# N827QS: 2022 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: 700-0067 - Year built: 2022 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: March 2, 2022 - Certificate issued: April 28, 2025 - Expires: April 30, 2032 - Mode S code: AB4C4B - Owner type: Co-owned - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=827QS - Page: https://openairdocs.org/aircraft/N827QS 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 N827QS. ## FAA accident and incident reports None matched to N827QS. ## Service difficulty reports (6) 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 DXTA2026102310285](https://openairdocs.org/sdr/DXTA2026102310285), Oct 20, 2026: DOOR. NO DISCREPANCY. MAIN CABIN DOOR WOULD NOT OPEN SO WE EXITED THROUGH THE EMERGENCY EXIT. PERFORMED MED OPS TEST AND NOTED WARNING/INDICATION WAS NOT WORKING CORRECTLY. DOOR OPEN - [SDR DXTA2025042303176](https://openairdocs.org/sdr/DXTA2025042303176), Apr 22, 2025: ACTUATOR. DEFECTIVE. RIGHT AILERON TRIM: DURING DESCENT THROUGH FL230 AILERON TRIM WAS APPLIED TO CORRECT A LEFT YOKE DISPLACEMENT AND FAILED TO RESPOND. AILERON TRIM WAS INOPERATIV - [SDR DXTA2025010301774](https://openairdocs.org/sdr/DXTA2025010301774), Dec 30, 2024: BATTERY. INOPERATIVE. EMERGENCY LIGHTING: STANDBYE EMERGENCY LIGHT BATTERIES DO NO HOLD A CHARGE. WHEN ACCEPTING THE AC AT THE BEGGINING OF THE DAY THE LIGHTS DONT WORK. AFTER THE AC - [SDR DXTA2024091100495](https://openairdocs.org/sdr/DXTA2024091100495), Sep 9, 2024: BATTERY PACK. INOPERATIVE. WITH THE AIRCRAFT POWERED UP AND THE EMERGENCY LIGHTS ARE IN THE ARM POSITION AND THE PAX SAFETY SWITCH IS TURNED ON, THE 3 EXIT LIGHTS DO NOT ILLUMINATE. WE RA - [SDR DXTA2023030281540](https://openairdocs.org/sdr/DXTA2023030281540), Mar 1, 2023: NONE. NONE. MAIN EXIT SIGN/LIGHT: ALL EMERGENCY LIGHTS FAIL TO COME ON ON PREFLIGHT CHECK WITH EMER LIGHT SWITCH IN ARM OR ON POSITION. *** CORRECTIVE ACTION *** UNABLE TO - [SDR DXTA2022122777080](https://openairdocs.org/sdr/DXTA2022122777080), Dec 25, 2022: G SWITCH. TRIPPED. AFTER POWERING DOWN AIRCRAFT, EMERGENCY LIGHTS REMAINED ILLUMINATED. RESET G-SWITCH ON AIRCRAFT IAW AMM 33-50-11 OPS CHECK GOOD ## Service difficulty reports on N827QS not matched to an aircraft (13) They name N827QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DXTA2017100500001](https://openairdocs.org/sdr/DXTA2017100500001), Oct 3, 2017: FAN. FAULTY. ON DESCENT INTO KAUS, WE SMELLED AN ELECTRICAL BURNING SMELL COMING FROM THE GLARESHIELD. WE TURNED OFF THE WINDSHIELD DEFOG FAN AND THE SMELL WENT AWAY. REMOVE - [SDR DXTA2016022906194](https://openairdocs.org/sdr/DXTA2016022906194), Mar 4, 2016: PRECOOLER. DEFECTIVE. RIGHT ENG, BLEED AIR OVERHEAT, LIGHT CAME ON AT 31,000 FEET. RAN CHECKLIST & LIGHT WENT OUT. DIVERTED AIRPLANE. ON TAKEOFF, THE RT ITT WENT TO 710 DEGREES C IN - [SDR DXTA2014060405788](https://openairdocs.org/sdr/DXTA2014060405788), Jun 3, 2014: VALVE. INOPERATIVE. WINDSHIELD ANTI-ICE WAS TURNED ON INFLIGHT & NO AIR WAS HEARD FOR 15 SECONDS, THEN AIR WAS HEARD ACCOMPANIED BY A RUBBER BURNING ODOR. ODOR WAS VERY STRONG & WE - [SDR DXTA2014060205785](https://openairdocs.org/sdr/DXTA2014060205785), May 31, 2014: CONTROLLER. FAILED. WINDSHIELD ANTI-ICE OVERHEATED IN FLIGHT AT -14 C RAT. BURNING ODOR IS ALSO ACCOMPANYING THE WINDSHIELD OVERHEAT LIGHT & MASTER CAUTION. DURING TESTING AND TROU - [SDR DXTA2014020705641](https://openairdocs.org/sdr/DXTA2014020705641), Feb 7, 2014: PRESSURE SWITCH. FAULTY. LOW BRAKE PRESS & ANTI-SKID INOPERATIVE LIGHTS ILLUMINATED ON TAXIWAY AFTER CLEARING THE RUNWAY. VERIFIED THAT THERE WAS NO BRAKE PRESS & STOPPED THE ACFT WITH - [SDR DXTA2014010705616](https://openairdocs.org/sdr/DXTA2014010705616), Jan 6, 2014: BRAKE SYS. FAILED. AFTER LANDING AND DURING TAXI, LOW BRAKE PRESSURE, ANTI-SKID INOPERATIVE & POWER BRAKES CIRCUIT BREAKER ANNUNCIATED & TRIPPED RESPECTIVELY, LOST ALL BRAKING. EM - [SDR CWQR2011110925](https://openairdocs.org/sdr/CWQR2011110925), Nov 9, 2011: TORQUE TUBE. CRACKED. DURING A SCHEDULED INSPECTION, FOUND THE NLG DOOR TORQUE TUBE CRACKED AT THE MOUNT BOLT PIVOT PLATE. . R & R TORQUE TUBE. - [SDR DXTA2011072204663](https://openairdocs.org/sdr/DXTA2011072204663), Jul 22, 2011: CIRCUIT BOARD. INOPERATIVE. FLAPS DID NOT EXTEND ON LANDING. R & R HYD PCB IAW WDM DWG PN 6509270. OPS CHECKED GOOD IAW MM 27-51-00. - [SDR DXTA2010110204286](https://openairdocs.org/sdr/DXTA2010110204286), Nov 1, 2010: COALESCER BAG. ODOR. IMMEDIATELY AFTER TAKEOFF THERE WAS A CHEMICAL OR ELECTRICAL BURNING ODOR THAT LASTED ENTIRE FLIGHT. INCREASING THE TEMP AND OVERHEAD/DEFOG FAN AIRFLOW INCREASE - [SDR DXTA2010082504206](https://openairdocs.org/sdr/DXTA2010082504206), Aug 24, 2010: CIRCUIT BOARD. INOPERATIVE. FLAPS INOPERATIVE. CLICKING SOUND HEARD ON TAKEOFF, COMING FROM LT SIDE OF COCKPIT. PLANNED A RETURN TO DEPARTURE; SELECTED FLAPS 15. FLAP HANDLE STOPPED AT THE - [SDR DXTA2010070204137](https://openairdocs.org/sdr/DXTA2010070204137), Jul 1, 2010: CLAMP. LOOSE. DURING CLIMB, CRUISE, & DESCENT. A VERY NOTICEABLE LOUD NOISE, LIKE BRAKE ACCUMULATOR PUMP CYCLING VERY FREQUENTLY. NO ANNUCIATOR NOTED. FOUND A CLAMP ON THE WI - [SDR DXTA2009103003835](https://openairdocs.org/sdr/DXTA2009103003835), Oct 29, 2009: SWITCH. OUT OF ADJUST. (REPEAT) ON FINAL, GEAR DID NOT COME DOWN ON OUR FIRST ATTEMPT. NO RED OR GREEN LIGHTS AND NO HYDRAULIC THUMP. WAITED 10 SEC THEN PUT GEAR HANDLE UP AND STILL N - [SDR DXTA2009100903810](https://openairdocs.org/sdr/DXTA2009100903810), Oct 8, 2009: LANDING GEAR. MALFUNCTIONED. PUT GEAR HANDLE DOWN ON FINAL. THERE WAS A FIVE TO 10 SECOND DELAY BEFORE GEAR EXTENDED. GEAR EXTENDED SLOWLY. GOT THREE GREEN. DID LANDING GEAR WILL NOT EXTEND ## 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.