# N804QS: 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: 700-0027 - Year built: 2020 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: March 13, 2020 - Certificate issued: August 7, 2025 - Expires: August 31, 2032 - Mode S code: AAF228 - Owner type: Co-owned, fractional ownership - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=804QS - Page: https://openairdocs.org/aircraft/N804QS 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 N804QS. ## FAA accident and incident reports None matched to N804QS. ## 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 DXTR2024101901](https://openairdocs.org/sdr/DXTR2024101901), Oct 19, 2024: PANEL. CORRODED. APU PANEL 331CR CONTAINS LEVEL 2 CORROSION. ACCOMPLISHED MINOR PERMANENT REPAIR IAW AQRD RFTS-11996 DATED OCT 19/2024. - [SDR DXTA2024081200190](https://openairdocs.org/sdr/DXTA2024081200190), Aug 11, 2024: LIGHT. MALFUNCTIONED. LAV EMERG LIGHT: LAV AFT OVERHEAD EMER LIGHT INOP WHEN PERFORMING EXPANDED POWER ON CHECKLIST. THIS LIGHT WILL ILLUMINATE IF EMER LIGHTS ARE SELECTED ON OR IF T - [SDR DXTA2023081192740](https://openairdocs.org/sdr/DXTA2023081192740), Aug 11, 2023: WINDOW. DAMAGED. FIRST OFFICER COCKPIT WINDOW: DURING PREFLIGHT, WE NOTICED THE COPILOT SIDE WINDOW IS SHATTERED. ALSO NOTED THERE ARE SMALL GLASS SLIVERS IN THE COPILOT (RIGHT) - [SDR DXTA2023032883370](https://openairdocs.org/sdr/DXTA2023032883370), Mar 28, 2023: UNKNOWN. UNKNOWN. EMERGENCY LIGHTS WILL NOT ILLUMINATE DURING PREFLIGHT SELECTION OF ARM [PREFLIGHT]. GAINED ACCESS TO THE A/C, PERFORMED EMERGENCY LIGHTS 5 G SWITCH OPERATIONAL - [SDR DXTA2023021780610](https://openairdocs.org/sdr/DXTA2023021780610), Feb 16, 2023: BATTERY. DEFECTIVE. EMERGENCY LIGHTING: THE EMERGENCY BATTERY PACK THAT POWERS INTERIOR EMERGENCY LIGHTS AND THE RIGHT WING INSPECTION LIGHTS DOES NOT HOLD POWER OVERNIGHT. - [SDR DXTA2021090748350](https://openairdocs.org/sdr/DXTA2021090748350), Sep 5, 2021: BATTERY PACK. DISCHARGED. EMERGENCY LIGHTING: UPON TESTING EMERGENCY LIGHT SYSTEM , LIGHTS FLASHED MOMENTARILY AND THEN ALL EMERGENCY LIGHTING EXTINGUISHED. ARRIVED AT AIRCRAFT AND PERFO - [SDR DXTA2021032239810](https://openairdocs.org/sdr/DXTA2021032239810), Mar 22, 2021: PROXIMITY SWITCH. INOPERATIVE. MAIN DOOR: MAIN CABIN DOOR IS VERY DIFFICULT TO OPEN AND CLOSE FROM INSIDE. "CORRECTIVE ACTION" REMOVED THE PAWL PROX SWITCH SC007 PN S2800-1257, NSN AND INSTAL - [SDR DXTA2021012204638](https://openairdocs.org/sdr/DXTA2021012204638), Jan 22, 2021: WIRE HARNESS. DEFECTIVE. UNABLE TO EXTINGUISH AMBER CABIN DOOR OPEN CAS MESSAGE. DOOR HANDLE STIFF TO OPERATE AND DOES NOT FEEL FULLY SEATED WHEN CLOSED. THE AUDABLE SOUND OF THE LOCKIN ## Service difficulty reports on N804QS not matched to an aircraft (18) They name N804QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DXTA2014021705655](https://openairdocs.org/sdr/DXTA2014021705655), Feb 15, 2014: BLEED VALVE. MALFUNCTIONED. WHILE LEVELING OFF AT 6000 FEET, LT ENG BEGAN TO VIBRATE, N1 BEGAN TO DECREASE, ITT INCREASED TO APPROXIMATELY 650 DEGREES. ITT DECREASED WITH POWER LEVER RETRA - [SDR DXTA2013011805248](https://openairdocs.org/sdr/DXTA2013011805248), Jan 17, 2013: STRUT. LEAKING. AFTER TAKEOFF, GEAR DID NOT RETRACT. THREE GREEN GEAR LIGHTS, ONE RED GEAR UNSAFE LIGHT, ANTI-SKID LIGHT AND THE BRAKE LOW PRESSURE LIGHT, REMAIN ILLUMINATED FO - [SDR CWQR20120914050](https://openairdocs.org/sdr/CWQR20120914050), Sep 14, 2012: DRAG ANGLE. CRACKED. DURING A SCHEDULED INSPECTION, FOUND RT WING TO FUSELAGE FAIRING DRAG ANGLE THAT ATTACHES TO THE WING, WAS CRACKED AT THREE FASTENER LOCATIONS. - [SDR CWQR20120914049](https://openairdocs.org/sdr/CWQR20120914049), Sep 14, 2012: DRAG ANGLE. CRACKED. DURING A SCHEDULED INSPECTION, FOUND THE LT WING TO FUSELAGE FAIRING DRAG ANGLE THAT ATTACHES TO THE WING, WAS CRACKED A 3 FASTENER LOCATIONS. - [SDR CWQR20120215006](https://openairdocs.org/sdr/CWQR20120215006), Feb 15, 2012: LINE. CHAFED. WHILE PREFORMING THE INSPECTION FOR SL560-28-09, FOUND FITTING CHAFED ON FUEL LINE. AFTER REMOVAL OF THE FUEL LINE ASSY, FOUND THAT THE FITTING CLAMP ANTI-ROTAT - [SDR CWQR20120210003](https://openairdocs.org/sdr/CWQR20120210003), Feb 10, 2012: LINE. CHAFED. WHEN ACCOMPLISHING SL560-28-09, FOUND FUEL LINE CHAFED ON FUEL BAY STRUCTURE IN THE LT WING, IT WAS MORE THAN 60 PERCENT CHAFED THROUGH. THE WING STRUCTURE SHOW - [SDR DXTA2011120604816](https://openairdocs.org/sdr/DXTA2011120604816), Dec 5, 2011: CONNECTOR. LOOSE. ON FINAL APPROACH, MLG SELECTED DOWN. DID NOT HEAR SOUNDS ASSOCIATED WITH MLG DOWN. RED MLG UNSAFE LIGHT ILLUMINATED ONLY. AFTER 20 SECONDS, NLG SHOWED DOWN & L - [SDR CWQR20110426001](https://openairdocs.org/sdr/CWQR20110426001), Apr 26, 2011: ANGLE. CRACKED. WHILE ACFT WAS IN A SCHEDULED INSP, DISCOVERED THE FWD Z ANGLE THAT THE UPLOCK IS ATTACHED TO WAS CRACKED. THE CRACKS WERE LOCATED IN THE OTBD ENDS OF THE BEND - [SDR DXTA2010050304083](https://openairdocs.org/sdr/DXTA2010050304083), Apr 30, 2010: GROUND WIRE. BROKEN. AFTER DEPARTURE, RED GEAR UNLOCKED LIGHT FAILED TO EXTINGUISH AFTER GEAR HANDLE WAS SELECTED IN THE UP POSITION. HYD SYS PRESSURE LIGHT REMAINED ILLUMINATED. 3 - [SDR 2009FA0000953](https://openairdocs.org/sdr/2009FA0000953), Nov 6, 2009: DISPLAY. INOPERATIVE. LT SEAT PILOTS PFD - BLANKED OUT AT APPROX 50 KTS ON TAKEOFF ROLL - (ABORTED TAKE OFF). PFD CAME BACK ON DURING ROLLOUT OF ABORT AND WORKED AGAIN UNTIL SHUTDOWN - [SDR DXTA2009051803658](https://openairdocs.org/sdr/DXTA2009051803658), May 15, 2009: LAMP. INOPERATIVE. WHEN MLG SELECTED DOWN FOR LANDING , LT MLG INDICATOR LIGHT DID NOT ILLUMINATE. NO MLG UNSAFE INDICATION NOTED. PERFORMED MLG WILL NOT EXTEND CHECKLIST. LT & RT - [SDR DXTA200702561](https://openairdocs.org/sdr/DXTA200702561), Oct 22, 2007: OUTFLOW VALVE. INOPERATIVE. PRESSURIZATION WORKED NORMALLY UP TO FL 310 BETWEEN FL 310 AND FL 320 THE CABIN STARTED TO RAPIDLY CLIMB AT A RATE OF 5500 FPM. THE CABIN BEFORE THE CLIMB WAS A - [SDR CWQR200712](https://openairdocs.org/sdr/CWQR200712), Aug 13, 2007: INTAKE DUCT. CRACKED. DURING A PHASE INSPECTION FOUND RT ENGINE INLET DUCT ASSY CRACKED. CRACKS WERE FOUND ON THE AFT PORTION OF THE INLET DUCT ASSY THROAT. THIS UNIT HAD TO BE RETUR - [SDR CWQR200711](https://openairdocs.org/sdr/CWQR200711), Aug 13, 2007: INTAKE DUCT. CRACKED. DURING A PHASE INSPECTION FOUND LT ENGINE INLET DUCT ASSY CRACKED. CRACKS WERE FOUND ON THE AFT PORTION OF THE INLET DUCT ASSY THROAT. THIS UNIT HAD TO BE RETUR - [SDR CWQR200710](https://openairdocs.org/sdr/CWQR200710), Aug 8, 2007: FORK. LOOSE. DURING A MAINTENANCE TAXI CHECK NOTICED SHIMMY FROM NOSE GEAR. UPON DISASSEMBLY FOUND FORK LOOSE ON NOSE GEAR PISTON, THIS SHOULD BE A PRESS FIT FROM THE FACTOR - [SDR DXTA200601684](https://openairdocs.org/sdr/DXTA200601684), Oct 25, 2006: FUEL CONTROL. FAILED. LEFT ENGINE FAILURE ON DESCENT THROUGH 17,000 FT. ENGINE POWER 40% N1 NOTICED ENGINE ROLLBACK WITH NO ABNORMAL INDICATIONS. NO FUEL OR OIL BYPASS LIGHTS ON, TRA - [SDR DXTA200400232](https://openairdocs.org/sdr/DXTA200400232), Jan 28, 2004: ENGINE. FLAMED OUT. WHILE DESCENDING THROUGH FL 310 WITH THE RIGHT POWER LEVER AT FLIGHT IDLE, THE BOOST PUMP CAME ON AND OIL PRESSURE DROPPED TO ZERO, GENERATOR WENT OFF-LINE. THE - [SDR DXTA200300208](https://openairdocs.org/sdr/DXTA200300208), Dec 22, 2003: FUEL CONTROL. FAILED. RIGHT ENGINE FLAMED OUT DURING DESCENT (THROUGH 22000) PERFORMED RESTART WITHOUT EVENT. ENGINE OPERATION WAS NORMAL THROUGH THE REST OF FLIGHT, AIRCRAFT CONTINU ## 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.