# N841QS: 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: 700-0088 - Year built: 2023 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: March 1, 2023 - Certificate issued: April 20, 2026 - Expires: April 30, 2033 - Mode S code: AB84FF - Owner type: Co-owned, fractional ownership - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=841QS - Page: https://openairdocs.org/aircraft/N841QS 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 N841QS. ## FAA accident and incident reports None matched to N841QS. ## Service difficulty reports (8) 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 DXTA2026081409273](https://openairdocs.org/sdr/DXTA2026081409273), Aug 13, 2026: SQUAT SWITCH. OUT OF RIG. ON DEPARTURE NOSE WHEEL GEAR WOULD NOT RETRACT . FOLLOWED THE QRH AND MANUALLY DEPLOYED THE GEAR. RIGGED SG014 SQUAT SWITCH AND TIGHTENED UPLOCK SWITCH AND PROP - [SDR DXTA2026071008729](https://openairdocs.org/sdr/DXTA2026071008729), Jul 7, 2026: SQUAT SWITCH. FAULTED. ON DEPARTURE, SELECTED GEAR UP AND RECEIVED 4-5 AMBER CAS MSGS, INCLUDING GEAR DISAGREE L N R. GEAR SHOWED AMBER DN ON NOSE, AND YELLOW HASHING ON LEFT AND RIGH - [SDR 2025FA0000353](https://openairdocs.org/sdr/2025FA0000353), May 13, 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 DXTA2025020502204](https://openairdocs.org/sdr/DXTA2025020502204), Feb 2, 2025: BRAKE ASSY. MALFUNCTIONED. MLG BRAKE PRESSURE: EXCESSIVE FORCE MUST BE APPLIED TO BRAKE PEDALS TO STOP AIRCRAFT AFTER LANDING. BRAKES FEEL LIKE THERE IS RESISTANCE OR BACK PRESSURE. NO DI - [SDR DXTA2024091200507](https://openairdocs.org/sdr/DXTA2024091200507), Sep 10, 2024: BATTERY PACK. NO TEST. EMERGENCY LIGHTING: ALL EMERGENCY LIGHTS INTERIOR, AND EXTERIOR DO NOT COME ON DURING FIRST FLIGHT OF THE DAY TEST IN THE ON POSITION CORRECTIVE ACTION: REMOVED - [SDR DXTA2024070812291](https://openairdocs.org/sdr/DXTA2024070812291), Jul 8, 2024: BATTERY PACK. NO TEST. EMERGENCY LIGHTS DO NOT OPERATE IN THE ARM POSITION. THE EMEGENCY LIGHTS OPERATE IN THE ON POSITION. ACCOMPLISHED THE PROCEDURE EMERGENCY LIGHTS FAIL PREFLIGHT - [SDR DXTA2024032211273](https://openairdocs.org/sdr/DXTA2024032211273), Mar 22, 2024: LATCH. STIFF. MAIN CABIN DOOR LATCH IS STIFF & DIFFICULT TO LATCH CLOSED & UNLATCH, WHETHER OPENING/CLOSING DOOR FROM INSIDE OR OUTSIDE THE ACFT. PERFORMED DOOR OPEN & CLOSE - [SDR DXTA2024030711116](https://openairdocs.org/sdr/DXTA2024030711116), Mar 5, 2024: DOOR. OBSTRUCTED. CABIN BEGAN DEPRESSURIZING AT APPROX 14,000' WHILE TO 17,000' . LOUD AIR SOUND LT SIDE OF ACFT DURING DEPRESSURIZATION. AMBER FOLLOWED BE RED CABIN ALT CAS. SHO ## Service difficulty reports on N841QS not matched to an aircraft (15) They name N841QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DXTA2015082706067](https://openairdocs.org/sdr/DXTA2015082706067), Aug 26, 2015: BRAKE. ODOR. ON DEPARTURE BURNING ODOR NOTICED IN THE COCKPIT. ON LANDING, BURNING ODOR APPEARED TO BE COMING FROM RT WHEEL BRAKE. REMOVED RT MLG WHEEL ASSEMBLY, VISUALLY IN - [SDR DXTA2013080505465](https://openairdocs.org/sdr/DXTA2013080505465), Aug 4, 2013: RELAY. FAILED. AFTER LANDING AND TAXIING TO RAMP, POWER BRAKES CIRCUIT BREAKER TRIPPED. RECEIVED A LOW BRAKE PRESSURE AND ANTI-SKID INOPERATIVE ILLUMINATED. NORMAL BRAKE FAILE - [SDR DXTA2013071205443](https://openairdocs.org/sdr/DXTA2013071205443), Jul 11, 2013: BULB. INOPERATIVE. RIGHT SIDE LANDING LIGHT INOPERATIVE. FOUND CIRCUIT BREAKER HT008 TRIPPED. FOUND BULB BAD. R & R WITH NEW BULB IAW MM 33-42-01. OPS CHECKED NORMAL. - [SDR DXTA2012123105223](https://openairdocs.org/sdr/DXTA2012123105223), Dec 30, 2012: MOTOR. FAILED. NORMAL LANDING. DURING TAXI HAD TOTAL BRAKE FAILURE WITH LOW BRAKE & ANTISKID INOPERATIVE LIGHT AND POWER BRAKES CIRCUIT BREAKER OUT. USED EMERGENCY BRAKE TO ST - [SDR CWQR2011120632](https://openairdocs.org/sdr/CWQR2011120632), Dec 6, 2011: TORQUE TUBE. CRACKED. DURING A SCHEDULED MX CHECK WE FOUND THIS RT LANDING GEAR TORQUE TUBE CRACKED AT THE MOUNT BOLT PIVOT PLATE WHERE IT IS WELDED TO THE TUBE. THIS WAS FOUND VISUA - [SDR CWQR2011120531](https://openairdocs.org/sdr/CWQR2011120531), Dec 5, 2011: CABLE ASSY. WORN. DURING AN INSPECTION, FOUND CABLE SAWING INTO THE RUDDER SERVO BRACKET GUARD. THE CABLE WAS FLATTENED AND HAD BROKEN STRANDS. THE CABLE GUARD WAS GROOVED. THE C - [SDR CWQR2011120530](https://openairdocs.org/sdr/CWQR2011120530), Dec 5, 2011: DRAG ANGLE. CRACKED. DURING SCHEDULED MX THE WING TO FUSELAGE FAIRINGS WERE REMOVED. FOUND 3 LOCK FASTNERS FROM THE WING SKIN TO DRAG ANGLE, WITH CRACKS IN THE DRAG ANGLE BRACKET. T - [SDR CWQR2011120529](https://openairdocs.org/sdr/CWQR2011120529), Dec 5, 2011: DRAG ANGLE. CRACKED. DURING SCHEDULED MX, FOUND 3 LOCK FASTENERS FROM THE WING SKIN TO DRAG ANGLE, WITH CRACKS IN THE DRAG ANGLE BRACKET. THE CRACKS ON THE DRAG ANGLE WERE HORIZONTA - [SDR DXTA2011021404465](https://openairdocs.org/sdr/DXTA2011021404465), Feb 13, 2011: LAMP. INOPERATIVE. GREEN "RT" GEAR DOWN INDICATOR LIGHT DID NOT COME ON AFTER THE GEAR HANDLE WAS PLACED DOWN. REPLACED RT GEAR INDICATOR LAMP WITH NEW IAW MM 31-40-00. OPS CHECK - [SDR DXTA2010072604173](https://openairdocs.org/sdr/DXTA2010072604173), Jul 25, 2010: DISPLAY. MALFUNCTIONED. PFD NR 2 FAILED ON TAKEOFF ROLL. CB IS POPPED. REMOVED CB PANEL, INSPECTED CIRCUIT BREAKERS AND WIRING. NOTED CB AND WIRING WERE IN GOOD CONDITION. CLOSED CB PA - [SDR DXTA2009120703883](https://openairdocs.org/sdr/DXTA2009120703883), Dec 4, 2009: DISPLAY. FAILED. LT PFD FAILED ACCOMPINIED BY ELECTRICAL ODOR. REMOVED LT PFD INSPECTED AREA AND FOUND NO DEFECTS TO WIRING OR PLUGS. ELECTRICAL ODOR EMINATED FROM PFD. INSTALLE - [SDR DXTA2009101203810](https://openairdocs.org/sdr/DXTA2009101203810), Oct 11, 2009: SKIN. DAMAGED. ON LANDING ROLL OUT AT APPROXIMATELY 80 KTS, ACFT STRUCK DEER. DAMAGE TO WING LEADING EDGE (RT). DRILLED & REMOVED FLAP ISLAND TOP SKIN & LOWER AFT SKIN DRILLED - [SDR DXTA2009031703553](https://openairdocs.org/sdr/DXTA2009031703553), Mar 17, 2009: BRAKE ASSY. MALFUNCTIONED. DURING LANDING WITH BRAKES APPLIED, LEFT BRAKE PEDAL FELT LIKE PULSATING HARD, TURNING A/C TO LEFT. RT PEDAL DID NOT SEEM EFFECTIVE. UPON ARRIVAL EXAMINED ANTI- - [SDR DXTA2009021803515](https://openairdocs.org/sdr/DXTA2009021803515), Feb 18, 2009: CONTROL BOX. INOPERATIVE. REMOVED AND REPLACED ANTISKID CONTROL UNIT ASSY. OP CHECKS SATISFACTORY. ALL WORK DONE IAW MM 32-41-08. - [SDR DXTA2009021903515](https://openairdocs.org/sdr/DXTA2009021903515), Feb 18, 2009: BRAKE ASSY. MALFUNCTIONED. UPON TOUCHDOWN AND INITIAL BRAKE APPLICATION, HEARD A POPPING NOISE. RT BRAKE GRABBED HARD YAWNING ACFT TO THE RT. ## 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.