# N816QS: 2021 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: 700-0051 - Year built: 2021 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 24, 2021 - Certificate issued: July 23, 2026 - Expires: July 31, 2033 - Mode S code: AB2115 - Owner type: Co-owned - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=816QS - Page: https://openairdocs.org/aircraft/N816QS 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 N816QS. ## FAA accident and incident reports None matched to N816QS. ## Service difficulty reports (10) 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 DXTA2026072708983](https://openairdocs.org/sdr/DXTA2026072708983), Jul 24, 2026: AIR FILTER. DIRTY. NOTICED A FOUL CHEMICAL LIKE SMELL DURING PRE FLIGHT. THE SMELL SEEMED TO BE COMING FROM WEMACS AND GET WORSE THE LONGER THE APU WAS RUNNING. AFTER POWERING DOW - [SDR 2026FA0000030](https://openairdocs.org/sdr/2026FA0000030), Jan 17, 2026: FAIRING. DAMAGED. RH INBOARD FLAP FAIRING IMPACT DAMAGE - [SDR 2026FA0000029](https://openairdocs.org/sdr/2026FA0000029), Jan 17, 2026: MESH. DETERIORATED. LEFT ENGINE INLET MESH DETERIORATION - [SDR 2026FA0000028](https://openairdocs.org/sdr/2026FA0000028), Jan 17, 2026: MESH. DETERIORATED. RIGHT ENGINE INLET MESH DETERIORATION - [SDR 2026FA0000027](https://openairdocs.org/sdr/2026FA0000027), Jan 17, 2026: MESH. DETERIORATED. RIGHT ENGINE INLET MESH DETERIORATION. - [SDR DXTA2024050611685](https://openairdocs.org/sdr/DXTA2024050611685), May 4, 2024: BATTERY. NO TEST. EMERGENCY LIGHTS BATTERY: COMPLETED EMERGENCY/ABNORMAL CHECKLIST 25X TO CHARGE EMERGENCY LIGHTS BATTERY PACK. PROCEDURE FAILED. REMOVED AND REPLACED FWD RH EMER - [SDR DXTA2023092696160](https://openairdocs.org/sdr/DXTA2023092696160), Sep 22, 2023: BLOCK. DEFECTIVE. MAIN DOOR UNABLE TO OPEN FROM OUTSIDE. HANDLE IS STUCK IN OPEN POSITION AND JAMMED. WAS ABLE TO OPEN MAIN ENTRY CABIN DOOR. APPLIED POWER AND CYCLED DOOR, NOTIC - [SDR DXTA2023062289200](https://openairdocs.org/sdr/DXTA2023062289200), Jun 27, 2023: UNKNOWN. UNKNOWN. NORMAL LANDING - NO CAS MESSAGES PULLING INTO CHOCKS. NOTICED THE PLANE ROLLED A COUPLE OF INCHES AFTERPARKING BRAKE WAS SET AND BRAKES RELEASED. WHEN UNLOADING - [SDR 2022F00385](https://openairdocs.org/sdr/2022F00385), Oct 6, 2022: WINGLET. DAMAGED. LH WING TIP DAMAGED DURING TAXI OPERATIONS. - [SDR 2022F00131](https://openairdocs.org/sdr/2022F00131), Mar 13, 2022: CLOSET. CRACKED. THE CUSTOMER REPORTED THE STRIKER TO BE PULLED OUT FROM THE COMPOSITE. ACCOMPLISHED NJA RFTS-105361 REV 3 DATE: 29JAN22, N816QS (0051) FORWARD LEFT CLOSET DOOR ## Service difficulty reports on N816QS not matched to an aircraft (9) They name N816QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DXTA2011042604564](https://openairdocs.org/sdr/DXTA2011042604564), Apr 25, 2011: CONNECTOR. LOOSE. AT LEVEL FLIGHT AT 16,000 FT, THE BAG FIRE ANNUNCIATOR ILLUMINATED. IT FLICKERED INTERMITTENLY THEN FLASHED PERMANENTLY FOR ABOUT 5 SECONDS. MORE FLICKERING THE - [SDR DXTA2010102804280](https://openairdocs.org/sdr/DXTA2010102804280), Oct 27, 2010: FLT CONTROLS. MALFUNCTIONED. F/O REPORTED ACFT REQUIRED "EXCESSIVE" ELEVATOR PRESSURE TO ROTATE ON T/O, WITH TRIM SET AT CALCULATED T/O POSITION. NOTED IN CRUISE, F/O'S YOKE CANTED 10-15 DE - [SDR DXTA2009062203695](https://openairdocs.org/sdr/DXTA2009062203695), Jun 20, 2009: DOOR. CORRODED. WHILE PERFORMING ENGINE REMOVAL FOR MX, CORROSION WAS FOUND ON THE RT UPPER AND LOWER THRUST REVERSER BUCKETS AT THE REAR INSIDE SKIN RIVETS. THIS SEEMS TO BE A - [SDR DXTA200702344](https://openairdocs.org/sdr/DXTA200702344), Jul 18, 2007: SEAL. LEAKING. DURING CLIMB THROUGH 9000 FT REAR BAY OVERHEAT ANNUNCIATOR CAME ON INTERMITTENTLY 3 TIMES. THEN STEADY FOR 5 SECONDS THEN OUT. LIGHT STAYED OUT UNTIL SHUTDOWN. - [SDR DXTA200702011](https://openairdocs.org/sdr/DXTA200702011), Mar 10, 2007: UNKNOWN. UNKNOWN. AIRCRAFT ROLLS TO THE RT 2 DEG PER SEC WHEN AIRBRAKES DEPLOYED. DECREASED LT UPPER AIRBRAKE PANEL ANGLE DEFLECTION AND INCREASED RT UPPER AIRBRAKE PANEL ANGLE D - [SDR DXTA200701951](https://openairdocs.org/sdr/DXTA200701951), Feb 16, 2007: SWITCH. INOPERATIVE. WHEN GEAR WAS RETRACTED AFTER TAKEOFF, THE LT MAIN INDICATED BOTH RED AND GREEN LIGHTS AND THE NOSE AND RT MAIN INDICATED RED LIGHTS. UPON PLACING THE LEVER IN - [SDR DXTA200501051](https://openairdocs.org/sdr/DXTA200501051), Oct 13, 2005: DUCT. BLEW OUT. WHILE CRUISING AT FL360, HEARD A LOUD POP FROM REAR OF AIRCRAFT. CABIN CLIMB INDICATOR WAS PEGGED AT MAXIMUM READING. PRESSURIZATION WAS LOST. INSPECTED J-DUCT - [SDR DXTA200500703](https://openairdocs.org/sdr/DXTA200500703), Apr 29, 2005: BATTERY PACK. WEAK. CABIN EMERGENCY LIGHTING SYSTEM INOP. SYSTEM DOES NOT OPERATE WHEN S/W MOVED FROM 'ARM' TO 'MANUAL' AND ONLY OPERATES FOR 3 SEC WHEN S/W IS MOVED TO 'MANUAL' FR - [SDR DXTA200500693](https://openairdocs.org/sdr/DXTA200500693), Apr 22, 2005: CONNECTOR. DIRTY. WHEN THE APR SYSTEM IS ARMED THE APR GREEN LIGHT COMES ON AND WILL NOT CANCEL. INTEGRATED NR 1 & NR 2 DEEC'S FOR STORED CODES AND NO CODES WERE FOUND. REMOVED C ## 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.