# N852QS: 2023 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: 700-0102 - Year built: 2023 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 1, 2023 - Certificate issued: October 8, 2026 - Expires: October 31, 2033 - Mode S code: ABB035 - Owner type: Co-owned, fractional ownership - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=852QS - Page: https://openairdocs.org/aircraft/N852QS 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 N852QS. ## FAA accident and incident reports None matched to N852QS. ## 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 DXTA2026083109495](https://openairdocs.org/sdr/DXTA2026083109495), Aug 30, 2026: STOP FITTING. OUT OF ADJUST. THE MAIN CABIN DOOR HANDLE IS DIFFICULT TO MOVE TO THE CLOSED POSITION WHEN CLOSING THE CABIN DOOR FROM INSIDE. WHEN CLOSING THE DOOR ON THE PREVIOUS FLIGHT, WE - [SDR DXTA2026081809308](https://openairdocs.org/sdr/DXTA2026081809308), Aug 16, 2026: PIN. OUT OF ALIGNMENT. UNABLE TO LATCH MAIN CABIN DOOR CLOSED. ONE OF THE PINS IS RECESSED INTO THE DOOR AND IS NO LONGER ALIGNED WITH ITS HOLE. REMOVED THE AIRSTAIRS AND COVER PLATE. - [SDR DXTA2026081709282](https://openairdocs.org/sdr/DXTA2026081709282), Aug 14, 2026: PIN. DAMAGED. WHEN THE CREW ARRIVED AT THE AIRCRAFT, THE MAIN CABIN DOOR WAS OPEN. THE SERVICE HUB CLEANERS HAVE BEEN ON BOARD AND WE'RE NOT ABLE TO CLOSE THE MAIN CABIN DOOR - [SDR DXTA2025100205149](https://openairdocs.org/sdr/DXTA2025100205149), Sep 30, 2025: CONTROL VALVE. DEFECTIVE. WHILE TAXING OUT AND APPLYING THE BRAKES THE AMBER "BRAKE 50% DEGRADED" CAS MESSAGE DISPLAYED EVERY TIME WE APPLIED THE BRAKES. IT WOULD DISAPPEAR WHEN BRAKES W - [SDR 2025F00095](https://openairdocs.org/sdr/2025F00095), Apr 17, 2025: THRUST REVERSER. CORRODED. LH AND RH THRUST REVERSER INNER AIR WASHED SURFACES HAVE CORROSION. ACCOMPLISHED CORROSION REMOVAL AND REPAIR TO LH AND RH THRUST REVERSER BEAMS AND PIVOT DOORS - [SDR 2025FA0000257](https://openairdocs.org/sdr/2025FA0000257), Apr 9, 2025: FUEL CELL. FOD. WHILE ACCOMPLISHING SL 700-28-02, A RAG WAS FOUND IN THE RIGHT WING FUEL BAY NUMBER 13 FLAPPER. THIS WAS THE FIRST INSPECTION OF THE FUEL STORAGE SYSTEM SINCE P - [SDR DXTA2025040202865](https://openairdocs.org/sdr/DXTA2025040202865), Mar 30, 2025: BATTERY PACK. FAULTED. EMERGENCY LIGHTING: EMER LIGHTS DO NOT ILLUMINATE WHEN POWER IS OFF AND SWITCH IS IN ON POSITION. ARM POSITION FUNCTIONS CORRECTLY. CORRECTIVE ACTION: EMERGENCY - [SDR DXTA2025022702520](https://openairdocs.org/sdr/DXTA2025022702520), Feb 26, 2025: RUB BLOCK. LOOSE. DOOR STICKS HARD TO OPEN INSIDE AND OUT. GAINED ACCESS TO AIRCRAFT AND FOUND CABIN DOOR RUB BLOCK LOOSE. AJUSTED RUB BLOCK AND PERFORMED OPS CHECK. OPS CHECK GO - [SDR DXTA2024010210482](https://openairdocs.org/sdr/DXTA2024010210482), Dec 31, 2023: SENSOR. FAULTED. BRAKE 50% DEGRADE CAS MESAGE. CYCLED GEAR , MESSAGE WENT AWAY. CYCLED AGAIN AND CAME BACK. LANDED WITHOUT OUTBOARD BRAKES. TAXING IN BRAKES BEGAN WORKING. IAW . - [SDR DXTA2023121410329](https://openairdocs.org/sdr/DXTA2023121410329), Dec 14, 2023: UNKNOWN. UNKNOWN. MAIN CABIN DOOR WILL NOT LATCH, DOOR OPERATES BUT WILL NOT LATCH. FOUND UPPER FORWARD MCD STRIKER LATCH TO BE OUT OF ADJUSTMENT. PERFORMED MCD STRIKER LATCH RIG - [SDR DXTA2023120410219](https://openairdocs.org/sdr/DXTA2023120410219), Dec 2, 2023: UNKNOWN. UNKNOWN. MAIN CABIN DOOR CABIN DOOR OPEN AMBER CAS WILL NOT EXTINGUISH. TRIED TO CLOSE DOOR SEVERAL TIMES. RAN CHECKLIST LIGHT IS STILL ILLUMINATED. ## Service difficulty reports on N852QS not matched to an aircraft (11) They name N852QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DXTA2015070806041](https://openairdocs.org/sdr/DXTA2015070806041), Jul 4, 2015: OIL SYSTEM. LOW PRESSURE. INFLIGHT ENGINE SHUTDOWN, DUE TO A HIGH OIL PRESSURE INDICATION. PERFORMED A VISUAL INSPECTION OF RT ENGINE WITH NO ISSUES. PERFORMED A GROUND RUN TO CONFIRM HI - [SDR DXTA2015050806016](https://openairdocs.org/sdr/DXTA2015050806016), Apr 27, 2015: STRUT. UNSERVICEABLE. ZERO RUDDER TRAVEL IN FLIGHT DESPITE NORMAL CHECKS ON GND. SUSPECT RUDDER BIAS ISSUE. PREFORMED FUNCTIONAL TEST OF RUDDER BIAS SYS, TESTED SATISFACTORY. PERFORM - [SDR DXTA2015050506015](https://openairdocs.org/sdr/DXTA2015050506015), Apr 27, 2015: UNKNOWN. MALFUNCTIONED. ZERO RUDDER TRAVEL IN FLIGHT DESPITE NORMAL CHECKS ON GND. - [SDR DXTA2015041606006](https://openairdocs.org/sdr/DXTA2015041606006), Apr 15, 2015: SEAL. FAILED. CLIMBING THROUGH 9000 FEET BOTH MWS SYS LIGHTS STARTED FLASHING FOLLOWED BY REAR BAY OVERHEAT LIGHT. REDUCED POWER & CLIMBED WHICH EXTINGUISHED REAR BAY OVERHEA - [SDR DXTA201504136005](https://openairdocs.org/sdr/DXTA201504136005), Apr 12, 2015: SLEEVE. LEAKING. WHILE CLIMBING THROUGH 15,000', BOTH RED MWS LIGHTS STARTED FLASHING FOLLOWED BY REAR BAY OVERHEAT LIGHT. INITIALLY REDUCED CLIMB & REDUCED POWER. AS POWER REDU - [SDR DXTA2011020904458](https://openairdocs.org/sdr/DXTA2011020904458), Feb 8, 2011: UNKNOWN. UNKNOWN. THERES IS A LOUD RUMBLE/ KNOCKING NOISE COMING FROM UNDERNEATH THE FLOORBOARD NEAR THE EMERGENCY EXIT WHILE IN TURBULANCE. (CREW DEBRIEF HAPPENED ON CLIMBOUT, L - [SDR DXTA2011011204409](https://openairdocs.org/sdr/DXTA2011011204409), Jan 11, 2011: UNKNOWN. ODOR. COLD AIR COMING OUT ON LT PILOT SIDE UNDER PANEL, TURN FLT DECK VALVE ON- NO HEAT JUST STRONG ODOR UNTIL VALVE SELECTED TO OFF. RAN ACFT AND OPERATED FLT DECK V - [SDR 2006FA0000927](https://openairdocs.org/sdr/2006FA0000927), Sep 19, 2006: SKIN. CORRODED. MAJOR CORROSION ON THE THRUST REVERSER DOOR RAMP SKINS DUE TO THE PAINT MISSING FROM THE RIVET HEADS. BY MAJOR CORROSION I MEAN WE ARE BLENDING THE AREAS BELOW - [SDR 2006FA0000926](https://openairdocs.org/sdr/2006FA0000926), Sep 19, 2006: THRUST REVERSER. CORRODED. MAJOR CORROSION ON THE THRUST REVERSER DOOR RAMP SKINS DUE TO THE PAINT MISSING FROM THE RIVET HEADS. BY MAJOR CORROSION, WE ARE BLENDING THE AREAS BELOW LIMITS - [SDR DXTA200500996](https://openairdocs.org/sdr/DXTA200500996), Oct 2, 2005: SMOKE. DETECTED. WITH APU RUNNING SMOKE WAS COMING FROM THE NR 2 AIR DUCT DUCT TEMP WAS 104 DEG C, ALSO WOULD NOT COOL OFF. RAN ONLY NR 2 ENGINE WITH SAME RESULTS AIRPLANE FILLE - [SDR DXTA200500597](https://openairdocs.org/sdr/DXTA200500597), Feb 18, 2005: COALESCER BAG. CONTAMINATED. DURING OCF FOR ENGINE CHANGE, WITH APPLICATION OF MAX CONTINUOUS POWER, DETECTED A VERY STRONG SMELL (ASSOCIATED WITH AN OIL/EXHAUST AND BURNING ODOR). REMOVED ## 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.