# N872QS: 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: 700-0128 - Year built: 2024 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: October 1, 2024 - Certificate issued: July 2, 2026 - Expires: July 31, 2033 - Mode S code: ABFF33 - Owner type: Co-owned - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=872QS - Page: https://openairdocs.org/aircraft/N872QS From the FAA registry file of October 27, 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. ## NTSB investigations None matched to N872QS. ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20260705007049I](https://openairdocs.org/incident/20260705007049I), Jul 5, 2026: Textron Aviation Inc 700 (N872QS), Charleston, SC, Minor damage. On roll out the aircraft struck a deer on the runway causing minor damage to a flap fairing. ## 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. ## 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 DXTA2026072408941](https://openairdocs.org/sdr/DXTA2026072408941), Jul 22, 2026: G SWITCH. TRIPPED. EMERGENCY LIGHTS WILL NOT SHUTOFF. WE TRIED QRH BOTH RESET SWITCHES UNDER EACH SEAT. EMERGENCY LIGHTS STILL REMAIN ON. UPPON ARRIVING TO THE A/C NO LIGHTS WERE - [SDR DXTA2025071604255](https://openairdocs.org/sdr/DXTA2025071604255), Jul 14, 2025: G SWITCH. TRIPPED. EMERGENCY LIGHTS REMAIN ON AFTER SHUTDOWN. RESET 5G SWITCH PER ORH AND LIGHTS REMAIN ON GAINED ACCESS TO ALL 4 G-SWITCHES, RESET ALL, LIGHTS EXTINGUISH ALL WORK - [SDR DXTA2025061603876](https://openairdocs.org/sdr/DXTA2025061603876), Jun 12, 2025: BATTERY. DEFECTIVE. EMERGENCY LIGHTING: DURING POSTFLIGHT, NOTED ALL EMERGENCY LIGHTS WERE ON. SHUTDOWN AND ATTEMPTED TO RESET THE TWO COCKPIT G SWITCHES. ALL EMERGENCY LIGHTING RE ## Service difficulty reports on N872QS not matched to an aircraft (16) They name N872QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DXTA2011022804481](https://openairdocs.org/sdr/DXTA2011022804481), Feb 25, 2011: SWITCH. INOPERATIVE. AFTER TAKEOFF LANDING GEAR DID NOT RETRACT PROPERLY. INDICATIONS WERE 3 RED GEAR LIGHT ANNUNCIATORS OVER ONE GREEN NOSE GEAR ANNUNCIATOR LIGHT. COMPLETED CHECKL - [SDR DXTA2010080504186](https://openairdocs.org/sdr/DXTA2010080504186), Aug 3, 2010: RELAY. MALFUNCTIONED. ON INITIAL CLIMBOUT WHOLE RT SIDE AVIONICS WENT OUT (BOTH EFIS TUBES, NR 2 RADIO, NR 2 FMS). HEARD A POPPING SOUND NORMALY ASSOCIATED WITH WHEN IT TURNS ON AND - [SDR DXTA200810093299](https://openairdocs.org/sdr/DXTA200810093299), Oct 9, 2008: CONTROL VALVE. LEAKING. ON LT SIDE (CAPT'S SIDE) NOT BRAKE PRESSURE ON LT PEDAL. LT PEDAL GOES TO THE FLOOR. RT PEDAL WORKS NORMAL. RT SIDE (SIC SIDE) BOTH PEDALS WORK NORMAL. TROUBLES - [SDR DXTA200803299](https://openairdocs.org/sdr/DXTA200803299), Oct 9, 2008: BRAKE SYS. MALFUNCTIONED. ON LEFT SIDE (CAPT'S SIDE) NO BRAKE PRESSURE ON LEFT PEDAL. LEFT PEDAL GOES TO THE FLOOR. - [SDR DXTA200809303292](https://openairdocs.org/sdr/DXTA200809303292), Sep 30, 2008: MASTER CYLINDER. LEAKING. LT BRAKE ON PILOTS SIDE HAS NO BRAKE PRESSURE ( GOES TO FLOOR WITH NO BRAKING AUTHORITY) BRAKE PRESSURE GAUGE ON DASH SHOWS ZERO (0) PSI. REPEAT WRITE UP. CONFI - [SDR MAS2008F00102](https://openairdocs.org/sdr/MAS2008F00102), Sep 30, 2008: BRAKE ASSY. WEAK. LEFT BRAKE ON POLOTS SIDE HAS NO BRAKE PRESSURE. - [SDR DXTA200809223284](https://openairdocs.org/sdr/DXTA200809223284), Sep 22, 2008: BRAKE SYS. CONTAMINATED. LT BRAKE PEDAL ON PILOTS SIDE HAS NO PRESSURE GOES TO FLOOR WITH NO BRAKING AUTHORITY. CO-PILOTS SIDE BRAKES WORK NORMALLY WITH GOOD PRESSURE ON INDICATOR. BLEE - [SDR DXTA200803284](https://openairdocs.org/sdr/DXTA200803284), Sep 22, 2008: PEDAL. FAULTY. LT BRAKE PEDAL ON PILOTS SIDE HAS NO PRESSURE GOES TO FLOOR WITH NO BRAKING AUTHORITY. - [SDR DXTA200808223237](https://openairdocs.org/sdr/DXTA200808223237), Aug 22, 2008: BULB. BURNED OUT. RT MAIN GEAR PRIMARY INDICATOR LITE BULBS BURNED OUT. RELAMPED INDICATOR. OPS CHECK GOOD AT THIS TIME. WORK IAW MM 33-10-05 - [SDR DXTA200803083](https://openairdocs.org/sdr/DXTA200803083), May 28, 2008: LINE. LOOSE. LT FOOT BRAKE ON CAPTS SIDE INOP. TIGHTENED LINE ON PILOTS BRAKE MASTER CYLINDER AND SERVICED AND BLED PILOTS BRAKE MASTER CYLINDER. - [SDR DXTA200702027](https://openairdocs.org/sdr/DXTA200702027), Mar 16, 2007: SMOKE DETECTOR. CONTAMINATED. RED (BAGGAGE FIRE) ANNUNCIATOR ILLUMINATED MOMENTARILY (3) TIMES DURING DESCENT. NO SMOKE OR VISUAL INDICATION OF FIRE PRESENT. CLEANED SMOKE DETECTOR GRILLS AN - [SDR DXTA200400432](https://openairdocs.org/sdr/DXTA200400432), Oct 25, 2004: CONNECTOR. LOOSE. ENGINE NR 2 FUEL LIGHT CAME ON AT BEGINNING OF TAKEOFF ROLL, ABORTED TAKEOFF. REMOVED NR 2 ENG FUEL FILTER, INSTALLED NEW FUEL FILTER, SEATED FUEL FILTER CONNEC - [SDR DXTA200400367](https://openairdocs.org/sdr/DXTA200400367), Aug 22, 2004: SENSOR. INOPERATIVE. DURING TAKEOFF ROLL NR 1 ENG TOOK 4-6 SECS TO ACHIEVE T/O POWER (95.5) PRIOR TO 80KTS, NR 1 ENG ROLLED BACK TO APPROX 93 PERCENT THEN UP TO 94 THEN BACK TO 91-2 - [SDR DXTA200400255](https://openairdocs.org/sdr/DXTA200400255), Mar 4, 2004: ENGINE. FAILED. ON TAKEOFF, NR 1 ENGINE FAILED WITH A LOUD BANG JUST AFTER LIFTOFF, THE ENGINE SLOWED DOWN VERY QUICKLY AND SHOWED NO N1 ROTATION. ACCOMPLISHED AIR TURNBACK TO - [SDR DXTA200300073](https://openairdocs.org/sdr/DXTA200300073), Jul 21, 2003: FILTER. DAMAGED. NR 1 ENG FUEL LIGHT CAME ON DURING TAKE OFF ROLL (LIGHT CAME ON AT 50 KIAS), LIGHT EXTINGUISHED WHEN POWER REDUCED. - REMOVED NR 1 AND 2 ENG FUEL FILTERS PER HO - [SDR DXTA200300071](https://openairdocs.org/sdr/DXTA200300071), Jul 18, 2003: WARNING LIGHT. ILLUMINATED. NR 1 ENGINE FUEL LIGHT CAME ON WHEN TAKEOFF POWER APPLIED, LIGHT EXTINGUISHED WHEN POWER REDUCED AT APPROX. 20 KNOTS. ABORTED TAKEOFF. - INSPECTED LT ENGINE FUE ## 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.