# N876QS: 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: 700-0133 - Year built: 2024 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 14, 2024 - Certificate issued: January 22, 2026 - Expires: January 31, 2033 - Mode S code: AC0E0F - Owner type: Co-owned, fractional ownership - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=876QS - Page: https://openairdocs.org/aircraft/N876QS 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 N876QS. ## FAA accident and incident reports None matched to N876QS. ## 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 DXTA2025120505941](https://openairdocs.org/sdr/DXTA2025120505941), Dec 2, 2025: TEST SWITCH. FAULTED. L ENG FIRE LIGHT. A SMALL LIGHT IN THE LOWER LEFT CORNER OF THE L ENG FIRE LIGHT APPEARED IN CRUISE FLIGHT. IT STAYED ILLUMINATED FOR ABOUT 1/2 HOUR BEFORE FADI - [SDR DXTA2025091504915](https://openairdocs.org/sdr/DXTA2025091504915), Sep 10, 2025: SWITCH. FAULTED. ON DECENT INTO VANCOUVER, PRESSED THE PAX SAFETY LIGHT SWITCH. BUTTON SAYS ON, BUT THE ONLY LIGHTS THAT COME ON ARE THE NO SMOKING LIGHTS. CHECKED THE EMERGENCY - [SDR DXTA2025042403191](https://openairdocs.org/sdr/DXTA2025042403191), Apr 23, 2025: HANDLE. BINDING. MAIN CABIN DOOR HANDLE IS BINDING. TAKES ABOUT 30-40 LBS OF EFFORT TO PULL THE OUTSIDE HANDLE DOWN TO OPEN THE DOOR AND WHEN WE TRIED TO OPEN IT FROM INSIDE IT ## Service difficulty reports on N876QS not matched to an aircraft (12) They name N876QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DXTA2013021405283](https://openairdocs.org/sdr/DXTA2013021405283), Feb 13, 2013: BULB. INOPERATIVE. UPON SELECTING GEAR DOWN, THE RT MLG PRIMARY INDICATOR DID NOT INDICATE DOWN AND LOCKED. THE RED AND GREEN RT GEAR LIGHTS DID NOT ILLUMINATE ON GROUND. REPLACED - [SDR DXTA2012072605058](https://openairdocs.org/sdr/DXTA2012072605058), Jul 25, 2012: DOWNLOCK SWITCH. OUT OF ADJUST. DURING TAXI OUT, GEAR WARNING SOUNDED. DURING RIGHT TURN, RED UNSAFE LIGHT CAME ON. ADJUSTED RT MLG NORMAL AND STANDBY DOWNLOCK SWITCHES LAW AMM 32-60-00. SYSTE - [SDR 2012FA0000093](https://openairdocs.org/sdr/2012FA0000093), Jan 24, 2012: SEAT. UNLOCKED. FOUND NR 1 AND NR 2 LT SEAT DID NOT HAVE "SPRING-LOADED TRACK FITTING" PROPERLY ENGAGED INTO THE SEAT TRACK. THIS IS THE 2ND ACFT FOUND TO HAVE THIS CONDITION. - [SDR DXTA2011030904500](https://openairdocs.org/sdr/DXTA2011030904500), Mar 8, 2011: TRIM SYSTEM. LACK OF LUBE. AT CRUISE ALTITUDE, AILERON TRIM COMPLETELY FROZEN/INOP. ON GROUND IN WARMER TEMPERATURE, AILERON TRIM WORKS NORMAL. VERIFIED STIFF OPERATION OF AILERON TRIM ON - [SDR DXTA2009121503897](https://openairdocs.org/sdr/DXTA2009121503897), Dec 14, 2009: MASTER CYLINDER. LEAKING. CAPTAIN'S LT BRAKE PEDAL GOES TO STOP WITH LITTLE OR NO PRESSURE. BRAKE PRESSURE GAUGE CONFIRMS NO PRESSURE. REMOVED LEAKING MASTER CYLINDER AND INSTALLED NEW M - [SDR DXTA2009111603863](https://openairdocs.org/sdr/DXTA2009111603863), Nov 13, 2009: BRAKE ASSY. WEAK. CAPTAIN'S SIDE, LT BRAKE GOES TO THE STOP WITH VERY LITTLE PRESSURE. SERVICED NR 1 BRAKE MASTER CYLINDER AND BLEED SYS. REF AMM 32-40-00. OPS CHECK GOOD. - [SDR DXTA2009030903536](https://openairdocs.org/sdr/DXTA2009030903536), Mar 7, 2009: TIRE. DEFLATED. LT MAIN TIRES ARE FLAT. RT MAIN TIRES ARE BOTH FLAT, SPOTTED. ACFT TOWED FROM RUNWAY. AXLE JACKED BOTH MAIN GEARS. REMOVED AND REPLACED MAIN WHEEL ASSEMBLIES. W - [SDR DXTA200701977](https://openairdocs.org/sdr/DXTA200701977), Feb 28, 2007: SWITCH. INOPERATIVE. WHEN RETRACTING LANDING GEAR AND AFTER GEAR RETRACTION CYCLE WAS COMPLETE, LT GEAR INDICATOR RED NOSE GEAR INDICATOR RED, RH GEAR INDICATOR GEAR GREEN AND RED. - [SDR DXTA200701965](https://openairdocs.org/sdr/DXTA200701965), Feb 25, 2007: SWITCH. DIRTY. RT MLG INDICATES GREEN AND RED UPON RETRACTION. GEAR SELECTED DOWN RT MLG INDICATES GREEN NOT RED. JACKED AIRCRAFT AND APPLIED HYDRAULIC POWER. CLEANED LT & RT - [SDR DXTA200601486](https://openairdocs.org/sdr/DXTA200601486), Jul 7, 2006: BRAKE. WORN. ACFT PULLS TO THE RIGHT ON TAXI AND SIGNIFICANT LEFT RUDDER NEEDED TO MAINTAIN RUNWAY CENTERLINE ON TAKEOFF. RIGHT BRAKE SIGNIFICANTLY HOTTER THAN LEFT BRAKE AF - [SDR DXTA200601214](https://openairdocs.org/sdr/DXTA200601214), Jan 25, 2006: RUDDER PEDAL. STIFF. DURING TAKEOFF ROLL RUDDER BECAME VERY STIFF AND HARD TO MOVE, AS IF YAW DAMPNER WAS ENGAGED. AT LOW POWER SETTINGS RUDDER IS FREE AND EASY TO MOVE. DID A STATI - [SDR DXTA200601196](https://openairdocs.org/sdr/DXTA200601196), Jan 13, 2006: FILTER. UNKNOWN. ENG 2 FUEL ANNUNCIATOR ILLUMINATES AT TAKEOFF THRUST, ABORTED TAKEOFF. REMOVED THE NR 2 ENGINE FUEL FILTER ELEMENT AND REPLACED WITH A NEW FILTER ELEMENT. PERFO ## 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.