# N898QS: 2026 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: 700-0172 - Year built: 2026 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: July 27, 2026 - Certificate issued: October 8, 2026 - Expires: October 31, 2033 - Mode S code: AC647B - Owner type: Co-owned - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=898QS - Page: https://openairdocs.org/aircraft/N898QS 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 N898QS. ## FAA accident and incident reports None matched to N898QS. ## Reports on N898QS not matched to an aircraft (1) They name N898QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [Incident 20090619015119I](https://openairdocs.org/incident/20090619015119I), Jun 19, 2009: Raythn HAWKER800XP (N898QS), Van Nuys, CA, No damage. (-23) Honeywell primary flight display (PFD) failed, causing smoke in the flight compartment. ## Service difficulty reports None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. ## Service difficulty reports on N898QS not matched to an aircraft (10) They name N898QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DXTA2013100105523](https://openairdocs.org/sdr/DXTA2013100105523), Sep 30, 2013: UNKNOWN. ODOR. CREW SMELLED STRONG ELECTRICAL BURNING ODOR ACCOMPANIED BY HAZE IN COCKPIT AT 33000 FT. POWERED AIRCRAFT ELETRICAL TO DUPLICATE FAULT. FOUND CO-PILOTS MFD SCREE - [SDR DXTA2012022804892](https://openairdocs.org/sdr/DXTA2012022804892), Feb 24, 2012: RUDDER. INOPERATIVE. RUDDER PEDALS LOCKED UP AFTER APPROX 800FT AFTER TAKEOFF. A "MECHANICAL CLICK" WAS HEARD AT LOCK-UP. COULD NOT MOVE PEDALS WITH YAW DAMPER ON OR OFF. AUTOPILOT - [SDR E81R2012110232332](https://openairdocs.org/sdr/E81R2012110232332), Jan 10, 2012: FITTING. CORRODED. ON APPROACH, FLIGHT CREW NOTED AIRBRAKE WARNING INDICATION AFTER ACFT FULLY CONFIGURED FOR LANDING, WITH AIRBRAKE CONTROL LEVER FULLY FWD IN AIRBRAKES SHUT SETT - [SDR DXTA2011020104440](https://openairdocs.org/sdr/DXTA2011020104440), Jan 29, 2011: WHEEL. MALFUNCTIONED. UPON GEAR RETRACTION THE NOSE WHEEL ASSY TAKES A LONG TIME (35 OR 40SEC) TO SPIN DOWN. WHEN IT FINALLY DOES COME TO A STOP, THERE IS A MODERATE SHAKE AND ONE CA - [SDR DXTA2010031804040](https://openairdocs.org/sdr/DXTA2010031804040), Mar 17, 2010: FUEL CONTROL. FAULTY. ON CLIMBOUT, RT ENG POWER ROLLED BACK TWICE. 1ST OCCURENCE DURING CLIMB 3000 TO 5000 WITH POWER SET FOR A SHORT DURATION CLIMB (APRROX 90 PERCNET N1). RT ENG RO - [SDR DXTA2009120103874](https://openairdocs.org/sdr/DXTA2009120103874), Nov 30, 2009: WIRE. LOOSE. AFTER ROTATION, PASSING 300' AGL, NR 1 ITT INDICATOR WENT INTO RED, SHOWED APPROX 1100 DEG C. REDUCED PWR BELOW 74 PERCENT N1. ITT CAME OUT OF RED BUT THEN INCR - [SDR DXTA2009062203696](https://openairdocs.org/sdr/DXTA2009062203696), Jun 19, 2009: DISPLAY. FAILED. SMOKE FROM BELOW GLARE SHIELD STARTED AT 5,000' ON ARRIVAL. SMOKE LASTED ABOUT 30 SEC TOTAL. HEAVY, THEN DISCIPATING. "ALL" AVIONICS STARTED TO FLICKER PRIOR TO - [SDR DXTA2009030903539](https://openairdocs.org/sdr/DXTA2009030903539), Mar 5, 2009: MIXING VALVE. FAILED. DURING CLIMBOUT AT 280KTS/2000FPM AND 23,000FT CABIN STARTED CLIMBING AT 1,000 FPM. TURNED RATE CONTROLLER TO ZERO WITH NO EFFECT. CABIN HORN FOLLOWED, INITIATE - [SDR DXTA200702285](https://openairdocs.org/sdr/DXTA200702285), Jun 21, 2007: ENGINE. FAILED. NR 2 ENGINE SHUDDERED FAIRLY VIOLENTLY FOLLOWED BY FAILURE INDICATIONS, ITT ROSE TO 1066. ENGINE SHUTDOWN ACCOMPLISHED. FL260 APPROX ISA + 20. [07-12-07] REMOVE - [SDR DXTA200500840](https://openairdocs.org/sdr/DXTA200500840), Jul 14, 2005: BRAKE. WEAK. BRAKES SEEM MUSHY, PERFORMED TAXI ON ACFT FOR BRAKE SYSTEM TROUBLESHOOTING. BRAKING PERFORMANCE NORMAL. COULD NOT DUPLICATE. RESEARCHED FOR RECENT HISTORY RELAT ## 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.