# N808QS: 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: 700-0035 - Year built: 2020 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: November 2, 2020 - Certificate issued: June 15, 2026 - Expires: June 30, 2033 - Mode S code: AB0104 - Owner type: Co-owned, fractional ownership - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=808QS - Page: https://openairdocs.org/aircraft/N808QS 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 N808QS. ## FAA accident and incident reports None matched to N808QS. ## Service difficulty reports (11) 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 2025F00287](https://openairdocs.org/sdr/2025F00287), Dec 21, 2025: FAIRING. CHAFED. LEFT MLG INNER GEAR DOOR IS CHAFING FAIRING STRUCTURE ON AFT EDGE. ACCOMPLISHED AQRD RFTS-115917 REV.0, DATED 20DEC2025, CHAFING ON FWD EDGE OF LOWER FAIRING SP - [SDR 2025F00286](https://openairdocs.org/sdr/2025F00286), Dec 21, 2025: FAIRING. CHAFED. LH MLG INNER GEAR DOOR IS CHAFING FAIRING STRUCTURE ON AFT EDGE. - [SDR 2025F00285](https://openairdocs.org/sdr/2025F00285), Dec 21, 2025: THRUST REVERSER. CORRODED. LEFT THRUST REVERSER HAS CORROSION ON THE OUTBOARD BEAM. RIGHT THRUST REVERSER HAS CORROSION ON THE INNER SURFACE OF THE INBOARD BEAM. - [SDR DXTA2024051711796](https://openairdocs.org/sdr/DXTA2024051711796), May 16, 2024: MIXER BOX. CRACKED. DURING CRIUSE AT FL 290, EXPERIENCED A RAPID DECOMPRESSION. THERE WAS A POPPING WOOSH SOUND, FOLLOWED BY CABIN PRESSURE RISING. WENT ON O2 MASKS & BEGAN AN IMME - [SDR DXTA2024020910831](https://openairdocs.org/sdr/DXTA2024020910831), Feb 8, 2024: BATTERY PACK. DISCHARGED. EMERGENCY LIGHTS BATTERY: POWER ON CHECKLIST. TURNING ON EMERGENCY LIST TO ON AND ARM WILL NOT COME ON. VERIFIED DISCREPANCY. APPLIED POWER AND LET EMERGENCY BA - [SDR DXTA2023051986610](https://openairdocs.org/sdr/DXTA2023051986610), May 18, 2023: UNKNOWN. UNKNOWN. ON TAKE OFF ROLL, IMMEDIATELY AFTER THROTTLES WERE SET TO TAKE OFF POWER, RECEIVED A NO TAKE OFF MESSAGE. NO TAKE OFF WAS ACCOMPANIED BY WHITE BRAKE FAULT CAS M - [SDR DXTA2023011278370](https://openairdocs.org/sdr/DXTA2023011278370), Jan 11, 2023: BRAKE SYS. FAULTED. BRAKE SYSTEM: UPON TAXIING TO THE RUNWAY ON DEPARTURE, BRAKES SHATTERED WHILE BEING APPLIED. ON ROTATION, WHITE CAS "BRAKE FAULT" DISPLAYED. UPON LANDING, MESSA - [SDR DXTA2022113075170](https://openairdocs.org/sdr/DXTA2022113075170), Nov 29, 2022: CONTROL CABLE. OUT OF RIG. APPROXIMATELY 100' AFTER LEAVING BLOCKS, AMBER BRAKE 50% DEGRADED CAS MESSAGE ILLUMINATED. RETURNED TO RAMP. AFTER SHUTDOWN, THE BATTERIES DISCONNECTED & RECONN - [SDR DXTA2022040559680](https://openairdocs.org/sdr/DXTA2022040559680), Apr 4, 2022: NONE. NONE. CABIN EMERG LIGHT: AFTER ENGINE SHUT DOWN, IT WAS NOTICED THAT THE EMERGENCY LIGHTS WILL NOT EXTINGUISH, REGARDLESS OF SWITCH POSITION. ATTEMPTED COCKPIT INERTI - [SDR DXTA2021102851030](https://openairdocs.org/sdr/DXTA2021102851030), Oct 27, 2021: DISCONNECT UNIT. MALFUNCTIONED. DURING APPROACH , PILOT NOTED AILERON INPUT WASN'T RESPONDING AT 400' AGL. DID A GO-AROUND, PILOT MONITORING CONTROL WHEEL ON RT HAD CORRECT RESPONSE. ATTEMPTED - [SDR DXTA202101044555](https://openairdocs.org/sdr/DXTA202101044555), Jan 4, 2021: ELECTRONIC UNIT. DEFECTIVE. AIRCRAFT EXPERIENCED A MOMENTARY LOSS OF POWER TO THE STANDBY ATTITUDE INDICATOR THAT SUBSEQUENTLY REINITIALIZED. AT THAT POINT WE RECEIVED A RUDDER MAINTENANCE ## Service difficulty reports on N808QS not matched to an aircraft (14) They name N808QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR JGVR20170517002](https://openairdocs.org/sdr/JGVR20170517002), May 17, 2017: BARREL. CORRODED. DURING REPACK OF NLG STRUT, FOUND NLG UPPER BARREL TO HAVE CORROSION AND DEEP PITS. REPLACED NLG UPPER BARREL. - [SDR DXTR2016091202](https://openairdocs.org/sdr/DXTR2016091202), Sep 12, 2016: THRUST REVERSER. CORRODED. THRUST REVERSER NOZZLE CORRODED. CORROSION REMOVED AND THE THRUST REVERSER REMAINING THICKNESS WAS BEYOND MINIMUM THICKNESS. THRUST REVERSER NOZZLE WAS REPAIRED - [SDR DXTR2016091201](https://openairdocs.org/sdr/DXTR2016091201), Sep 11, 2016: STRINGER. CORRODED. TAIL STRINGER CORRODED. REPAIRED IAW ERO-8588679. - [SDR DXTA2014062405806](https://openairdocs.org/sdr/DXTA2014062405806), Jun 22, 2014: MOTOR. FAULTY. AFTER DEPARTING LAX WE LOST THE AIR CONDITIONER GREEN LIGHT & THEN SMELLED A HINT OF SOMETHING LIKE BURNT ELECTRICAL. REMOVED FAULTY COMPRESSOR RELAY AND INSTAL - [SDR DXTA2011062004623](https://openairdocs.org/sdr/DXTA2011062004623), Jun 19, 2011: MOTOR. FAILED. AC COMPRESSOR INOPERATIVE. ELECTRICAL SMOKE ODOR PRESENT IN HELL HOLE. FOUND AIR CON COMPRESSOR MOTOR BRUSHES BURNED. R & R THE MOTOR, COMPRESSOR, RECEIVER/DRYE - [SDR DXTA2010102604272](https://openairdocs.org/sdr/DXTA2010102604272), Oct 25, 2010: FLAP SYSTEM. MALFUNCTIONED. FLAPS STOPPED AT 10 WHEN 15 SELECTED, HYD PRESSURE REMAINED ON (MOVED FLAP HANDLE TO MATCH FLAP INDICATOR, HYD PRESS WENT OUT). SELECTED FLAPS 15 AGAIN, FLAP IN - [SDR DXTA2010083004211](https://openairdocs.org/sdr/DXTA2010083004211), Aug 28, 2010: RELAY. INOPERATIVE. UPON GEAR EXTENSION THE LOW BRAKE PRESS LIGHT ILLUMINATED. ANTI SKID LIGHT CAME ON DURING APPROACH. DID MISSED APPROACH AND HELD TO RUN CHECKLIST. LIGHT STAYED - [SDR DXTA2010080204183](https://openairdocs.org/sdr/DXTA2010080204183), Jul 30, 2010: UPLOCK SWITCH. MALFUNCTIONED. AFTER TAKEOFF, MLG WOULD NOT RETRACT. GEAR UNLOCKED LIGHT ILLUMINATED. A GROUND OBSERVATION PROVIDED THAT RT MLG WAS FULLY EXTENDED. JACKED ACFT, PREFORMED MLG - [SDR DXTA2010070604141](https://openairdocs.org/sdr/DXTA2010070604141), Jul 2, 2010: DISPLAY. INTERMITTENT. INFLIGHT THE NR1 PFD WENT BLANK, ALONG WITH A CHECK PFD 1 ANNUNCIATOR. BOTH SEEMED TO RESET TO NORMAL WITHIN 5 SECONDS. WE HAVE NOTICED THE LAST SEVERAL DAYS TH - [SDR DXTA2009120703885](https://openairdocs.org/sdr/DXTA2009120703885), Nov 11, 2009: WIRE HARNESS. CHAFED. DURING UNSCHEDULED MX, DISCOVERED A WIRE BUNDLE CHAFING TO THE POINT OF COPPER WIRING EXPOSED FOR THE N1 INDICATING SYS. ALSO, CONDITIONED AIR TUBING CHAFED (HA - [SDR DXTA200702393](https://openairdocs.org/sdr/DXTA200702393), Aug 9, 2007: DOOR. OUT OF ALIGNMENT. DURING T/O ROIL MAIN CABIN DOOR ANNUNCIATOR CAME ON, UPON INSPECTION PRIOR TO OPENING DOOR NOTICED ALLIGNMENT MARKS TO BE OUT OF ALIGNMENT APROX .1250 INCH. - [SDR DXTA200702372](https://openairdocs.org/sdr/DXTA200702372), Aug 1, 2007: UPLOCK SWITCH. OUT OF ADJUST. UPON GEAR RETRACTION THE 3 GREEN LIGHTS WENT OUT, THE HYDRAULIC PUMP LIGHT WENT OUT, AND THE RED GEAR UNLOCK LIGHT REMAINED ON. JACKED A/C, PERFORMED LANDING GE - [SDR DXTA200501096](https://openairdocs.org/sdr/DXTA200501096), Nov 19, 2005: RELAY. STICKING. UPON LANDING, AFTER APPLYING BRAKES, LOW BRAKE PRESS + ANTI-SKID INOP + MASTER CAUTION LAMPS ON FOR 6 SECONDS THEN EXTINGUISHED. NO BRAKING AVAIL FOR INITIAL 2 - [SDR DXTA200501090](https://openairdocs.org/sdr/DXTA200501090), Nov 17, 2005: ACCUMULATOR. LOW. UPON LANDING, AFTER APPLYING BRAKES, LOW BRAKE PRESS AND ANTI SKID INOP. MASTER CAUTION LAMPS ON FOR 6 SECONDS THEN EXTINGUISHED. ALSO BRAKES GRABBY LT MORE THA ## 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.