXTA2023071991280), Jul 19, 2023: UNKNOWN. UNKNOWN. UNABLE TO CLOSE MAIN CABIN DOOR FROM INSIDE OR OUTSIDE. MAIN HANDLE WILL NOT CLOSE, IT FEELS JAMMED. GAINED ACCESS TO DOOR INTERNALS. FOUND UPPER AFT LATCH PIN - [SDR DXTA2023071490840](https://openairdocs.org/sdr/DXTA2023071490840), Jul 13, 2023: UNKNOWN. UNKNOWN. UNABLE TO CLOSE MAIN CABIN DOOR FROM INSIDE OR OUTSIDE. 4 PINS ARE COMPLETELY RECESSED AND ARE STOPPING MAIN DOOR HANDLE TO MOVE. REINSTALLED DOOR PIN, CLEANED - [SDR DXTA2023042684900](https://openairdocs.org/sdr/DXTA2023042684900), Apr 25, 2023: UNKNOWN. UNKNOWN. MAIN DOOR HANDLE: MAIN DOOR HANDLE IS JAMMED WILL NOT MOVE TO LOCK POSITION. EVEN WITH DOOR OPEN HANDLE WILL NOT MOVE FREELY. ///SIGN-OFF/// REMOVED STEPS AND I - [SDR DXTA2022062364470](https://openairdocs.org/sdr/DXTA2022062364470), Jun 22, 2022: BATTERY. DEFECTIVE. EMERGENCY LIGHTING: WHEN EMER LTS SWITCH IS PLACED TO THE ARM POSITION, NO LIGHTS ILLUMINATE, WHEN PLACED ON, ALL LIGHTS ILLUMINATE.//CORRECTIVE ACTION//REMOVED - [SDR DXTA2022060863530](https://openairdocs.org/sdr/DXTA2022060863530), Jun 8, 2022: SWITCH. LOOSE. EMERG LIGHT SWITCH: EMER LIGHTS DO NOT ILLUMINATE IN THE ARMED POSITION. THEY DO COME ON IN THE ON POSITION. SWITCH IS LOOSE IN PANEL. PERFORMED VARIOUS SUCCESS - [SDR DXTA2022051761910](https://openairdocs.org/sdr/DXTA2022051761910), May 16, 2022: SWITCH. INTERMITTENT. CABIN EMERG LIGHT: EMERGENCY LIGHTING SYSTEM FAILS TO TEST PROPERLY ON PREFLIGHT. ALTHOUGH THEY INITIALLY ALL ILLUMINATE PROPERLY WHEN SELECTING THEM TO "ARM" W - [SDR DXTA2022051661790](https://openairdocs.org/sdr/DXTA2022051661790), May 14, 2022: BATTERY. ABNORMAL. CABIN EMERG LIGHT: CABIN EMERGENCY LIGHTS FLICKER AND EXTINGUISH WHEN TESTING. ONCE SHIPS POWER IS APPLIED EMERGENCY LIGHTS WORK FINE. ONCE SHIPS BATTERIES ARE ## Service difficulty reports on N807QS not matched to an aircraft (15) They name N807QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DXTR2017042701](https://openairdocs.org/sdr/DXTR2017042701), Apr 27, 2017: STINGER. CORRODED. THE STINGER ASSY HAS CORROSION ON THE OUTER SKIN AT THE 6 O’CLOCK POSITION. - [SDR DXTA2014070905815](https://openairdocs.org/sdr/DXTA2014070905815), Jun 22, 2014: RIB. CRACKED. CRACK NOTED AT LT & RT WING RIB STATION 133.07 FLAP BAY. REPAIRED LT & RT WING TE RIB AT WS 133.07 IAW AQRD ERO-586871. - [SDR DXTA2013012205254](https://openairdocs.org/sdr/DXTA2013012205254), Jan 21, 2013: DUCT. DISLODGED. ONE HOUR INTO CRUISE AT FL410, DETECTED AN UNDEFINED ODOR. TEMP SELECTOR WAS IN 11:00 POSITION. THE LT SIDE OF THE CABIN WAS NOTICEABLY WARMER THAN THE RT SIDE. - [SDR DXTA2012112605193](https://openairdocs.org/sdr/DXTA2012112605193), Nov 25, 2012: SQUAT SWITCH. OUT OF ADJUST. DURING CLIMBE, PLACED GEAR HANDLE IN THE UP POSITION, AND GEAR WOULD NOT RETRACT, SHOWED RED "GEAR UNLOCKED" LIGHT. THREE GREEN PLUS THE RED. AFTER ABOUT 30 SEC - [SDR DXTA2012111905186](https://openairdocs.org/sdr/DXTA2012111905186), Nov 18, 2012: SWITCH. STICKING. TO START THE SEQUENCE OF GEAR RETRACTION, HAVE TO JIGGLE THE GEAR HANDLE IN ITS UP POSITION. FOUND GEAR HANDLE UP SWITCHES TO BE STICKING. REMOVED DME INDICATOR - [SDR DXTA2011011104404](https://openairdocs.org/sdr/DXTA2011011104404), Jan 8, 2011: CONNECTOR. CONTAMINATED. ON GEAR RETRACTION AFTER TAKEOFF, GEAR UNLOCKED LIGHT REMAINED ILLUMINATED. INSPECTED GEAR, NO DEFECTS NOTED. CHECKED RIGGING ON UPLOCK SWITCHES & FOUND DEBRIS - [SDR DXTA2010061504123](https://openairdocs.org/sdr/DXTA2010061504123), Jun 14, 2010: BULB. INOPERATIVE. THE LT MAIN "DOWN AND LOCKED" LIGHT WOULD NOT ILLUMINATE. R & R BULB ON LT GEAR DOWN LOCK ANNUNCIATOR. PERFORMED LANDING GEAR FUNCTIONAL CHECK AND FULL HYD SYS - [SDR DXTA2009100803808](https://openairdocs.org/sdr/DXTA2009100803808), Oct 7, 2009: MOTOR. ARCED. AFTER UNLOADING PASSENGER BAGGAGE IN THE AFT BAGGAGE COMPARTMENT, I NOTICED A BURNING ODOR. OPENED THE HELL HOLE. IT WAS EITHER AN ELECTRICAL OR RUBBER ODOR. WE - [SDR DXTA20082884](https://openairdocs.org/sdr/DXTA20082884), Feb 16, 2008: ENGINE. POWER LOSS. ATTEMPTED A STATIC T/O AND THE RT ENG DIDN'T MAKE THE COMPUTED T/O PWR WITH FULL THROTTLE TRAVEL. IT WAS 2 PERCENT SHORT OF THE REQUIRED 92.2 PERCENT AT 0 DEG C - [SDR DXTA200802862](https://openairdocs.org/sdr/DXTA200802862), Feb 10, 2008: ENGINE. OVERTEMP. RT ENG WOULD NOT ATTAIN POWER WITHOUT EXCEEDING ITT AND N2 LIMITS. TAKE OFF ABORTED. REPLACED RT ENGINE WITH REPAIRED UNIT AND REPLACED RT BDV CONTROLLER WITH R - [SDR DXTA200802824](https://openairdocs.org/sdr/DXTA200802824), Feb 3, 2008: GASKET. LEAKING. DURING TAKEOFF ROLL, RT ENGINE ITT CLIMBED TO 700 DEG WHERE AS LT ENGINE STABILILZED AT 650 DEG ABORTED TO ROLL. CONFIRMED RT ENGINE TO GO UP TO 700 DEGREES AND - [SDR DXTA200701973](https://openairdocs.org/sdr/DXTA200701973), Feb 27, 2007: STRUT. BINDING. AFTER T/O THE GEAR WOULD NOT RETRACT. INDICATIONS WERE THREE GREEN, UNSAFE DOOR LIGHT AND GEAR HANDLE UP-GEAR HANDLE WAS PLACED BACK DOWN AND WE HAD THREE GREEN - [SDR DXTA200501061](https://openairdocs.org/sdr/DXTA200501061), Nov 4, 2005: BULB. BURNED OUT. RT MAIN LANDING GEAR LIGHT WOULD NOT ILLUMINATE. FOLLOWED EMERGENCY CHECKLIST PRIOR TO LANDING. BLEW DOWN W/ EMERGENCY PNEUMATIC AIR. ROTARY TEST VERIFED LIGHT - [SDR DXTA200400218](https://openairdocs.org/sdr/DXTA200400218), Jan 16, 2004: FUSIBLE PLUG. BLOWN. AFTER LANDING DURING TAXI, THE FUSIBLE PLUGS BLEW ON THE RT MAIN TIRE. REMOVED AND REPLACED RT MAIN WHEEL AND BRAKE ASSEMBLIES IAW CESSNA 560 MM CHAPTER 32-41-0 - [SDR DXTA200300003](https://openairdocs.org/sdr/DXTA200300003), Jan 6, 2003: CIRCUIT BOARD. FAILED. DURING DESCENT FROM 35,000, THE EMERGENCY PRESSURIZATION CAME ON AT ABOUT 18,000 AT 10 DEG AND STAYED ON FOR 3-4 SECONDS. ## 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.