# N879QS: 2025 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: 700-0136 - Year built: 2025 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: March 31, 2025 - Certificate issued: April 28, 2025 - Expires: April 30, 2032 - Mode S code: AC1934 - Owner type: Co-owned, fractional ownership - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=879QS - Page: https://openairdocs.org/aircraft/N879QS 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 N879QS. ## NTSB investigations on N879QS not matched to an aircraft (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB LAX06FA277](https://openairdocs.org/ntsb/LAX06FA277), Aug 28, 2006: Raytheon Hawker 800XP (N879QS), Smith, NV, substantial damage. Probable cause: The failure of the glider pilot to utilize his transponder and the high closure rate of the two aircraft, which limited each pilot's opportunity to see and avoid the other aircraft. ## FAA accident and incident reports None matched to N879QS. ## Reports on N879QS not matched to an aircraft (1) They name N879QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [Accident 20060828018491A](https://openairdocs.org/incident/20060828018491A), Aug 28, 2006: Raythn HAWKER800XP (N879QS), Smith, NV, Substantial damage. (-23) A Hawker 800-XP jet was on an IFR, FAR part 91K flight from kcrq (carlsbad, CA) to krno (reno, Nevada) at 16000 feet. The aircraft had just changed… ## Service difficulty reports (3) 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 DXTA2026010906467](https://openairdocs.org/sdr/DXTA2026010906467), Jan 6, 2026: UNKNOWN. SMOKE. AFTER APU START WE SMELLED OIL AND SAW SLIGHT SMOKE IN CABIN. AFTER MOTORING ENGINE BEFORE START, SMOKE REAPPEARED A LITTLE MORE DENSE WITH SMELL AGAIN. MCC ELE - [SDR DXTA2025072204296](https://openairdocs.org/sdr/DXTA2025072204296), Jul 18, 2025: PCB. FAULTED. ELEC EMER L CAS MESSAGE IN FLIGHT. CORRECTIVE ACTION: SWAPPED POSITIONS OF LH AND RH PCB. OPS CHECK GOOD. IAW AMM 24-60-11 - [SDR DXTA2025061603857](https://openairdocs.org/sdr/DXTA2025061603857), Jun 11, 2025: SQUAT SWITCH. DEFECTIVE. NLG LANDING GEAR RETRACTION: AFTER TAKEOFF DURING RETRACTION THE NOSE GEAR VIBRATED AND WE GOT THE FOLLOWING INDICATIONS GEAR CONTROL FAULT, GROUND DETECT FAULT ## Service difficulty reports on N879QS not matched to an aircraft (2) They name N879QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DXTA200601599](https://openairdocs.org/sdr/DXTA200601599), Aug 28, 2006: SEAT BELT. UNSECURE. DURING FLIGHT, A PASSENGER TIGHTENED HIS LAP BELT AND THE INBOARD ATTACHMENT END CAME OUT FROM BETWEEN THE SEAT CUSHIONS, JUMPED UP FROM SEAT NR 7 AND SAT IN SE - [SDR DXTA200601217](https://openairdocs.org/sdr/DXTA200601217), Jan 26, 2006: FIRE DETECTOR. MALFUNCTIONED. BAGGAGE FIRE LIGHT SPORATICLY BLINKING. NO SMOKE OR FIRE INDICATING. VISUALLY INSPECTED FORWARD BAGGAGE, AFT BAGGAGE AND LAV SMOKE DETECTORS, NO DEFECTS NOTED. ## 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.