# N831QS: 2022 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: 700-0075 - Year built: 2022 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: August 10, 2022 - Certificate issued: September 17, 2026 - Expires: September 30, 2033 - Mode S code: AB5D80 - Owner type: Co-owned, fractional ownership - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=831QS - Page: https://openairdocs.org/aircraft/N831QS 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 N831QS. ## FAA accident and incident reports None matched to N831QS. ## 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 DXTA2026082709424](https://openairdocs.org/sdr/DXTA2026082709424), Aug 24, 2026: WIRE HARNESS. FAULTED. ON THE DESCENT WE HAD A WHITE ENG CTRL FAULT L CAS MESSAGE THAT REVERTED TO AMBER ENG CTRL FAULT L UPON LANDING. REMOVED LT ENG W6 WIRE HARNESS AND REPLACED WIT - [SDR 2025FA0000833](https://openairdocs.org/sdr/2025FA0000833), Dec 18, 2025: THRUST REVERSER. CORRODED. CORROSION ON THE INSIDE SURFACE OF LH AND RH ENGINE THRUST REVERSER PIVOT DOORS AND BEAMS. REMOVED CORROSION AND VERIFIED REMAINING MATERIAL THICKNESS TO BE WIT - [SDR DXTA2025021102281](https://openairdocs.org/sdr/DXTA2025021102281), Feb 7, 2025: AIR FILTER. DEFECTIVE. SMELLS IN CABIN/COCKPIT: BOTH THE CABIN AND THE COCKPIT HAVE A MUSTY SMELL ANYTIME THE APU OR ENGINES ARE RUNNING. CORRECTIVE ACTION: REPLACED HEPA FILTER. OPS - [SDR DXTA2023121310321](https://openairdocs.org/sdr/DXTA2023121310321), Dec 13, 2023: UNKNOWN. UNKNOWN. EMERGENCY LIGHTS DO NOT ILLUMINATE DURING POWER ON CHECK PER AOM 2.12.2.1. R & R BATTERY PACKS. - [SDR DXTA2023121110290](https://openairdocs.org/sdr/DXTA2023121110290), Dec 8, 2023: BATTERY. INOPERATIVE. EMERGENCY EXIT LIGHTS WILL NOT TEST. NONE OF THE LIGHTS WILL ILLUMINATE UNDER THEIR OWN BATTERY POWER. COMPLIED WITH OPS CHECK OF BATTERIES IAW MM 33-50-00. OPS - [SDR DXTA2023090594380](https://openairdocs.org/sdr/DXTA2023090594380), Sep 1, 2023: MODULE. DEFECTIVE. L AMBER CAS: GEAR DISAGREE AMBER LRN CASS MESSAGE DISPLAYED AFTER TAKE OFF AND DURING GEAR RETRACTION. RAN QRH FOR GEAR DISAGREE CAS MESSAGE WHICH RESULTED IN P - [SDR DXTA2023041784380](https://openairdocs.org/sdr/DXTA2023041784380), Apr 16, 2023: UNKNOWN. UNKNOWN. MAIN DOOR: MAIN DOOR HANDLE DIFFICULT TO LATCH. MAY REQUIRE 2 HANDS TO PULL. // SIGNOFF // GAINED ACCESS TO MED HANDLE MECHANISM AND VERIFY DISCREPANCY. DOOR HA - [SDR DXTA2023031082360](https://openairdocs.org/sdr/DXTA2023031082360), Mar 10, 2023: UNKNOWN. UNKNOWN. NOSE LANDING GEAR WOULD NOT RETRACT. COULD HEAR BINDING OF NOSE GEAR/ DOORS IN COCKPIT. VIBRATION FELT IN YOKE CONTROL. PERFORMED THE NOSE LANDING GEAR SQUAT SW - [SDR DXTA2023022781310](https://openairdocs.org/sdr/DXTA2023022781310), Feb 25, 2023: NONE. NONE. CABIN EMERG LIGHT: EMER LIGHTS WILL NOT EXTINGUISH. *** CORRECTIVE ACTION *** RESET ALL G-SWITCHES, CHARGED EMERGENCY BATTERIES AND PERFORMED OPS CHECKS IAW CES - [SDR DXTA2022121976460](https://openairdocs.org/sdr/DXTA2022121976460), Dec 17, 2022: DOOR. OUT OF ADJUST. DURING ARRIVAL INSPECTION, FOUND MCD DOES NOT DROP DOWN WHEN OPENING (FOUND BY MX) // SIGNOFF// FOUND DURING ARRIVAL INSPECTION. ADJUSTED MAIN CABIN DOOR FORWAR - [SDR DXTA2022092270900](https://openairdocs.org/sdr/DXTA2022092270900), Sep 22, 2022: WIRE. SHORTED. CABIN DOOR OPEN AMBER CAS: WHEN CLOSING MAIN CANIN DOOR, YELLOW DOOR HANDLE LOCK LIGHT WOULD NOT EXTINGUISH. ALSO AMBER CAS CABIN DOOR OPEN WAS ILUMINATED. FOLL - [SDR 2022F00338](https://openairdocs.org/sdr/2022F00338), Sep 10, 2022: NONE. CHIPPED. LH MAIN LANDING GEAR DOOR DAMAGED. ACCOMPLISHED TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ36249M1 DATED: 09/08/2022, LEFT MAIN LANDING GEAR DOOR DAMAGE (CHIP ## Service difficulty reports on N831QS not matched to an aircraft (14) They name N831QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR JGVR20170808001](https://openairdocs.org/sdr/JGVR20170808001), Aug 8, 2017: SKIN. CORRODED. FOUND CORROSION ON EXTERNAL AREA OF THE UPPER SKIN NEAR LWS 121 AND AFT SPAR OF THE LEFT WING. REPAIRED BY BLENDING, EDDY CURRENT AND ULTRASOUND INSPECTIONS, AN - [SDR DXTA2017010306353](https://openairdocs.org/sdr/DXTA2017010306353), Jan 2, 2017: BRAKE SYS. MALFUNCTIONED. DURING LANDING, RECEIVED A LOW BRAKE PRESSURE AND ANTI-SKID FAILURE LIGHTS WITH THE MASTER CAUTION LIGHT. AT FIRST HAD BRAKES THEN THEY FAILED. USED THE EMERGEN - [SDR DXTA2016050706237](https://openairdocs.org/sdr/DXTA2016050706237), May 7, 2016: SPAR CAP. CORRODED. CORROSION ALONG RT WING UPPER SPAR CAP SURFACES. IDENTIFIED ALL CORRODED AREAS ON THE RT UPPER WING SPAR CAP & REMOVED ALL CORROSION. PERFORMED A FLUORESCENT DY - [SDR DXTA2016050706236](https://openairdocs.org/sdr/DXTA2016050706236), May 7, 2016: SPAR CAP. CORRODED. CORROSION ALONG LT WING UPPER SPAR CAP SURFACES. PERFORMED A FLUORESCENT DYE PENETRANT INSPECTION OF THE BLENDED AREAS ON LEFT WING UPPER SPAR CAP, FOR REMAININ - [SDR DXTA2016050705236](https://openairdocs.org/sdr/DXTA2016050705236), May 7, 2016: SPAR CAP. CORRODED. CORROSION ALONG LT WING UPPER SPAR CAP SURFACES. PERFORMED A FLUORESCENT DYE PENETRANT INSPECTION OF THE BLENDED AREAS ON LT WING UPPER SPAR CAP, FOR REMAINING - [SDR DXTA2015102006110](https://openairdocs.org/sdr/DXTA2015102006110), Oct 19, 2015: UNKNOWN. ODOR. ELECTRICAL ODOR DETECTED IN CABIN AT AREA SURROUNDING SEAT 10, PROGRESSING TO COCKPIT. REDUCING CABIN TEMP HAD NO EFFECT ON ODOR, FULL COLD. AFTER INTERIOR MAST - [SDR DXTA2014092905897](https://openairdocs.org/sdr/DXTA2014092905897), Sep 26, 2014: A/C PACK. ODOR. AFTER TAKEOFF AFTER TURNING ON FREON AIR CONDITIONER SMELLED A BURNING ODOR IN THE CABIN. ACCOMPLISHED A VISUAL INSPECTION & AN OPS TEST WITH GROUND POWER OF TH - [SDR DXTA2014091805886](https://openairdocs.org/sdr/DXTA2014091805886), Sep 17, 2014: TRANSDUCER. LOOSE. DURING TAXI RIGHT BRAKE MOMENTARILY FAILED. PEDAL WENT TO FLOOR AND PRESSURE THEN RETURNED AFTER ABOUT ONE SECOND. A SECOND EPISODE OCCURRED WITH A MUCH SHORTER - [SDR DXTA2014090905878](https://openairdocs.org/sdr/DXTA2014090905878), Sep 8, 2014: CONTROL UNIT. FAULTY. ON LANDING ROLLOUT THE BRAKES FELT LIKE THEY FAILED FOR ABOUT 1 - 2 SECONDS THEN RETURNED TO NORMAL. IT HAPPENED AGAIN ON TAXI INTO THE RAMP. NO LIGHTS APPEARED - [SDR DXTR2014081101](https://openairdocs.org/sdr/DXTR2014081101), Aug 11, 2014: BEAM. GOUGED. GOUGE ON FWD FACE OF I-SECTION LT SIDE AND FWD OF PRESSURE BULKHEAD 0.30" D X .2500" IN LENGTH. ACCOMPLISHED ENGINEERING REPAIR ORDER ERO-601176. - [SDR DXTA2014031005681](https://openairdocs.org/sdr/DXTA2014031005681), Mar 9, 2014: ACTUATOR. MALFUNCTIONED. AT CRUISE ALTITUDE FL 410 WITH AUTOPILOT ENGAGED, AN AMBER BOXED A APPEARED, FOLLOWED BY A RED BOXED A ON BOTH PFD'S. COPILOT BELIEVES THE RED ARROW WAS POINTIN - [SDR DXTA2013111505566](https://openairdocs.org/sdr/DXTA2013111505566), Nov 14, 2013: BATTERY. FAILED. DURING CRUISE, FL 32,000 FT. MASTER WARNING ILLUMINATED WITH NO ASSOCIATED ANNUNCIATORS. AFTER RESET, ILLUMINATED AGAIN WITH NO ANNUNCIATORS. WHEN IT ILLUMINATE - [SDR DXTA2009121103891](https://openairdocs.org/sdr/DXTA2009121103891), Dec 10, 2009: PRESSURE SWITCH. INOPERATIVE. LOW BRAKE PRESS AND ANTISKID LIGHT ILLUMINATED EXITING RUNWAY. LOST BRAKE PRESSURE ON FBO RAMP USED EMERGENCY BRAKES TO STOP, RESEVOIR IS FULL OF FLUID, BRAKE A - [SDR DXTA2009092103794](https://openairdocs.org/sdr/DXTA2009092103794), Sep 20, 2009: RELAY. INOPERATIVE. AFTER LANDING, RECEIVED A LOW BRAKE PRESS ANTI-SKID INOP ANNUNCIATOR, FOLLOWED BY LOSS OF BRAKES. USED EMERGENCY BRAKE TO STOP ON TAXIWAY. INSPECTED AND TROUBLE ## 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.