# N800QS: 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: 700-0022 - Year built: 2020 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: February 28, 2020 - Certificate issued: October 1, 2025 - Expires: October 31, 2032 - Mode S code: AAE34C - Owner type: Co-owned, fractional ownership - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=800QS - Page: https://openairdocs.org/aircraft/N800QS 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 N800QS. ## FAA accident and incident reports None matched to N800QS. ## Service difficulty reports (10) 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 DXTA2024122001580](https://openairdocs.org/sdr/DXTA2024122001580), Dec 17, 2024: G SWITCH. DAMAGED. EMERGENCY LIGHTING: EMERGENCY LIGHTS WILL NOT TURN OFF. REMOVED PANEL AND RESET INTERTIAL SWITCH FOR LH AFT EMER BATTERY. HOWEVER FOUND THAT INERTIAL SWITCH WAS - [SDR DXTA2024121601528](https://openairdocs.org/sdr/DXTA2024121601528), Dec 14, 2024: BATTERY PACK. DEFECTIVE. CABIN EMERG LIGHT: PREFLIGHT CHECK OF THE EMER LTS REVEALED AN INCONSITENCY WITH SWITCH PLACEMENT. FOLLOWING A 2.5 HOUR FLIGHT AND CREW SWAP, THE LIGHTS ILLUMIN - [SDR DXTA2024110501047](https://openairdocs.org/sdr/DXTA2024110501047), Nov 3, 2024: ANTI-ICE VALVE. DEFECTIVE. AFTER LEAVING ICING CONDITIONS, SELECTED ANT-ICE OFF, WHICH LEAD TO AN AMBER CAS, L WING ANTI -ICE OVERHEAT, FOLLOWED SHORTLY AFTER BY A RED CAS L WING HOT. FOL - [SDR DXTA2024092600646](https://openairdocs.org/sdr/DXTA2024092600646), Sep 23, 2024: UPLOCK SWITCH. FAULTED. IN CRUISE AT FL410, VERY LOUD FLUTTER SOUND WAS FELT AND HEARD. THEN ABOUT 30 SECONDS LATER AN AMBER GEAR DOOR OPEN CAS MESSAGE DISPLAYED. CAS STAYED ON FOR ABO - [SDR DXTA2024011210596](https://openairdocs.org/sdr/DXTA2024011210596), Jan 12, 2024: BATTERY. FAILED. EMERGENCY LIGHTS DO NOT COME ON IN WHEN SWITCH IS SELECTED TO THE "ON" POSITION. REMOVED DEFECTIVE #4 EMERGENCY BATTERY P/N:CBS28-1, S/N:1934M AND INSTALLED A C - [SDR DXTA2024011210588](https://openairdocs.org/sdr/DXTA2024011210588), Jan 11, 2024: UNKNOWN. UNKNOWN. EMERG LIGHT SWITCH: EMERGENCY LIGHTS DO NOT WORK WHEN EMER LIGHT SWITCH IS MOVED TO THE "ON" POSITION. CHARGED BATTERIES PER THE CESSNA LETTER. BATTERIES DO NOT - [SDR 3J7R2023010300001](https://openairdocs.org/sdr/3J7R2023010300001), Jan 3, 2023: LIGHT. DIM. DURING MX NOTED RH OVERWING EMERGENCY EXIT LIGHT HAS INOP/DIM LED'S. - [SDR DXTA2021060743260](https://openairdocs.org/sdr/DXTA2021060743260), Jun 4, 2021: BATTERY. DEFECTIVE. EMERGENCY LIGHTS BATTERY: FIRST FLIGHT OF THE DAY. DURING POWER ON CHECKLIST, EMER LTS DO NOT TURN ON WHEN SWITCH IS IN THE ON POSITION OR IN THE ARM POSITION. - [SDR DXTA2020110504315](https://openairdocs.org/sdr/DXTA2020110504315), Nov 5, 2020: DOOR. UNKNOWN. MAIN CABIN DOOR IS MORE DIFFICULT THAN NORMAL TO SHUT AND OPEN. EXTRA PHYSICAL FORCE REQUIRED ON HANDLE. SIGNOFF. PERFORMED SERVERAL OPERATION OF THE CLOSING AN - [SDR DXTA2020082504021](https://openairdocs.org/sdr/DXTA2020082504021), Aug 25, 2020: PROXIMITY SWITCH. DEFECTIVE. AFTER TAKEOFF AND SELECTING THE LANDING GEAR HANDLE UP, SEVERAL LOUD BANGING NOISES WERE HEARD. MAIN GEAR INDICATIONS WERE UP, NOSE GEAR DOWN, FOLLOWED BY GEAR ## Service difficulty reports on N800QS not matched to an aircraft (6) They name N800QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DXTA200601510](https://openairdocs.org/sdr/DXTA200601510), Jul 19, 2006: THROTTLE CABLE. MISRIGGED. DURING THE CONTROLS AND SPEEDBRAKE TEST THE LT ENGINE SHUTDOWN AFTER BRINGING THE LT THROTTLE TO IDLE. FOUND LT ENGINE THROTTLE IMPROPERLY RIGGED AND ASSEMBLED, - [SDR DXTA200601234](https://openairdocs.org/sdr/DXTA200601234), Feb 7, 2006: THROTTLE CABLE. OUT OF RIG. RIGHT ENGINE SPOOLED DOWN WHILE TAXIING OFF THE RUNWAY, IT SPOOLED BACK UP WHEN THE BOOST PUMP CAME ON. SHORTLY THEREAFTER IT SPOOLED DOWN AGAIN AND QUIT COMPLE - [SDR DXTA200500892](https://openairdocs.org/sdr/DXTA200500892), Aug 8, 2005: PIPE. CHAFED. MCC REQUEST TO INSPECT LINE ASSY, (REFUEL/DEFUEL FLOW) P/N 6516311-55 (IPC 28-22-00 ITEM #156) FOR CHAFING BY FLAP CROSS OVER CABLE. REMOVED PANELS 171BB AND 17 - [SDR DXTA200500714](https://openairdocs.org/sdr/DXTA200500714), May 8, 2005: FRICTION BRAKE. MALFUNCTIONED. UPON LANDING BOTH PILOTS AND CO-PILOTS RT BRAKE PEDALS WENT SOFT. BLED AND LEAK CHECKED RT BRAKE, LEAK AND OPS CHECKS GOOD AT THIS TIME. ALL WORK DONE IAW CESSN - [SDR DXTA200400336](https://openairdocs.org/sdr/DXTA200400336), Jul 12, 2004: BULB. INOPERATIVE. RIGHT GEAR POSITION INDICATOR LIGHT SEEMS INOPERATIVE, ROTARY TEST IN FLIGHT SHOWED ONLY TWO GREEN LIGHTS. NO GEAR HORN BELOW 150 KTS UNDER 70 PERCENT N2. TROUB - [SDR CWQ2003F00004](https://openairdocs.org/sdr/CWQ2003F00004), Feb 21, 2003: BRACKET. BROKEN. DURING ROUTINE INSP OF GEAR CYCLE AND UPLOCK CHECKS NOTICED THAT RT MAIN GEAR HAD PROBLEMS IN UP AND LOCKED POSITION. UPON FURTHER INSP FOUND (PN 6521641-2) UPL ## 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.