# N880QS: 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: 700-0139 - Year built: 2025 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: April 10, 2025 - Certificate issued: May 12, 2025 - Expires: May 31, 2032 - Mode S code: AC1F44 - Owner type: Co-owned, fractional ownership - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=880QS - Page: https://openairdocs.org/aircraft/N880QS 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 N880QS. ## FAA accident and incident reports None matched to N880QS. ## Service difficulty reports (1) 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 DXTA2026013006682](https://openairdocs.org/sdr/DXTA2026013006682), Jan 26, 2026: FLAP SYSTEM. FAULTED. AFTER DEPARTURE CLIMBING THROUGH 400' FLAPS REMAINED IN FLAPS 1 POSITION FOLLOWED BY FLAPS FAIL CAS MESSAGE RAN THE QRH FOLLOWED BY THE QRC. COMPLIED WITH TASK ## Service difficulty reports on N880QS not matched to an aircraft (13) They name N880QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DXTA2014033005705](https://openairdocs.org/sdr/DXTA2014033005705), Mar 29, 2014: SWITCH. DIRTY. DURING GEAR EXTENSION RECEIVED THREE GREEN MAIN LIGHTS & ONE LT RED LIGHT. AFTER MISSED APPROACH IT BEGAN TO FLICKER, IT FLICKERED FOR THE WHOLE NEXT APPROACH W - [SDR DXTA2013080105463](https://openairdocs.org/sdr/DXTA2013080105463), Aug 1, 2013: ENGINE. OVERTEMP. AFTER ROTATION ON TAKEOFF, LEFT ENGINE ITT WAS NOTED TO BE RED. POWER WAS REDUCED AND TEMP WAS NOTED TO BE AT LEAST 979 FOR APPROX 7-10 SECONDS. PERFORMED 5 POI - [SDR DXTA2012110805177](https://openairdocs.org/sdr/DXTA2012110805177), Nov 7, 2012: MASTER CYLINDER. MALFUNCTIONED. CO PILOTS LT AND RT BRAKE PEDALS ALL THE WAY TO THE FLOOR ONLY GET A FEW HUNDRED LBS OF PSI SHOWING. CAPTAINS BRAKES ARE VERY TOUCHY. SERVICED THE CO-PILOTS BRA - [SDR DXTA2012090405112](https://openairdocs.org/sdr/DXTA2012090405112), Aug 31, 2012: SWITCH. OUT OF ADJUST. 3 GREEN AND 3 RED GEAR UNSAFE ANNOUNCIATOR STAY ILLUMINATED AFTER LANDING GEAR WAS EXTENDED DURING FLIGHT. FOUND SELECTOR LEVER SWITCH OUT OF ADJUSTMENT ADJUSTE - [SDR DXTA2011021504468](https://openairdocs.org/sdr/DXTA2011021504468), Feb 14, 2011: STRUT. DISCHARGED. DURING TAKEOFF GEAR DID NOT RETRACT NORMALLY. (RED/GREEN). LOWERED GEAR AND INDICATED 3 GREENS NORMALLY. BUT THE NOSE GEAR WAS CANTED 45 DEGREES TO RT. FOLLOWED - [SDR DXTA2010090904227](https://openairdocs.org/sdr/DXTA2010090904227), Sep 8, 2010: UNKNOWN. MULTIPLE IND. OST FMS 1, FMS 2, COMM 1, NAV 1, FLIGHT DIRECTOR, AUTO PILOT, GPWS, WX RADAR, RADAR ALTIMETER AND HAD A FLASHING AOA WHEN WE ENCOUNTERED MODERATE TURBULENCE AT - [SDR DXTA200807203194](https://openairdocs.org/sdr/DXTA200807203194), Jul 20, 2008: DISPLAY. SHORTED. NR 1 MFD WENT COMPLETELY BLANK IN FLIGHT, NOTICED A SLIGHT ODOR SO PULLED MFD BREAKER AS A PRECAUTION. REMOVED NR 1 MFD AND NOTICED SLIGHT ELECTRICAL ODOR COMIN - [SDR DXTA200803194](https://openairdocs.org/sdr/DXTA200803194), Jul 20, 2008: DISPLAY. FAILED. NR 1 MDF WENT COMPLETELY BLANK IN FLIGHT, NOTICED A SLIGHT ODOR SO PULLED MFD BREAKER AS A PRECAUTION. (A) - [SDR DXTA200803054](https://openairdocs.org/sdr/DXTA200803054), May 11, 2008: BULB. BURNED OUT. PRIMARY NOSE GEAR GREEN DOWN ANNUNCIATOR DID NOT ILLUMINATE PRIOR TO LANDING. REMOVED 2 EA UNSERVICEABLE LIGHT BULBS. INSTALLED 2 EA NEW LIGHT BULBS. OPERATIONA - [SDR DXTA200702210](https://openairdocs.org/sdr/DXTA200702210), May 22, 2007: BRAKE ASSY. WEAK. UPON LANDING, CREW STATED THAT (BRAKES FEEL SPONGY). ACCOMPLISHED BLEEDING OF MAIN BRAKE SYSTEM, EMERG BRAKE SYSTEM, AND MAXARETS, TAXI CHECKED AND BRAKES FOUND - [SDR DXTA200601378](https://openairdocs.org/sdr/DXTA200601378), May 3, 2006: POSITION SWITCH. OUT OF POSITION. ELEVATOR/AILERON TRIM LIGHT CAME ON DURING TAKEOFF. PERFORMED ELEVATOR TRIM CONTROL SYSTEM ADJUSTMENT TEST. ADJUSTED MICROSWITCH AND OPS CHECKED OK IAW HAWKER 8 - [SDR DXTA200601341](https://openairdocs.org/sdr/DXTA200601341), Apr 11, 2006: SWITCH. SHORTED. THE POWER CIRCUIT BREAKER IN THE LAV CIRCUIT BREAKER PANEL(GALLEY) POPS WHENEVER THE LIGHTS CIRCUIT BREAKER IN THAT PANEL IS PUSHED IN AND MASTER GALLEY POWER I - [SDR DXTA200500613](https://openairdocs.org/sdr/DXTA200500613), Mar 3, 2005: FUEL FILTER. CLOGGED. NR 1 ENG FUEL LIGHT ILLUMINATED AT 60 KTS ON TAKEOFF. REMOVED AND REPLACED NR 1 ENGINE FUEL FILTER IAW HONEYWELL 731 LIGHT MAINTENANCE MANUAL CHAPTER 73-00-00. ## 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.