# N822QS: 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: 700-0060 - Year built: 2021 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: November 4, 2021 - Certificate issued: December 8, 2021 - Expires: December 31, 2028 - Mode S code: AB39B8 - Owner type: Co-owned - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=822QS - Page: https://openairdocs.org/aircraft/N822QS 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 N822QS. ## FAA accident and incident reports None matched to N822QS. ## 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 DXTA2026060108265](https://openairdocs.org/sdr/DXTA2026060108265), May 28, 2026: WIRE HARNESS. MALFUNCTIONED. ON DEPARTURE OUT OF KTEB AFTER CALLING FOR "GEAR UP" THE FO TRIED TO RETRACT THE GEAR. THE HANDLE SEEM LIKE IT WAS LOCKED INTO PLACE AND WOULD NOT MOVE FROM THE - [SDR DXTA2025102105355](https://openairdocs.org/sdr/DXTA2025102105355), Oct 17, 2025: TRANSDUCER. FAULTED. RED CAS HYD O' TEMP B MESSAGE CAME ON IN FLIGHT CORRECTIVE ACTION: REMOVED FAULTY HYDRAULIC TEMPERATURE TRANSDUCER ON SYSTEM B RESERVOIR AND REPLACED WITH A CUS - [SDR DXTA2025042503196](https://openairdocs.org/sdr/DXTA2025042503196), Apr 24, 2025: SQUAT SWITCH. FAULTED. AFTER POSITIVE RATE PM ATTEMPTED TO RETRACT GEAR. HE COULD NOT GET THE HANDLE TO MOVE. SHORTLY AFTER RECEIVED AN AMBER GROUND DETECT FAULT. THE GEAR WAS NEVER R - [SDR 2024F00171](https://openairdocs.org/sdr/2024F00171), Jul 22, 2024: ACCESS DOOR. CORRODED. RH APU ACCESS PANEL (331CR) HAS LEVEL 2 CORROSION AND CRACK AT FASTENER HOLE - [SDR DXTA2023060587880](https://openairdocs.org/sdr/DXTA2023060587880), Jun 5, 2023: UNKNOWN. UNKNOWN. ON TAKE OFF, UNABLE TO RETRACT THE LANDING GEAR. SEQUENTIALLY "GROUND DETECT FAULT " CAS APPEARED. FERRIED THE AIRPLANE WITH THE GEAR DOWN. USING ARES VIEW TO T - [SDR DXTA2023060187590](https://openairdocs.org/sdr/DXTA2023060187590), May 31, 2023: UNKNOWN. UNKNOWN. MAIN DOOR: CLIMBING THROUGH 13K GOT AMB CABIN ALT. DECENDING TO 13K GOT RED CABIN ALT AND AMBER CHECK DOORS AND CABIN DOOR OPEN. DIVERTED AND LANDED UNEVENTFUL. - [SDR DXTA2023052687090](https://openairdocs.org/sdr/DXTA2023052687090), May 25, 2023: UNKNOWN. UNKNOWN. WE HAD TO RESET DOOR 2X, ALSO STIFF TO CLOSE AND STIFF TO OPEN SOMETIMES. PERFORMED CLEANING OF THE INTERIOR DOOR ANDLE RELEASE SWITCH AND MODEL 700 MAINTENANCE - [SDR DXTA2023041183990](https://openairdocs.org/sdr/DXTA2023041183990), Apr 10, 2023: UNKNOWN. UNKNOWN. MAIN DOOR HANDLE: MAIN CABIN DOOR EXTREMELY DIFFICULT TO OPEN. REQUIRES INORDINATE STRENGTH TO OPEN IT FROM THE INSIDE AND OUTSIDE OF THE CABIN. TROUBLE SHOT DO - [SDR DXTA2023020679960](https://openairdocs.org/sdr/DXTA2023020679960), Feb 4, 2023: NOT REPORTED. NOT REPORTED. EMERGENCY LIGHTING: ON PREFLIGHT NONE OF THE EMERGENCY LIGHTS WORK. //SIGNOFF// CHARGED BATTERIES FOR 2 HRS WAITED 1/2 HR AND OPS CHECK LIGHTS WITH GOOD RESULTS - [SDR DXTA2022120675610](https://openairdocs.org/sdr/DXTA2022120675610), Dec 5, 2022: CONNECTOR. DAMAGED. WHEN CLOSING MAIN CABIN DOOR FROM INSIDE AIRCRAFT, HANDLE DOES NOT POSITIVE DETENT AND CABIN DOOR DOOR OPEN AND CHECK DOOR CAS MESSAGES REMAIN DISPLAYED. CHECKL - [SDR DXTA2022030357800](https://openairdocs.org/sdr/DXTA2022030357800), Mar 3, 2022: WIRE HARNESS. DAMAGED. CABIN DOOR OPEN AMBER CAS: DEPARTING KAPF-KPTK CLIMBING THEOUGH 2000' WE GOT A AMBER: CABIN DOOR OPEN CASA FOLLOWED BY A CHECK DOORS AMBER CAS. WE STOPPED THE C - [SDR DXTA2021122754120](https://openairdocs.org/sdr/DXTA2021122754120), Dec 25, 2021: NONE. NONE. CABIN EMERG LIGHT: OVERHEAD CABIN EMERGENCY LIGHTS ARE INOP. // SIGNOFF// PERFORMED OPERATIONAL CHECK OF THE EMERGENCY LIGHTS AND IS GOOD IRW CE-700 AMM 33-50-0 ## Service difficulty reports on N822QS not matched to an aircraft (12) They name N822QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DXTR2014070901](https://openairdocs.org/sdr/DXTR2014070901), Jun 29, 2014: SKIN. DENTED. FOUND TWO DENTS IN FUSELAGE SKIN INBD AND FWD OF LT LOWER WING AND CRACK AT DOME NUT. ONE AT BS 254.35, PROTRUDING OUT 0.025" DEEP, 0.35" LONG, 0.20" WIDE, AND - [SDR DXTA2014071405818](https://openairdocs.org/sdr/DXTA2014071405818), Jun 19, 2014: RIB. CRACKED. RIGHT WING HAS CRACKED RIB IN THE OTBD FLAP WELL WS 133.07. COMPLIED WITH THE RT WING RIB REPAIR IAW THE ERO-555540QC. ACCOMPLISHED EDDY CURRENT INSPECTION OF R - [SDR DXTA2014071405817](https://openairdocs.org/sdr/DXTA2014071405817), Jun 19, 2014: RIB. CRACKED. LEFT WING HAS CRACKED RIB IN THE INBD FLAP WELL WS 79.06. REPAIRED LT WING RIB IN THE INBD FLAP WELL AT WS 79.06 IAW ERO-585141-2 INSPECTED 6. ACCOMPLISHED EDDY - [SDR DXTA2013050805381](https://openairdocs.org/sdr/DXTA2013050805381), Apr 26, 2013: LINER. UNSERVICEABLE. BORESCOPE INSPECTION OF COMBUSTION CHAMBER LINER HARDWARE IAW SI 35-2013 INSTRUCTIONS. LINER FAILED INSPECTION WITH ONE NUT CONDITION "C" MISSING. ENGINE DISASS - [SDR DXTR20120117003](https://openairdocs.org/sdr/DXTR20120117003), Jan 17, 2012: FUEL LINE. CHAFED. RT REFUEL/DEFUEL FLOW TUBE ASSY IS CHAFED BEYOND LIMITS. - [SDR DXTR20120113002](https://openairdocs.org/sdr/DXTR20120113002), Jan 13, 2012: INLET. CRACKED. RT ENGINE INLET IS CRACKED 2X (1 & 5 O'CLOCK POSITIONS) ON THE OUTER DUCT & FLANGE ATTACH POINTS. - [SDR DXTR20120113001](https://openairdocs.org/sdr/DXTR20120113001), Jan 13, 2012: DOOR. STUCK. THE EMERGENCY EXIT DOOR WILL NOT RELEASE FROM AIRFRAME WHEN THE HANDLE IS TURNED AND PULLED. EXCESSIVE FORCE WAS REQUIRED TO OPEN. - [SDR DXTA2011111104781](https://openairdocs.org/sdr/DXTA2011111104781), Nov 10, 2011: DUCT. DISCONNECTED. LEVEL AT FL400, NOTICED ACRID ODOR OF ELECTRICAL AND SMALL AMOUNT OF HAZE IN THE AIR: COMING FROM REAR OF CABIN BY THE LAV. DID EMERGENCY DESCENT AND LANDED. BO - [SDR DXTA2011100404743](https://openairdocs.org/sdr/DXTA2011100404743), Oct 4, 2011: MOTOR. FAILED. WHILE ACFT ELECTRICAL WAS POWERED ON GROUND WITH GPU, SMOKE DETECTED COMING FROM LOWER LOUVERS BENEATH AFT EQUIPMENT BAY ALONG WITH A STRONG ELECTRICAL BURNING - [SDR CWQR20110617001](https://openairdocs.org/sdr/CWQR20110617001), Jun 17, 2011: CONTROL CABLE. WORN. DURING AN INSP, THE RUDDER CABLE ASSY WAS FOUND TO HAVE BEEN SAWING INTO THE RUDDER SERVO BRACKET CABLE GUARD. THIS HAS BEEN DOING THIS SINCE THE ACFT WAS MANUF - [SDR DXTA2010112904334](https://openairdocs.org/sdr/DXTA2010112904334), Nov 28, 2010: WARNING LIGHT. FALSE ACTIVATION. LEFT ENGINE FUEL FILTER BYPASS ANNUNCIATOR ILLUMINATED OUT OF 27,000 ON CLIMB OUT, SHORTLY AFTER RT SIDE ILLUMINATION. RT FUEL FILTER BYPASS ANNUNCIATOR ILLUMIN - [SDR DXTA2009081303756](https://openairdocs.org/sdr/DXTA2009081303756), Aug 12, 2009: PRESSURE SWITCH. FAILED. LANDING ROLLOUT LESS THAN 40 KTS LOW BRAKE PRESSURE/ANTI SKID LIGHT ILLUMINATED. MAKING TURN ONTO TAXIWAY BRAKES FAILED. REQUIRED TUG INTO FBO AND NOTICED BRAKE ## 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.