# N802QS: 2020 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: 700-0025 - Year built: 2020 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: February 28, 2020 - Certificate issued: July 18, 2025 - Expires: July 31, 2032 - Mode S code: AAEABA - Owner type: Co-owned, fractional ownership - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=802QS - Page: https://openairdocs.org/aircraft/N802QS 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 N802QS. ## NTSB investigations on N802QS not matched to an aircraft (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB CEN09LA541](https://openairdocs.org/ntsb/CEN09LA541), Aug 23, 2009: Cessna CE-560 (N802QS), Kremmling, CO, no damage. Probable cause: The lineman’s inadvertent encounter with jet blast. ## FAA accident and incident reports None matched to N802QS. ## Reports on N802QS not matched to an aircraft (1) They name N802QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [Accident 20090823014709A](https://openairdocs.org/incident/20090823014709A), Aug 23, 2009: Cessna 560 (N802QS), Kremmling, CO, No damage. (-23) On August 23, 2009, at 0906 MST, a Cessna CE-560, N802QS,registered to netjets sales, inc. was moving off the refueling point at mcelroy airfield (K20V)… ## Service difficulty reports (16) 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 DXTA2026032307336](https://openairdocs.org/sdr/DXTA2026032307336), Mar 19, 2026: ELEC CONNECTOR. DAMAGED. EVACUATION PATH LIGHT UNDER SEAT NR 4 IS NOT ILLUMINATING. REPAIRED POWER WIRE CONNECTOR. OPS CHECK GOOD. IAW SPM 20-30-20 - [SDR DXTA2025102005342](https://openairdocs.org/sdr/DXTA2025102005342), Oct 16, 2025: LIGHT. MALFUNCTIONED. WHEN EMER LTS ARE IN ARM AND PAX SAFETY SWITCH IS IN ON POSITION, THE WHITE EXIT LIGHT ABOVE THE FORWARD AIRSHOW SCREEN ON THE CABIN DIVIDER IS NOT ILLUMINATED. - [SDR DXTA2025082904757](https://openairdocs.org/sdr/DXTA2025082904757), Aug 28, 2025: ELEC CONNECTOR. DISCONNECTED. EMERGENCY EXIT LIGHT ON RIGHT SIDE OF AIRSTAIRS NOT ILLUMINATING. FOUND LIGHT DISCONNECTED FROM CONNECTOR, CHECK WIRES FOR DAMAGAE, RECONNECTED EMERGENCY LIGHT - [SDR DXTA2025062303989](https://openairdocs.org/sdr/DXTA2025062303989), Jun 21, 2025: STEERING UNIT. DEFECTIVE. AFTER TAKEOFF AND DURING GEAR RETRACTION WE RECIEVED THE FOLLOWING AMBER INDICATIONS: GEAR CONTROL FAULT, GEAR DOOR OPEN, ADC SSEC MISCOMPARE, AND GEAR DISAGREE - [SDR 2025FA0000404](https://openairdocs.org/sdr/2025FA0000404), Jun 17, 2025: SKIN. DENTED. ACCOMPLISHED FR-700-0025-15113 - REV- DATED: 20MAY2025: FIELD REPAIR - DENT AND GOUGE, RH WING, LOWER SKIN, INBOARD OF RIB 2 AT STRINGER 03WL. PERFORM THE FOLLO - [SDR DXTA2025030702587](https://openairdocs.org/sdr/DXTA2025030702587), Mar 5, 2025: SQUAT SWITCH. DEFECTIVE. NLG: NOSE GEAR WOULD NOT RETRACT. GEAR DISAGREE N AMBER CAS MESSAGE DISPLAYED. CORRECTIVE ACTION: REPLACED SQUAT SWITCH. OPS CHECK GOOD. IAW CE-700 AMM 32-60-10 - [SDR DXTR202240912101](https://openairdocs.org/sdr/DXTR202240912101), Sep 11, 2024: THRUST REVERSER. CORRODED. LH & RH UPPER AND LOWER TR BUCKETS HAVE EXCESSIVE CORROSION REMOVED AND REPLACED LEFT & RH HAND THRUST REVERSER REF. CE700 MM 78-30-00 THRU STEP 5.(7)(A). STEP - [SDR DXTA2022121676260](https://openairdocs.org/sdr/DXTA2022121676260), Dec 15, 2022: CIRCUIT BOARD. MALFUNCTIONED. APPROX 3 SECONDS AFTER DOOR IS RAISED FROM INSIDE, DOOR OPENS. DOOR RAISE BUTTON IS THEN UNRESPONSIVE UNTIL CANCEL BUTTON IS PUSHED. WHEN HANDLE IS ATTEMPTED TO - [SDR DXTA2022110773360](https://openairdocs.org/sdr/DXTA2022110773360), Nov 5, 2022: LIGHT. SHORTED. THE INTERIOR AND EXTERIOR EMERGENCY LIGHT SYSTEM IS NOT OPERSTING PROPERLY. DIFFERENT LIGHTS ARE COMING OFF/ON AT TIMES. CONFIRMED BOTH FUSES FOR SEAT 5 EMERGEN - [SDR DXTA2022102472660](https://openairdocs.org/sdr/DXTA2022102472660), Oct 23, 2022: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS BATTERY: EMERGENCY LIGHTS DO NOT ILLUMINATE WHEN SELECTED TO ON. ACCOMPLISHED A POWER CYCLE TO INCLUDE DISCONNETING THE MAIN BATTERIES, WHICH H - [SDR DXTA2022101372030](https://openairdocs.org/sdr/DXTA2022101372030), Oct 12, 2022: BATTERY PACK. DISCHARGED. EMERGENCY LIGHTING SYSTEM BATTERIES COMPLETELY DISCHARGE OVERNIGHT. THE SYSTEM WORKS FINE AFTER A FIVE MINUTE OF CHARGING ON APU POWER. CHARGED EMERGENCY BATTER - [SDR DXTA2022041860470](https://openairdocs.org/sdr/DXTA2022041860470), Apr 16, 2022: MONITOR. DEFECTIVE. MAIN DOOR LOCK: CABIN DOOR OPEN CAS MESSAGE REMAINS ON AFTER DOOR IS CLOSED AND LATCHED. THERE IS NO SOUND OF THE DOOR LOCK SOLENOID CLOSING. TRIED THE DOOR RES - [SDR DXTA2021110851560](https://openairdocs.org/sdr/DXTA2021110851560), Nov 8, 2021: NONE. NONE. MAIN DOOR MOTOR SWITCH: MAIN CABIN WILL NOT CLOSE. DOOR GOES UP 1/4 OF THE WAY BEFORE STOPPING AND THE "CHECK DOOR HANDLE" LIGHT COMES ON. DOOR HANDLE SWITCHES - [SDR DXTA2021073046030](https://openairdocs.org/sdr/DXTA2021073046030), Jul 29, 2021: WIRE. BROKEN. MAIN DOOR: MAIN CABIN DOOR WILL NOT OPEN FROM THE INSIDE. RED BUTTON HAS NO EFFECT. TROUBLESHOT RED PUSHBUTTON RELEASE AND FOUND THAT THE PUSHBUTTON SWITCH WAS - [SDR 2021F00071](https://openairdocs.org/sdr/2021F00071), Apr 14, 2021: SKIN. PUNCTURED. RRL LH IN-BOARD FLAP DAMAGE REF ENGINEERING MEMO DQ29618M1 RRL - [SDR DXTA2020090854054](https://openairdocs.org/sdr/DXTA2020090854054), Sep 5, 2020: DOOR. UNKNOWN. MAIN CABIN DOOR EXTREMELY HARD TO OPEN AFTER FLIGHT. INSPECTED AND OPS CHECKED MAIN CABIN DOOR, IAW AMM 52-10-00-10. OPS CHECK GOOD AND NO DEFECTS NOTED, A/C OK ## Service difficulty reports on N802QS not matched to an aircraft (14) They name N802QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DXTR20170721](https://openairdocs.org/sdr/DXTR20170721), Jul 21, 2017: STRUCTURE. BENT. SHEETMETAL DAMAGE ON MAIN CABIN DOOR LOWER FOWARD CORNER ON EXTERIOR EDGE. ACCOMPLISHED REPAIR BY AQRD ENGINEERING ERO-900686 INSTRUCTIONS - [SDR DXTA2014112605937](https://openairdocs.org/sdr/DXTA2014112605937), Nov 25, 2014: FUEL CONTROL. MALFUNCTIONED. DESCENDING OUT OF CRUISE ALTITUDE, RT THROTTLE LEVER HAD NO EFFECT ON ENGINE POWER SETTING. RT ENGINE MAINTAINED CRUISE POWER, EVEN WHEN RT THROTTLE WAS BROUGHT - [SDR DXTA2014082805869](https://openairdocs.org/sdr/DXTA2014082805869), Aug 27, 2014: MOTOR. UNSERVICEABLE. AFTER LANDING THE LOW RAKE PRESS & ANTI-SKID INOPERATIVE, ANNUNCIATOR ILLUMINATED. NORMAL BRAKES NOT AVAILABLE, USED EMER BRAKES TO STOP THE ACFT. THE POWER BRA - [SDR DXTA2014082105861](https://openairdocs.org/sdr/DXTA2014082105861), Aug 20, 2014: RELAY. UNSERVICEABLE. AFTER TOUCHDOWN DURING ROLL OUT THE LOW BRAKE PRESS ANNUNCIATOR ILLUMINATED. THE FIRST OFFICER THEN SAID HE HAD LOST BRAKES. USED EMER BRAKES TO STOP ACFT. POWE - [SDR DXTA2014081505856](https://openairdocs.org/sdr/DXTA2014081505856), Aug 14, 2014: MOTOR. UNSERVICEABLE. AFTER NORMAL LANDING THE LOW BRAKE PRESS ANTI-SKID INOPERATIVE ANNUNCIATOR ILLUMINATED. NORMAL BRAKES NOT AVAILABLE DURING TAXI, HAD TO USE EMER BRAKES TO STOP - [SDR DXTA2014080605842](https://openairdocs.org/sdr/DXTA2014080605842), Aug 5, 2014: DISPLAY. MALFUNCTIONED. DURING CRUISE FLIGHT AT FL410, MFD BLANKED OUT. ONE MINUTE LATER LARGE RED X APPEARED ON THE SCREEN COUPLED WITH AN ELEC BURNING SMELL. THE MFD CAME BACK ON & E - [SDR DXTA2014052805787](https://openairdocs.org/sdr/DXTA2014052805787), May 29, 2014: UNKNOWN. ODOR. AFTER PLYING TAKEOFF POWER A FAINT ODOR BEGAN COMING INTO THE CABIN. AROUND 2000' AGL BURNING SMELL BECAME VERY STRONG. RETURNED TO APA FOR LANDING. FREON AIR W - [SDR DXTA2010081304189](https://openairdocs.org/sdr/DXTA2010081304189), Aug 12, 2010: MOTOR. BURNED. ACFT CAUGHT FIRE. SPRAYED WITH FIRE EXTINGUISHER. MOTOR BURNED. DESERVICED SYS & REMOVED A/C PALLET ASSY IAW MM, CH 21-52-00 8/13/10. INSTALLED NEW MOTOR, PULLE - [SDR CWQR200908](https://openairdocs.org/sdr/CWQR200908), Nov 16, 2009: FLEX DUCT. CHAFED. DURING PHASE 1-5 INSPECTION, FOUND FLEX DUCT HAD CHAFED THROUGH THE INSULATION ON SEVERAL WIRE AND MAKE CONTACT WITH THE BARE WIRE SPINE OF THE FLEX DUCT. INDIC - [SDR DXTA2009102001](https://openairdocs.org/sdr/DXTA2009102001), Oct 2, 2009: TRANSCEIVER. MALFUNCTIONED. IN FLIGHT, THE RADAR WHILE IN STBY WOULD FLASH "WAIT" ON THE MFD LOWER LEFT. IN WX MODE ON THE CONTROL HEAD AND SUBPANEL IT WOULD CYCLE BETWEEN A YELLOW "WX" AN - [SDR 2009FA0000693](https://openairdocs.org/sdr/2009FA0000693), Aug 13, 2009: INVERTER. FAILED. INVERTER NR 1 FAILED IN FLIGHT. - [SDR DXTA2008111703359](https://openairdocs.org/sdr/DXTA2008111703359), Nov 16, 2008: LANDING GEAR. VIBRATION. EXPERIENCED VIOLENT NOSE WHEEL SHIMMY DURING TAKEOFF ROLL. ABORTED TAKEOFF. - [SDR DXTA200803049](https://openairdocs.org/sdr/DXTA200803049), May 8, 2008: COMPUTER. INOPERATIVE. AUTOPILOT DISENGAGED TWICE ON CLIMB-OUT ON PFD1. REMOVED AND REPLACED 1IC-615 AND C/W SYS. OPS CHECK IAW MM 34-23-10 - [SDR DXTA200702381](https://openairdocs.org/sdr/DXTA200702381), Aug 5, 2007: UNKNOWN. SMOKE. SMOKE DISCOVERED IN CABIN AFTER TAKEOFF. REMOVED AND INSTALLED ACM IAW R70.3G CMM CHAPTER 21-50-03. OPERATIONAL AND LEAK CHECK NORMAL. ## 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.