# N811QS: 2021 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: 700-0046 - Year built: 2021 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: May 3, 2021 - Certificate issued: June 12, 2026 - Expires: June 30, 2033 - Mode S code: AB0E82 - Owner type: Co-owned - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=811QS - Page: https://openairdocs.org/aircraft/N811QS 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 N811QS. ## FAA accident and incident reports None matched to N811QS. ## Service difficulty reports (20) 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 DXTA2026102110289](https://openairdocs.org/sdr/DXTA2026102110289), Oct 20, 2026: DOOR. NO DISCREPANCY. DOOR HANDLE IS HARD TO CLOSE. ( PULL DOWN ) WHEN PULLING IN ON DOOR MAKES IT A LITTLE EASIER BUT STILL STIFF. COMPLIED WITH CABIN DOOR OPS CHECK DUE TO DOOR HAN - [SDR DXTA2026022006939](https://openairdocs.org/sdr/DXTA2026022006939), Feb 18, 2026: ACTUATOR. FAULTED. GETTING GEAR DOOR OPEN MOMENTARILY AFTER GEAR RETRACTION. LASTS ANYWHERE FROM 1 TO 5 SECONDS. REMOVED DEFECTIVE NOSE LANDING GEAR ACTUATOR P/N 9914676-4, S/N 00 - [SDR 2025FA0000826](https://openairdocs.org/sdr/2025FA0000826), Dec 12, 2025: INLET. DETERIORATED. RIGHT ENGINE INLET MESH DETERIORATION - [SDR 2025FA0000825](https://openairdocs.org/sdr/2025FA0000825), Dec 12, 2025: INLET. DETERIORATED. LEFT ENGINE INLET MESH DETERIORATION - [SDR 2025FA0000824](https://openairdocs.org/sdr/2025FA0000824), Dec 12, 2025: INLET. DETERIORATED. LEFT ENGINE INLET MESH DETERIORATION. - [SDR 2025FA0000819](https://openairdocs.org/sdr/2025FA0000819), Dec 11, 2025: ATTACH FITTING. CHAFED. FUSELAGE TO RT WING ATTACHMENT FITTING CHAFED. - [SDR 2025FA0000818](https://openairdocs.org/sdr/2025FA0000818), Dec 11, 2025: REVERSER HALF. CORRODED. RH THRUST REVERSER UPPER DOOR SHOWS SIGNS OF CORROSION. - [SDR 2025FA0000817](https://openairdocs.org/sdr/2025FA0000817), Dec 11, 2025: REVERSER HALF. CORRODED. RH THRUST REVERSER LOWER DOOR SHOWS SIGNS OF CORROSION. - [SDR 2025FA0000816](https://openairdocs.org/sdr/2025FA0000816), Dec 11, 2025: REVERSER HALF. CONTAMINATED. LH THRUST REVERSER UPPER DOOR SHOWS SIGNS OF CORROSION. - [SDR 2025FA0000815](https://openairdocs.org/sdr/2025FA0000815), Dec 11, 2025: REVERSER HALF. CORRODED. LH THRUST REVERSER LOWER DOOR SHOWS SIGNS OF CORROSION. - [SDR DXTA2025112005773](https://openairdocs.org/sdr/DXTA2025112005773), Nov 20, 2025: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHT BATTERY PACK, NOT HOLDING CHARGE PERFORMED QRH CHARGE PROCEDURE TWICE CORRECTIVE ACTION: REMOVED LT AFT EMERGENCY BATTERY DUE TO NOT HOLDING CHA - [SDR DXTA2025051103450](https://openairdocs.org/sdr/DXTA2025051103450), May 11, 2025: HANDLE. NO DISCREPANCY. MAIN DOOR HANDLE: MED INTERIOR HANDLE IS HARD TO CLOSE AND STIFF FOR OPENING CORRECTIVE ACTION: INSPECTED PAX MAIN DOOR HANDLE IN CABIN AND FOUND NO DEFECTS WIT - [SDR DXTA202401100688](https://openairdocs.org/sdr/DXTA202401100688), Sep 27, 2024: SQUAT SWITCH. DEFECTIVE. NLG LANDING GEAR RETRACTION: AFTER ROTATION GEAR WOULD NOT COME UP. COMPLETED CHECKLISTS AND RECOVERED GEAR DOWN. UNDERWEIGHT LANDING AND EMERGENCY DECLARED FOR - [SDR DXTA2024093000682](https://openairdocs.org/sdr/DXTA2024093000682), Sep 27, 2024: SQUAT SWITCH. FAULTED. AFTER ROTATION GEAR WOULD NOT COME UP. COMPLETED CHECKLISTS AND RECOVERED GEAR DOWN. UNDERWEIGHT LANDING AND EMERGENCY DECLARED FOR POSSIBLE PAX EGRESS. CORRECT - [SDR 2024F00177](https://openairdocs.org/sdr/2024F00177), Jul 25, 2024: THRUST REVERSER. CORRODED. LH OUTBOARD THRUST REVERSER BEAM HAS PEELING PAINT. - [SDR 2024F00176](https://openairdocs.org/sdr/2024F00176), Jul 25, 2024: THRUST REVERSER. CORRODED. RH INBOARD THRUST REVERSER BEAM HAS PEELING PAINT. - [SDR DXTA2024021210879](https://openairdocs.org/sdr/DXTA2024021210879), Feb 12, 2024: BATTERY. FAULTED. WHEN CONDUSTING THE POWER ON CHECKLIST THE EMERGENCY LIGHTS DO NOT TEST PROPERLY. IN THE ON POSITION LIGHTS ILLUMINATE. IN THE ARM POSITION THE LIGHTS WILL NOT - [SDR DXTA2024011110580](https://openairdocs.org/sdr/DXTA2024011110580), Jan 11, 2024: UNKNOWN. UNKNOWN. EMERG LIGHT SWITCH: WHILE PREFORMING POWER ON CHECKLIST: EMERG LIGHT SWITCH WHEN IN THE ON POSITION THE LIGHTS ILLUMINATE. WHEN IN THE ARM POSITION ALL LIGHTS E - [SDR DXTA2023110299550](https://openairdocs.org/sdr/DXTA2023110299550), Nov 1, 2023: UNKNOWN. UNKNOWN. EMERGENCY LIGHTS BATTERY: EMERGENCY BATTERY LIGHTS WILL NOT ILLUMINATE WHEN NO POWER IS ON THE AIRCRAFT AND EMER LIGHTS ARE SELECTED TO ARM. PERFORMED EMERGENCY - [SDR DXTA2023012579110](https://openairdocs.org/sdr/DXTA2023012579110), Jan 24, 2023: AUTOTHROTTLE SYS. FAULTED. ON TAKEOFF THE AIRPLANE TOOK AN UNUSUAL AMOUNT OF DOWNWARD TRIM TO KEEP THE NOSE IN CONFIGURATION. DURING CLIMB-OUT WE WERE SEEING A -.2 ON THE TRIM, BUT STILL ## Service difficulty reports on N811QS not matched to an aircraft (12) They name N811QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DXTA2016101206318](https://openairdocs.org/sdr/DXTA2016101206318), Oct 12, 2016: WIRE HARNESS. FAULTED. CLIMBING THROUGH 11,000 FEET AT 93 % N1, THE NR 1 ENGINE COMPUTER LIGHT ILLUMINATED. THE LEFT ENGINE ROLLED BACK APRX 20 % N1. QRH CHECKLIST WAS COMPLETED. LIGH - [SDR DXTA2014022005661](https://openairdocs.org/sdr/DXTA2014022005661), Feb 19, 2014: BRAKE SYS. CONTAMINATED. LEFT & RT WHEEL BRAKE PEDALS ON LT PILOTS SIDE HAVE EXCESSIVE TRAVEL ALMOST TO THE FLOORBOARD WHEN WHEEL BRAKES APPLIED UPON LANDING. PEDALS HAVE A VERY SPONGY - [SDR DXTA2012082005098](https://openairdocs.org/sdr/DXTA2012082005098), Aug 18, 2012: MASTER CYLINDER. FAILED. PILOT'S SIDE RT BRAKE PEDAL DEPRESSES ALL THE WAY TO THE STOP. ONLY MINIMAL PRESSURE SHOWING ON THE GUAGE. NO BRAKING AVAILABLE FROM RT PEDAL. FOUND PILOTS RT M - [SDR DXTA2012081005084](https://openairdocs.org/sdr/DXTA2012081005084), Aug 9, 2012: BRAKE. WEAK. RIGHT BRAKE IS SPONGY, COMPARED TO THE LEFT. BLED RIGHT BRAKES INBD AND OTBD IAW AMM 32-40-00. OPS CHECKED GOOD. - [SDR DXTA2011011804412](https://openairdocs.org/sdr/DXTA2011011804412), Jan 16, 2011: UNKNOWN. UNKNOWN. LOUD SNAP SOUND IN COCKPIT FOLLOWED BY RED MASTER WARNING. NO ASSOCIATED ANNUNCIATORS; CANCELED THE WARNING. CHECKED CIRCUIT BREAKERS, AMPS, VOLTS; ALL NORMAL. - [SDR DXTA2010102004267](https://openairdocs.org/sdr/DXTA2010102004267), Oct 19, 2010: MASTER CYLINDER. LEAKING. NO LT BRAKE PSI WHEN BRAKE PEDAL APPLIED. LT BRAKE PEDAL GOES ALL THE WAY TO STOP. RT BRAKE WORKS NORMAL. FOUND THE PILOTS LT MASTER CYLINDER LEAKING EXTERNALLY - [SDR DXTA2010030304011](https://openairdocs.org/sdr/DXTA2010030304011), Mar 2, 2010: RECEPTACLE. LOOSE. IN FLIGHT WE LOST ALL COMMUNICATIONS, APPEARED TO BE STUCK MIC ON CAPTAINS SIDE. WHEN WE SWITCHED RADIOS IT FOLLOWED TO NEXT RADIO. WE FINALLY WERE ABLE TO COMM - [SDR DXTA200803080](https://openairdocs.org/sdr/DXTA200803080), May 27, 2008: COMPENSATOR. MALFUNCTIONED. ON TAKEOFF, IMMEDIATELY AFTER APR WAS ARMED, BOTH N1 SPEEDS WENT TO 100.5 BUT LT CLIMBED TO 100.7, ABORTED TAKE OFF. - [SDR DXTA20082892](https://openairdocs.org/sdr/DXTA20082892), Feb 21, 2008: DOWNLOCK SWITCH. INOPERATIVE. AFTER TAKEOFF, GOT RED NOSE GEAR RT GEAR AND LT GEAR INDICATIONS ALSO GREEN LT GEAR INDICATION. REPLACED LT GEAR DOWN LOCK SWITCH IAW MM 32-60-00. OPS CHECKS GO - [SDR DXTA200702169](https://openairdocs.org/sdr/DXTA200702169), May 1, 2007: UNKNOWN. MALFUNCTIONED. ENG NR 1 FUEL AND FUEL LOOK UP LIGHT CAME ON DURING T/O ROLL. T/O ABORTED AT APPROX 60 KTS, LIGHT WENT OUT WITH THROTTLES REDUCTION. REPLACED BOTH FUEL FILTERS - [SDR DXTA200400422](https://openairdocs.org/sdr/DXTA200400422), Oct 11, 2004: FILTER. FAULTY. ENGINE 1 FUEL LIGHT ILLUMINATED ON TAKEOFF AT 60KTS. REMOVED FILTER AND SHIPPED TO HONEYWELL FOR TEST. INSTALLED NEW FILTER, OPERATED ENGINE ON GROUND THROUGH V - [SDR DXTA200400416](https://openairdocs.org/sdr/DXTA200400416), Oct 5, 2004: FUEL FILTER. ACTIVATED. ENG 2 FUEL ANNUNCIATOR LIGHT CAME ON DURING TAKEOFF ROLL. REPLACED THE NR 2 FUEL FILTER IAW TFE-731-5 HONEYWELL LMM CHAPT 73-21-02, LEAK CHECK GOOD. ## 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.