# N846QS: 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: 700-0095 - Year built: 2023 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: May 11, 2023 - Certificate issued: June 13, 2023 - Expires: June 30, 2030 - Mode S code: AB9792 - Owner type: Co-owned, fractional ownership - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=846QS - Page: https://openairdocs.org/aircraft/N846QS 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 N846QS. ## FAA accident and incident reports None matched to N846QS. ## Service difficulty reports (17) 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 DXTA2026101210085](https://openairdocs.org/sdr/DXTA2026101210085), Oct 8, 2026: SHIM. DEFECTIVE. IN CLIMB FL 410 TO FL 430, RECEIVED CAS CHECK DOORS AND CABIN DOOR OPEN. THERE WAS NO PRESSURE CHANGE BUT RAN THE CHECKLIST, ADVISED THE COMPANY AND DIVERTED TO - [SDR DXTA2026100810051](https://openairdocs.org/sdr/DXTA2026100810051), Oct 5, 2026: HARNESS. FAULTED. DOOR HANDLE FEELS AS THERE'S A SLIGHT BINDING WHILE MOVING. AMBER DOOR OPEN CASS MSG WILL NOT EXTINGUISH. PREFORMING QRH PROCEDURE, LIGHT WOULD NOT FLASH WHICH - [SDR DXTA2026100510009](https://openairdocs.org/sdr/DXTA2026100510009), Oct 2, 2026: MOTOR. FAULTY. MAIN CABIN DOOR HANDLE AT TIMES REQUIRES EXCESSIVE FORCE TO OPERATE. OTHER TIMES IT SEEMS TO OPERATE MOSTLY NORMAL, BUT WITH MORE RESISTANCE THAN USUAL WHEN CLO - [SDR DXTA2026030907167](https://openairdocs.org/sdr/DXTA2026030907167), Mar 6, 2026: DOOR. LACK OF LUBE. WE ARE NOT ABLE TO GET THE MAIN CABIN DOOR TO LATCH. WE ARE ABLE TO LIFT THE DOOR FROM OUTSIDE AND INSIDE, HOWEVER IT WILL NOT LOCK OR LATCH FROM THE OUTSIDE OR - [SDR DXTA2026010806476](https://openairdocs.org/sdr/DXTA2026010806476), Jan 7, 2026: DOOR LATCH. FAULTY. MAIN DOOR WILL RAISE INTO CLOSED POSITION BUT DOOR HANDLE WILL NOT MOVE TO LOCK THE DOOR. ALSO TRIED CLOSING THE DOOR FROM THE OUTSIDE AND THE OUTER DOOR LATCH - [SDR DXTA2026010706436](https://openairdocs.org/sdr/DXTA2026010706436), Jan 4, 2026: PROXIMITY SWITCH. FAULTY. FLT CREW REPORTED DOOR OPEN CAS, LINXUS SHOWS CABIN DOOR OPEN FAULT ID 2230 AND CHECK DOOR FAULT ID 2265. DOWNLOADED AND REVIEWED ARES DATA TO CONFIRM THE DOOR - [SDR DXTA2025091804990](https://openairdocs.org/sdr/DXTA2025091804990), Sep 16, 2025: DOOR. OUT OF ALIGNMENT. MAIN CABIN DOOR IS OUT OF ALIGNMENT FOUND THE FORWARD DOOR BUMPER MAKING CONTACT WITH THE DOOR WHEN CLOSING REMOVE 3 SHIMS BEHIND 4 DOOR BUMPER TO GET CLEARANCE - [SDR DXTA2025090304796](https://openairdocs.org/sdr/DXTA2025090304796), Sep 1, 2025: DOOR. NO DISCREPANCY. MAIN CABIN DOOR REQUIRES EXCESSIVE FORCE TO CLOSE. OPENS NORMALLY. : INSPECTED DOOR WITH NO DEFECTS NOTED. FOUND DOOR TOUGH TO CLOSE INTERMITTENTLY, INSPECTED C - [SDR DXTA2025082504708](https://openairdocs.org/sdr/DXTA2025082504708), Aug 23, 2025: ELEC CONNECTOR. DAMAGED. PATH LIGHT AT SEAT NR 9 IS INOPERATIVE. FOUND PIN OUT OF CONNECTOR, REATTACHED PIN, OPS CHECK GOOD REF IMM 25-20-21 - [SDR DXTA2025051103453](https://openairdocs.org/sdr/DXTA2025051103453), May 11, 2025: DOOR. UNKNOWN. MAIN DOOR: WHEN CLOSING MAIN CABIN DOOR, WE HAVE TO OPEN AND CLOSE DOOR 2-3 TIMES, FOR DOOR SENSOR TO EXTINGUISH. SEEMS TO NEED AN ADJUSTMENT TO ALIGNMENT CORRE - [SDR DXTA2025032402771](https://openairdocs.org/sdr/DXTA2025032402771), Mar 21, 2025: ELEC CONNECTOR. DISCONNECTED. EMERG EXIT SIGN/LIGHT: DURING POWER ON CHECKLIST, FFOD, CHECKING EMER LIGHTS IN ARM, PER AOM, ALL EMER EXIT SIGN LIGHTS SHOULD BE ILLUMINATED. THE EXIT SIGN ABO - [SDR DXTA2025032102747](https://openairdocs.org/sdr/DXTA2025032102747), Mar 19, 2025: DOOR. OUT OF ADJUST. CREW IS UNABLE TO CLOSE THE MAIN ENTRY DOOR FROM THE INSIDE. CREW WAS ABLE TO CLOSE THE DOOR FROM THE OUTSIDE BUT HAD TO USE EXCESSIVE FORCE CORRECTIVE ACTION; - [SDR DXTA2025012702078](https://openairdocs.org/sdr/DXTA2025012702078), Jan 22, 2025: WIRE HARNESS. DEFECTIVE. GEAR POSITION & WARNING: AMBER GROUND DETECT FAULT HAS PERIODICALLY ILLUMINATED AND EXTINGUISHED MULTIPLE TIMES DURING THE PAST THREE FLIGHTS. ON THE LAST DEPAR - [SDR DXTA2024112701274](https://openairdocs.org/sdr/DXTA2024112701274), Nov 24, 2024: DOOR. LACK OF LUBE. HARD TO LATCH CLOSE/OPEN. STICKS IN THE CLOSED POSITION AFTER UNLOCKING REQUIRING MOTIVATION TO OPEN. DURING VISUAL INSPECTION OF DOOR, FOUND MAIN DOOR PINS DIR - [SDR DXTA2024111501126](https://openairdocs.org/sdr/DXTA2024111501126), Nov 12, 2024: BATTERY PACK. NO TEST. EMERGENCY LIGHTS BATTERY: EMERGENCY LIGHTS DO NOT TURN ON WITH SWITCH IN ARMED POSION DURRING PREFLIGHT TEST. CHARGED THE EMERGENCY BATTERIES PER QRH PROCEDURE - [SDR DXTA2024110401013](https://openairdocs.org/sdr/DXTA2024110401013), Oct 31, 2024: LIGHT. NO DISCREPANCY. EMERGENCY LIGHTING: EMER LIGHTS AND PAX SAFETY LIGHTS STAY ON NO MATTER WHAT POSITION THEY ARE IN. CORRECTIVE ACTION; OPERATED EMERGENCY LIGHTS. ALL LIGHTS OPER - [SDR DXTA2024062412137](https://openairdocs.org/sdr/DXTA2024062412137), Jun 22, 2024: DOOR. BINDING. MAIN DOOR: MAIN CABIN DOOR DIFFICULT TO CLOSE. FEELS LIKE IT IS BINDING. DOOR OPENS NORMALLY. INSPECT THE CABIN DOOR LATCH /LOCK SYSTEM, FOUND THE BOTTOM PINS O ## Service difficulty reports on N846QS not matched to an aircraft (13) They name N846QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR JGVR20170627004](https://openairdocs.org/sdr/JGVR20170627004), Jun 26, 2017: SUPPORT. WORN. ELEVATOR BELLCRANK ATTACHMENT BOLT HAS EXCESSIVE PLAY. FOUND WHILE PERFORMING TASK 27-31-00-211 ELEVATOR LINKAGE INSPECTION. THIS IS PART OF THE PHASE 5 INSPECT - [SDR JGVR20170627003](https://openairdocs.org/sdr/JGVR20170627003), Jun 26, 2017: RIVET. SHEARED. RIVET WITH MISSING THE HEAD ON VERTICAL STABILIZER AFT SPAR LT LOWER SUPPORT ANGLE. REPLACED THE RIVET. - [SDR JGVR20170627002](https://openairdocs.org/sdr/JGVR20170627002), Jun 26, 2017: STRUT. CORRODED. DURING REMOVAL OF NLG STRUT FOR REPACK, FOUND THE UPPER BARREL TO BE CORRODED AND HAVE DEEP PITTING. REMOVED THE CORRODED NLG UPPER BARREL AND INSTALLED A NEW S - [SDR JGVR20170627001](https://openairdocs.org/sdr/JGVR20170627001), Jun 26, 2017: SKIN. ERODED. VERTICAL STAB CAP LEADING EDGE IS ERODED THROUGH THE SURFACE SKIN. REPAIRED. - [SDR DXTA2016092806311](https://openairdocs.org/sdr/DXTA2016092806311), Sep 28, 2016: CONTROLLER. MALFUNCTIONED. AFTER TAKEOFF, CABIN CLIMBED TO 4500 FT, BEHIND ACFT ALTITUDE. CABIN ALT DECREASE DOWN TO 2000 FT. CONTINUED TO CLIMB UP TO 40,000 FT, NOTICED CABIN RATE SHOWED - [SDR DXTA2015061506030](https://openairdocs.org/sdr/DXTA2015061506030), Jun 14, 2015: UNKNOWN. ODOR. BEFORE CONNECTING BATTERY, SMELLED AN ELECTRICAL BURNING ODOR IN THE AFT TAIL CONE AREA. INSPECTED TAILCONE FOR ANY EVIDENCE OF CHARRING OR BURNING. RAN AIR COM - [SDR DXTA2013091605504](https://openairdocs.org/sdr/DXTA2013091605504), Sep 14, 2013: UNKNOWN. UNKNOWN. AFTER TAKEOFF, GEAR SELECTED UP BUT REMAINED DOWN. GEAR HANDLE TOUCHED, AND GEAR CAME UP. JACKED A/C COMPLETED SEVERAL GEAR SWINGS MOVED HANDLE FAST AND SLOW. N - [SDR DXTA2011120104810](https://openairdocs.org/sdr/DXTA2011120104810), Nov 30, 2011: BOLT. MISSING. LANDING GEAR DID NOT RETRACT WHEN GEAR HANDLE WAS SELECTED UP. INDICATION WAS 3 GREEN WITH A RED LIGHT. WHEN THE GEAR HANDLE WAS REPLACED IN THE DOWN POSITION, - [SDR DXTA2010091704240](https://openairdocs.org/sdr/DXTA2010091704240), Sep 16, 2010: BRAKE. FIRE. ACFT TAXIED OUT AND NOTICED THAT IT FELT LIKE A FLAT TIRE. TOWER ADVISED THAT THE TIRE WAS FLAT AND THERE WAS SMOKE COMING FROM IT. LT BRAKE WAS ON FIRE AND WAS - [SDR DXTA2010082304200](https://openairdocs.org/sdr/DXTA2010082304200), Aug 22, 2010: BULB. INOPERATIVE. WHEN LANDING GEAR WAS EXTENDED, LT MAIN INDICATOR LIGHT DID NOT ILLUMINATE. PERFORMED ROTARY TEST AND INDICATOR LIGHT DID NOT ILLUMINATE. EMERGENCY CHECKLIST WA - [SDR CNQ3200902](https://openairdocs.org/sdr/CNQ3200902), Dec 4, 2009: DUCT. CHAFED. FOUND WIRE BUNDLE THAT ORIGINATES IN THE BOTTOM OF THE AFT J-BOX AND RUNS HORIZONTALLY THROUGH BULKHEAD VERTICLE SUPPORT STRUCTURE FEED-THROUGH HOLE TOWARD ORAN - [SDR 2009FA0001014](https://openairdocs.org/sdr/2009FA0001014), Dec 3, 2009: CABIN PRESSURE. MALFUNCTIONED. PRESSURIZATION FAILED DURING THE DESCENT. SYS WAS IN NORMAL, DIFFERENTIAL PRESSURE DROPPED TO NEAR ZERO, AND THE CONTROLLER RATE INDICATED ZERO THROUGHOUT. ATTE - [SDR 2009FA0000944](https://openairdocs.org/sdr/2009FA0000944), Oct 29, 2009: WARNING LIGHT. ILLUMINATED. RIGHT NOSE BAGGAGE ANNUNCIATOR ILLUMINATED IN FLIGHT. ## 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.