# N892QS: 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: 700-0156 - Year built: 2025 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 17, 2025 - Certificate issued: July 28, 2026 - Expires: July 31, 2033 - Mode S code: AC4E31 - Owner type: Co-owned - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=892QS - Page: https://openairdocs.org/aircraft/N892QS 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 N892QS. ## FAA accident and incident reports None matched to N892QS. ## Service difficulty reports (2) 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 DXTA2026101210093](https://openairdocs.org/sdr/DXTA2026101210093), Oct 8, 2026: WIRE HARNESS. DEFECTIVE. WHEN THE MAIN CABIN DOOR IS CLOSED FROM THE INSIDE, THE DOOR HANDLE LOCKING MECHANISM SOMETIMES ENGAGES EARLY, BUT MORE OFTEN, DOES NOT ENGAGE AT ALL, ALLOWING - [SDR DXTA2026100710060](https://openairdocs.org/sdr/DXTA2026100710060), Oct 5, 2026: PCB. FAULTED. CABIN DOOR WILL CLOSE AND HANDLE STOWS, HOWEVER, YELLOW LIGHT WILL NOT GO OUT AND CAS MESSAGE WILL NOT GO OUT. UPON RUNNING QRH PROCEDURE, WHEN PUSHING THE CANC ## Service difficulty reports on N892QS not matched to an aircraft (7) They name N892QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DXTA2013092505518](https://openairdocs.org/sdr/DXTA2013092505518), Sep 24, 2013: BRAKE. UNKNOWN. PILOTS SIDE LT BRAKES FEEL "SPONGY" HAVE TO BE PRESSED ALMOST TO THE FLOOR BEFORE ADEQUATE BRAKING IS ACHIEVED. OPERATED BRAKES SEVERAL TIMES AND TAXIED ACFT AR - [SDR DXTA2013060505410](https://openairdocs.org/sdr/DXTA2013060505410), Jun 4, 2013: BRAKE ASSY. WEAK. LEFT BRAKE PEDAL SPONGEY ON CAPTAIN AND F/O SIDE. PEDAL WILL TRAVEL SEVERAL INCHES BEFORE GRABBING. A FAINT SOUND CAN BE HEARD FROM CAPTAINS SIDE PEDAL AREA. RE - [SDR DXTA2012110505170](https://openairdocs.org/sdr/DXTA2012110505170), Nov 5, 2012: UNKNOWN. CORRODED. PERFORMED AN NDT INSPECTION AFTER CORROSION WAS REMOVED AROUND SOME SCREW HOLES. NDT WAS READING AN ANOMALY UNDER THE SURFACE ABOUT .020 DEEP. STARTED BLENDING - [SDR E81R_JW30216_1](https://openairdocs.org/sdr/E81R_JW30216_1), Dec 23, 2009: WIRE HARNESS. SHORTED. INVESTIGATED PATS STC INSTALLATION GTCP36-150W FAILING TO START. APU HANGS AT 60 PERCENT, WILL NOT ACCELERATE OR LOAD. FOUND INTERMITTENT OPEN CONNECTION IN WIR - [SDR DXTA200802973](https://openairdocs.org/sdr/DXTA200802973), Mar 30, 2008: BRAKE SYS. CONTAMINATED. BRAKES ARE VERY MUSHY AND GO TO THE FLOOR. INSPECTED SYS FOR LEAKS, NONE NOTED. PERFORMED OPS CHECK, ALL CHECK GOOD. BLED BRAKE SYS AND PERFORMED TAXI CHECK, AL - [SDR DXTA20082973](https://openairdocs.org/sdr/DXTA20082973), Mar 30, 2008: BRAKE ASSY. FAILED. BRAKES ARE VERY MUSHY AND GO TO THE FLOOR. INSPECTED SYSTEM FOR LEAKS NONE NOTED. PERFORMED OPS CHECK ALL CHECK GOOD BLEED BRAKE SYSTEM AND PERFORM TAXI CHECK A - [SDR DXTA200300132](https://openairdocs.org/sdr/DXTA200300132), Oct 2, 2003: COMPRESSOR. DAMAGED. AT FLIGHT LEVER 370, NR 1 ENGINED EXPERIENCE A LOUD BANG WITH ITT SPIKING AT 1016 DEGREES WITH AIRFRAME VIBRATION. N1 AND N2 ROSE, ITT THEN FELL TO 450 DEGREES ## 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.