# N875QS: 2024 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: 700-0132 - Year built: 2024 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 20, 2024 - Certificate issued: August 3, 2026 - Expires: August 31, 2033 - Mode S code: AC0A58 - Owner type: Co-owned, fractional ownership - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=875QS - Page: https://openairdocs.org/aircraft/N875QS From the FAA registry file of November 5, 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 N875QS. ## FAA accident and incident reports None matched to N875QS. ## 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 DXTA2026100209973](https://openairdocs.org/sdr/DXTA2026100209973), Sep 30, 2026: STRUT. DISCHARGED. AFTER GEAR RETRACTION, AROUND 1500' A LOUD AUDIBLE THUMP WAS FELT & HEARD FROM THE NOSE GEAR. NO OTHER INDICATIONS OBSERVED, ALL SYNOPTICS WERE NORMAL. GEAR CAM - [SDR DXTA2026100209974](https://openairdocs.org/sdr/DXTA2026100209974), Sep 30, 2026: PIN. FOD. MAIN CABIN DOOR HANDLE, BOTH INTERIOR AND EXTERIOR ARE EXTREMELY HARD TO LATCH, TAKES BOTH HANDS. GAINED ACCESS TO AIRCRAFT, CONFIRMED INTERIOR AND EXTERIOR MAI - [SDR DXTA2026052608227](https://openairdocs.org/sdr/DXTA2026052608227), May 25, 2026: DOOR. FAULTED. MAIN CABIN DOOR WILL NOT SECURE CLOSED FROM EITHER INSIDE CABIN OR OUTSIDE AIRCRAFT. DOOR LOCKING MECHANISM SEAMS OUT OF RIG. REMOVED MAIN CABIN DOOR SIDE PANEL ## Service difficulty reports on N875QS not matched to an aircraft (8) They name N875QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DXTA2012072705061](https://openairdocs.org/sdr/DXTA2012072705061), Jul 26, 2012: LANDING GEAR. MALFUNCTIONED. GEAR RETRACTION TAKES APPROXIMATELY 15 SECONDS. IMMEDIATELY AFTER SELECTING GEAR UP THERE IS A BINDING/GRINDING NOISE IN THE NOSE. NOSE GEAR LIGHT GOES OUT WHEN - [SDR DXTA20082909](https://openairdocs.org/sdr/DXTA20082909), Mar 2, 2008: B-NUT. LOOSE. AT THROTTLE ADVANCE FOR T/O, AT 75 PERCENT N1 HAD ABRUPT FULL RT RUDDER DEFLECTION. OPERATED BOTH ENGINES AND PERFORMED FUNCTIONAL TEST OF RUDDER BIAS SYSTEM, O - [SDR DXTA200701893](https://openairdocs.org/sdr/DXTA200701893), Jan 30, 2007: FIRE DETECTOR. MALFUNCTIONED. BAGGAGE FIRE LIGHT FLASHES INTERMITTENTLY UPON LANDING. TESTED MWS AND LIGHT WOULD NOT COME ON. COULD NOT DUPLICATE SMOKE DETECTOR FAILURE. CLEANED CONTACTOR EY - [SDR DXTA200701840](https://openairdocs.org/sdr/DXTA200701840), Jan 6, 2007: SMOKE DETECTOR. MALFUNCTIONED. RED FIRE ANNUNICATOR ILLUMINATES, FLASHES INTERMITTENTLY IN FLIGHT. VISUALLY INSPECTED ALL BAGGAGE COMPARTMENTS. CLEANED AND INSPECTED FORWARD, AFT AND LAV SMOK - [SDR 2006FA0000522](https://openairdocs.org/sdr/2006FA0000522), May 22, 2006: CURRENT LIMITER. MISDRILLED. MOUNTING HOLES IN CURRENT LIMITER DOES NOT MATCH LUGS IN ELECTRICAL PANEL. - [SDR DXTA200601379](https://openairdocs.org/sdr/DXTA200601379), May 3, 2006: APU. OVERSERVICED. WHEN STARTING THE APU AND OPENED THE BLEED VALVE THE COCKPIT FILLED WITH SMOKE (AND THE CABIN) IT DOSEN'T SMELL ELECTRICAL. VERIFIED CORRECT OIL SERVICE IN APU. - [SDR DXTA200400360](https://openairdocs.org/sdr/DXTA200400360), Aug 13, 2004: WARNING LIGHT. ILLUMINATED. AS THROTTLES WERE ADVANCED TO TAKEOFF POWER, THE FUEL LOOK UP ANNUNCIATOR LIGHT CAME ON, ACCOMPANIED BY THE ENGINE FUEL NR 1 ANNUNCIATOR. REMOVED AND REPLACED L - [SDR DXTA200400333](https://openairdocs.org/sdr/DXTA200400333), Jul 6, 2004: BRAKE. STICKING. DURING TAXIING, NOTICED BRAKES WERE STICKING AND FADING, ALSO FELT LIKE BRAKES WERE OUT OF SYNC. GAINED ACCESS TO THE BRAKE CONTROL VALVE, BLED ALL FOUR MASTER ## 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.