# N806QS: 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: 700-0029 - Year built: 2020 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: May 22, 2020 - Certificate issued: September 4, 2025 - Expires: September 30, 2032 - Mode S code: AAF996 - Owner type: Co-owned, fractional ownership - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=806QS - Page: https://openairdocs.org/aircraft/N806QS 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 N806QS. ## FAA accident and incident reports None matched to N806QS. ## Service difficulty reports (13) 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 DXTA2026042107701](https://openairdocs.org/sdr/DXTA2026042107701), Apr 19, 2026: PROXIMITY SWITCH. OUT OF ADJUST. AT FL410, RECEIVED A MASTER CAUTION CAS, EMERGENCY EXIT OPEN. RAN THE QRH 25C AND NOTED NO ABNORMAL INDICATIONS THROUGH THROUGH THE SYNOPTIC PAGES OR ON THE EXI - [SDR DXTA2026030607119](https://openairdocs.org/sdr/DXTA2026030607119), Mar 4, 2026: SMOKE DETECTOR. DIRTY. ON GROUND GOT RED BAGGAGE FIRE LIGHT CAS MESSAGE. POWERED UP ACFT & ABLE TO DUPLICATE DISCREPANCY, WENT THRU FAULT HISTORY & FOUND ALERT ID 593. THIS FAULT IS T - [SDR DXTA2026020206727](https://openairdocs.org/sdr/DXTA2026020206727), Jan 29, 2026: OXYGEN BOTTLE. LEAKING. OXYGEN BOTTLES LOST PRESSURE WHILE IN FLIGHT. BOTH OXYGEN BOTTLES WERE AT 1500-1600 ON PREFLIGHT. - [SDR DXTA2025120205921](https://openairdocs.org/sdr/DXTA2025120205921), Nov 30, 2025: BATTERY PACK. NO TEST. CABIN EMERGENCY LIGHTING IS NOT WORKING PROPERLY. WITH BATTERIES OFF & FOLLOWING A 30 MIN CHARGE WITH APU ON, EMERGENCY LIGHTS WILL ILLUMINATE IN ON, BUT FAIL T - [SDR DXTA2024122301590](https://openairdocs.org/sdr/DXTA2024122301590), Dec 18, 2024: DIODE. INOPERATIVE. FLOOR LIGHTING UNDER SEATS 5, 9, AND LAV ARE INOP. CABIN EMERG LIGHT: FLOOR LIGHTING UNDER SEATS 5, 9, AND LAV ARE INOP. REMOVED SEAT 5 SHROUD AND INSPECTED CON - [SDR DXTA2024120201329](https://openairdocs.org/sdr/DXTA2024120201329), Nov 29, 2024: LIGHT. INOPERATIVE. EMERG EXIT SIGN/LIGHT: CABIN FORWARD BULKHEAD EXIT SIGN ABOVE SEAT 3 INTERMITTENT. APPEARS TO WORK WITH EMER LIGHTS ON, BUT DOES NOT WORK WITH EMER LIGHTS ARMED - [SDR DXTA2024050711697](https://openairdocs.org/sdr/DXTA2024050711697), May 6, 2024: BATTERY PACK. FAILED. EMERGENCY LIGHTING WILL NOT WORK UNDER OWN POWER. THEY DO WORK WITH SHIPS POWER ON. R & R BATTERY PACKS DUE TO INTERNAL FAILURE IAW AMM 33-50-05. - [SDR DXTA2023112910172](https://openairdocs.org/sdr/DXTA2023112910172), Nov 28, 2023: FUSE. FAULTED. LOWER LAV EMER LIGHT DOES NOT ILLUMINATE WITH POWER ON CHECKLIST PER AOM. INSPECTED ALL LIGHT CONNECTIONS & WIRING ASSOCIATED WITH EMER TOILET PATH WIRING . REF - [SDR DXTA2023062889750](https://openairdocs.org/sdr/DXTA2023062889750), Jun 28, 2023: UNKNOWN. UNKNOWN. EMERGENCY LIGHT SING ON THE FORWARD BULKHEAD IS OUT WHEN IN THE ARMED POSITION. CREW HAS GIVEN MCC PERMISSION TO SIGN OFF AS EIE. - [SDR 2023FA0000318](https://openairdocs.org/sdr/2023FA0000318), Jun 15, 2023: THRUST REVERSER. CORRODED. L/H THRUST REVERSER I/B AND O/B BEAMS HAS AREAS OF MINOR CORROSION. - [SDR DXTA2022092370950](https://openairdocs.org/sdr/DXTA2022092370950), Sep 22, 2022: BATTERY PACK. ABNORMAL. EMERG EXIT SIGN/LIGHT: EMER LIGHTS WORKED ON INITIAL POWER UP PRE FLIGHT BUT ARE FAILING TO ILLUMINATE ON SHUT DOWN. // SIGNOFF// REMOVED AND REPLACED EMERGENCY - [SDR DXTA2022021056500](https://openairdocs.org/sdr/DXTA2022021056500), Feb 10, 2022: NOT REPORTED. NOT REPORTED. CABIN EMERG LIGHT: EMER LIGHTS WILL NOT ILLUMINATE IN THE "ON" POSITION, BUT THEY DO ILLUMINATE IN THE "ARM" POSITION. WE RAN THE APU FOR 20 MINUTES AND THEN SH - [SDR DXTA2020082304018](https://openairdocs.org/sdr/DXTA2020082304018), Aug 23, 2020: SENSOR. OUT OF POSITION. AFTER TAKEOFF AND SELECTING LANDING GEAR UP, NOSE GEAR CAME UP, BUT BOTH MAIN GEAR INDICATIONS WERE AMBER. GEAR MISCOMPARE AND GEAR DOOR OPEN CAS MESSAGES APPEA ## Service difficulty reports on N806QS not matched to an aircraft (13) They name N806QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DXTA2014033005704](https://openairdocs.org/sdr/DXTA2014033005704), Mar 28, 2014: BRAKE ASSY. MALFUNCTIONED. RIGHT BRAKE DRAGGED SEVERELY DURING EXITING RUNWAY. SIGNIFICANT VIBRATION & YAWING WERE EXPERIENCED. AFTER SETTING & RELEASING THE PARKING BRAKE & WAITED 5 MINU - [SDR DXTA2010091704241](https://openairdocs.org/sdr/DXTA2010091704241), Sep 16, 2010: FLAP SYSTEM. FROZEN. DURING FLAP EXTENSION ON APPROACH, THE FLAPS FROZE BETWEEN THE 7 DEGREE DETENT AND THE 15 DEGREE DETENT. RAN FLAPS THUR ALL POSITIONS VARIOUS TIMES - NO DEFECTS - [SDR DXTA2009010103452](https://openairdocs.org/sdr/DXTA2009010103452), Jan 1, 2009: PITOT SYSTEM. CONTAMINATED. VISUAL DISCREPANCY OBSERVED DURING TAKEOFF CROSS CHECKS. NO FLAGS OR ANNUNCIATORS WITNESSED. PILOTSIDE AIRSPEED STAYED STEADY AT 53 KTS. COPILOTS AIRSPEED WAS I - [SDR DXTA2009010203452](https://openairdocs.org/sdr/DXTA2009010203452), Jan 1, 2009: INDICATOR. MALFUNCTIONED. PILOTSIDE AIRSPEED STAYED STEADY AT 53 KTS. COPILOTS AIRSPEED WAS INCREASING AT A NORMAL RATE. ABORTED TAKEOFF AT 86 KTS. - [SDR DXTA2008110603338](https://openairdocs.org/sdr/DXTA2008110603338), Nov 5, 2008: WIRE. CHAFED. DURING FLIGHT THE RIGHT CLOCK CIRCUT BREAKER POPPED FOLLOWED BY A BURNING SMELL THAT LASTED FOR 5-10 SECONDS. FOUND POWER WIRE CHAFED ON COPILOTS DISPLAY UNIT. - [SDR DXTA200802983](https://openairdocs.org/sdr/DXTA200802983), Apr 6, 2008: ACTUATOR. MALFUNCTIONED. AFTER SELECTING GEAR DOWN, RT MAIN GREEN LIGHT AND GEAR UNLOCKED RED LIGHT BEGAN TO FLICKER INTERMITTENT (3 GREEN NO RED). TROUBLESHOT TO FAULTY RT MLG ACTUATOR - [SDR DXTA20082983](https://openairdocs.org/sdr/DXTA20082983), Apr 6, 2008: WARNING LIGHT. ILLUMINATED. AFTER SELECTING GEAR DOWN, RT MAIN GREEN LIGHT AND GEAR UNLOCKED RED LIGHT BEGAN TO FLICKER INTERMITTENT (3 GREEN NO RED). - [SDR DXTA20082890](https://openairdocs.org/sdr/DXTA20082890), Feb 19, 2008: LANDING GEAR. MALFUNCTIONED. DURING NORMAL GEAR EXTENISON ON FINAL APPROACH, LT MAIN GEAR WOULD NOT INDICATE DOWN AND LOCKED BY THE GEAR INDICATOR LIGHT. CLEAN AND LUBRICATED LT AND RT MLG - [SDR DXTA200702236](https://openairdocs.org/sdr/DXTA200702236), Jun 1, 2007: O-RING. LEAKING. TAXING FOR DEPARTURE, ANTISKID LIGHT ILLUMINATED RETURNING., THE LOW BRAKE PRESS LITE ILLUMINATED, WE USED THE EMERGENCY BRAKES FOR PARKING. FOUND BRAKE PUMP FI - [SDR DXTA200501031](https://openairdocs.org/sdr/DXTA200501031), Oct 19, 2005: STRUT. DISCHARGED. LOUD BANG HEARD AT ROTATION ON THE AIRCRAFT. JACKED AIRCRAFT AND SERVICED MAIN STRUTS WITH FLUID AND NITROGEN IAW 560 MM 12-14-01. PERFORMED GEAR SWING SEVERAL - [SDR DXTA200500906](https://openairdocs.org/sdr/DXTA200500906), Aug 19, 2005: CONTROL SYSTEM. STUCK. UPON TAXI OUT THE CO-PILOT APPLIED FULL RT RUDDER AND HAD NO RT BRAKE. THE CAPT APPLIED RT BRAKE WHICH WORKED BUR THE RT BRAKE AND RUDDER PEDAL MADE A LOUD CATC - [SDR DXTA200400486](https://openairdocs.org/sdr/DXTA200400486), Dec 19, 2004: INDICATOR. INOPERATIVE. NO GREEN LIGHT ON LEFT MAIN LANDING GEAR WHEN SELECTED DOWN. INTRANSIT LIGHT ON, HYD PRESS LIGHT OFF, GEAR UNSAFE WARNING HORN ON. ITEM IS UNDER INVESTIGATION. - [SDR DXTA200400404](https://openairdocs.org/sdr/DXTA200400404), Sep 21, 2004: WARNING LIGHT. ILLUMINATED. AT ROTATION GOT LOUD NOISE AND EXCESSIVE HEAT AND A NOTICEABLE ODOR WAS PRESENT. ANNUNCIATOR PANEL WAS CLEAR, PRESSURE SOURCE WAS NORMAL, ANNUNCIATOR PANEL EMER ## 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.