# N817QS: 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: 700-0052 - Year built: 2021 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: July 29, 2021 - Certificate issued: June 25, 2026 - Expires: June 30, 2033 - Mode S code: AB24CC - Owner type: Co-owned - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=817QS - Page: https://openairdocs.org/aircraft/N817QS 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 N817QS. ## FAA accident and incident reports None matched to N817QS. ## Reports on N817QS not matched to an aircraft (1) They name N817QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [Incident 20010921024989I](https://openairdocs.org/incident/20010921024989I), Sep 21, 2001: Raythn HAWKER800XP (N817QS), Salt Lake City, UT, Minor damage. (-23) On take-off, at rotation, the right inbd tire failed. Pieces of tire exited the wheel wel through the upper wing skin, breaking out a piece of the carbon… ## Service difficulty reports (6) 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 DXTA2026082809442](https://openairdocs.org/sdr/DXTA2026082809442), Aug 26, 2026: LIGHT. FAULTY. THE PATHWAY EMERGENCY LIGHT ON THE BASE OF SEAT 9 IS INOP. REMOVED CABIN LIGHT ASSY, INSTALLED NEW CABIN LIGHT ASSY. OPS CHECK GOOD. WORK PERFORMED IAW IMM 25-2 - [SDR 2023FA0000460](https://openairdocs.org/sdr/2023FA0000460), Aug 20, 2023: THRUST REVERSER. CORRODED. PROCEDURE TO REPAIR CORROSION DAMAGE AND RESTORING SURFACE PROTECTION ON THE BEAM INNER SKIN. REPAIR SCHEME NO. RS907-623 REV. A - [SDR DXTA2023062289110](https://openairdocs.org/sdr/DXTA2023062289110), Jun 20, 2023: BATTERY. DEFECTIVE. WITH MAIN BATTERIES CONNECTED AND BATTERIES OFF, EMER LIGHTS - ARM DOES NOT ILLUMINATE ANY EMERGENCY LIGHTS. WITH EMER LIGHTS - ON, ALL LIGHTS ILLUMINATE WITH T - [SDR DXTA2023060888170](https://openairdocs.org/sdr/DXTA2023060888170), Jun 7, 2023: UNKNOWN. UNKNOWN. EMERG EXIT SIGN/LIGHT: WITH BATTERIES OFF AND EMER SWITCH IN ARMED THERE ARE NO LIGHTS COMING ON. WHEN THE EMER SWITCH IS FLIPPED TO THE ON POSITION THE LIGHTS - [SDR DXTA2023032082790](https://openairdocs.org/sdr/DXTA2023032082790), Mar 17, 2023: HARNESS. DAMAGED. EXTENSION / RETRACTION: AFTER TAKEOFF LANDING GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. AT APPROXIMATELY 400' AMBER GROUND DETECT FAULT CAS ILLUMINATED FOL - [SDR DXTA2022050661330](https://openairdocs.org/sdr/DXTA2022050661330), May 5, 2022: HINGE. BROKEN. MAIN DOOR: MAIN CABIN DOOR TOP MOST STEP IS ELEVATED ABOUT 1 INCH ABOVE FLUSH. DEFINITE TRIP HAZARD. PICS ATTACHED. INSPECTED STEP RISER HINGES AND NOTED ALL TH ## Service difficulty reports on N817QS not matched to an aircraft (12) They name N817QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DXTA2011022804480](https://openairdocs.org/sdr/DXTA2011022804480), Feb 25, 2011: CHECK VALVE. FAILED. ACFT FAILED TO PRESSURIZE EVENLY; ALT WARNING HORN SOUNDED AND MASKED FELL AS WE CLIMBED THOUGH FL200. AFTER EMERGENCY DESCENT, APU WAS REENGAGED BUT EVEN THEN - [SDR DXTA2010090904228](https://openairdocs.org/sdr/DXTA2010090904228), Sep 8, 2010: TRANSDUCER. FLUCTUATES. NR 2 ENG SHUTDOWN IN FLT DUE TO FLUCTUATION OF N1, N2, & FUEL FLOW. FLUCTUATIONS INCREASED AS POWER DECREASED. PRIOR TO SHUTDOWN, ENG FLUCTATED 75-95 % N1. A SM - [SDR DXTA2010030104009](https://openairdocs.org/sdr/DXTA2010030104009), Feb 26, 2010: COMPUTER. FAILED. ELECTRIC PITCH TRIM WENT FULL NOSE DOWN WHEN LEVEL AT 38000. ELECTRIC PITCH TRIM CIRCUIT BREAKER WAS PULLED. ELECTRIC PITCH MOTOR CONTINUED TO RUN WITH CIRCUIT - [SDR DXTA2010021203982](https://openairdocs.org/sdr/DXTA2010021203982), Feb 11, 2010: ROLLER. OUT OF ADJUST. AFTER TAKEOFF AND GEAR RETRACTION PERFORMED, RED "R GEAR" ILLUMUNATED AND STAYED ILLUMINATED CONTINOUSLY UNTIL SUBSEQUENT GEAR EXTENSION. ADJUSTED RT MLG DOOR R - [SDR DXTA2010020803975](https://openairdocs.org/sdr/DXTA2010020803975), Feb 6, 2010: UPLOCK SWITCH. FAULTY. AFTER GEAR RETRACTION, RED 'R GEAR' ANNUNCIATOR REMAINED ILLUMINATED AND REMAINED ON WITH NO FLICKERING. PERFORMED ABNORMAL CHECKLIST, EXTENDED GEAR WITH ALL IN - [SDR DXTA2010020203966](https://openairdocs.org/sdr/DXTA2010020203966), Feb 1, 2010: UPLOCK SWITCH. OUT OF ADJUST. AFTER TAKEOFF RT GEAR UNSAFE LIGHT REMAINED ON. RECYCLED GEAR AND LIGHT REMAINED ON. AFTER EXTENDING GEAR, ALL INDICATIONS WERE NORMAL. ADJUSTED RT MLG UPLOCK S - [SDR DXTA2009101603812](https://openairdocs.org/sdr/DXTA2009101603812), Oct 15, 2009: ACTUATOR. FAILED. AILERON TRIM KNOB FROZEN IN NEUTRAL POSITION ,WILL NOT TURN. REMOVED AND REPLACED AILERON TRIM TAB ACTUATOR IAW MM 27-10-71, OPS CHECKS AND FUNCTIONAL CHECKS GO - [SDR DXTA200811113351](https://openairdocs.org/sdr/DXTA200811113351), Nov 11, 2008: SQUAT SWITCH. INOPERATIVE. LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. (HAD BEEN DEICED) FOUND CHAFING WIRES ON LT MLG SQUAT SWITCH AT UPPER TORQUE LINK. REMOVED LT SQUAT SWITCH AND INS - [SDR DXTA2008111203351](https://openairdocs.org/sdr/DXTA2008111203351), Nov 11, 2008: LANDING GEAR. MALFUNCTIONED. LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. - [SDR DXTA200808243241](https://openairdocs.org/sdr/DXTA200808243241), Aug 24, 2008: LANDING GEAR. LACK OF LUBE. AFTER TAKEOFF, GEAR WOULD NOT COME UP AND SQUAT SWITCH LIGHT CAME ON. STALL IDENT ALSO ON. SHORT FINAL SQUAT SWITCH LIGHT WENT OUT. COULD NOT MOVE HANDLE UP. LT - [SDR DXTA200400464](https://openairdocs.org/sdr/DXTA200400464), Dec 3, 2004: CONTROL LEVER. MALFUNCTIONED. RIGHT RED GEAR INDICATION ILLUMINATED WITH GEAR SELECTED UP. JACKED AIRCRAFT AND USED EXTERNAL HYDRAULIC CART TO SUPPLY FLUID TO GEAR SYSTEM. CYCLED GEAR NUMERO - [SDR DXT2001F00002](https://openairdocs.org/sdr/DXT2001F00002), Sep 24, 2001: TIRE. SEPARATED. GOODYEAR FLIGHT EAGLE PN 237K23-2, SN 10961491 FAILED ON TAKE-OFF. SEPARATED TREAD PENETRATED WING UPPER SURFACE, ALSO DAMAGED FUSELAGE SIDE FAIRING AND RIGHT E ## 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.