# N801QS: 2019 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: 700-0023 - Year built: 2019 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 31, 2019 - Certificate issued: December 11, 2025 - Expires: December 31, 2032 - Mode S code: AAE703 - Owner type: Co-owned, fractional ownership - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=801QS - Page: https://openairdocs.org/aircraft/N801QS 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 N801QS. ## FAA accident and incident reports None matched to N801QS. ## Service difficulty reports (12) 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 DXTA2026102210291](https://openairdocs.org/sdr/DXTA2026102210291), Oct 20, 2026: FUSE. BLOWN. EVACUATION PATH LIGHTING UNDER SEAT FIVE, IS INOPERATIVE. THE "EMERGENCY LIGHT FAIL PREFLIGHT TEST" ABNORMAL PROCEDURES CHECKLIST WAS COMPLIED WITH. NO CHANGE I - [SDR DXTA2026101310100](https://openairdocs.org/sdr/DXTA2026101310100), Oct 9, 2026: GSD. FAULTED. AT CRUISE, AMBER GEAR DISAGREE R DISPLAYED. TROUBLESHOOTED IN QRH AND LANDED AS SOON AS PRACTICAL. REMOVAL OF #3 GSD41 PN: 011-01457-02 SN: 2U4005148 PER TEAM 7 - [SDR DXTA2026050607925](https://openairdocs.org/sdr/DXTA2026050607925), May 3, 2026: BATTERY PACK. NO TEST. EMERGENCY LIGHTS REMAIN ON WHEN SWITCH IS IN OFF POSITION. 5G SWITCH MANUALLY RESET ON PILOT AND CO-PILOT SIDE BUT EMERGENCY LIGHTS REMAIN ON. CORRECTIVE ACTION - [SDR DXTA2025052703594](https://openairdocs.org/sdr/DXTA2025052703594), May 22, 2025: SQUAT SWITCH. MALFUNCTIONED. AFTER TAKEOFF NOSE GEAR L-R MISCOMPATE LOGHTS ILLUMINATED. GEAR UP INDICATION WAS NORMAL. RAN APPROPRAITE CHECKLIST EMERGENCY GEAR RELEASE HANDLE WAS PULLED PER - [SDR DXTA2023102398460](https://openairdocs.org/sdr/DXTA2023102398460), Oct 20, 2023: UNKNOWN. UNKNOWN. CABIN EMERG LIGHT: EMERGENCY EXIT LIGHT ABOVE SEAT 3 DOESN'T ILLUMINATE WITH THE SWITCH IN THE ARMED POSITION WITH THE OTHER EMERCENCY LIGHTS. ONLY ILLUMINATES - [SDR DXTA2022120775730](https://openairdocs.org/sdr/DXTA2022120775730), Dec 7, 2022: BATTERY PACK. FAILED. IN THE ON POSITION, THE EMERGENCY LIGHTS DO NOT COME ON. IN THE ARM POSITION THEY DIMLY FLICKER ON, THEN FADE TO OFF. REMOVED THE NR 1, 2, 3, & 4 EMERGENCY LIGH - [SDR 2022FA0000737](https://openairdocs.org/sdr/2022FA0000737), Dec 4, 2022: CASE. CRACKED. MX HAS REPORTED A CRACK ON THE ELT CASE. ACCOMPLISHED NJA RFTS-107347 REV. O. N801QS (700-0023) ELT CASE CRACKED - TEMPORARY REPAIR. - [SDR 2022F00188](https://openairdocs.org/sdr/2022F00188), Apr 15, 2022: COWLING. MISSING. R/H UPPER COWLING AFT INBOARD LATCH PIN BROKEN. ACCOMPLISHED NJA RFTS-106244 REV. 0 DATE: 14APR2022; N801QS (700-0023) COWL LATCH PIN MISSING. PERMANENT REPAIR - [SDR 2022F00175](https://openairdocs.org/sdr/2022F00175), Apr 2, 2022: NONE. NONE. LH INBOARD ROLL SPOILER OB HINGE POINT FOUND CHAFFING AGAINST UPPER WING SKIN WHEN DEPLOYED. W.S. 213.32. ACCOMPLISHED TEXTRON AVIATION ENGINEERING MEMO DQ34255 - [SDR DXTA2022031858670](https://openairdocs.org/sdr/DXTA2022031858670), Mar 18, 2022: SWITCH. DEFECTIVE. EMERG LIGHT SWITCH: DURING CRUISE FLIGHT ALL EMERGENCY LIGHTS CAME ON. LIGHTS EVENTUALLY WENT OUT AND THEN CAME BACK ON UPON LANDING. UNABLE TO RESET ALL LIGHTS - [SDR DXTA2021071345220](https://openairdocs.org/sdr/DXTA2021071345220), Jul 13, 2021: BATTERY PACK. INOPERATIVE. INTERNAL AND EXTERNAL EMR LIGHTS WILL NOT ILUMINATE WITH THE SWITCH IN THE ARM POSITION AND BATTERIES OFF. OPS CHECK OF EMERGENCY LIGHTING ADJUSTMENT/TEST IS GO - [SDR DXTA2021070844890](https://openairdocs.org/sdr/DXTA2021070844890), Jul 7, 2021: RELAY. DEFECTIVE. EMERGENCY LIGHTS DID NOT PASS THE TEST DURING POWER ON CHECKLIST. IN THE ON POSITION ALL EMER LIGHTS ARE ON. IN THE ARM POSITION, ALL EMER LIGHTS ARE OFF WHEN T ## Service difficulty reports on N801QS not matched to an aircraft (13) They name N801QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DXTA2014092505894](https://openairdocs.org/sdr/DXTA2014092505894), Sep 24, 2014: A/C PACK. FAILED. STRONG ELECTRICAL ODOR WAS NOTED. DENSE SMOKE CAME OUT COMBINED WITH STRONG ELECTRICAL ODOR WHEN CREW OPENED ELECTRICAL COMPARTMENT. REMOVED AND REPLACED FAILED - [SDR DXTA2013021205282](https://openairdocs.org/sdr/DXTA2013021205282), Feb 11, 2013: THRESHOLD. CRACKED. MAIN ENTRY DOOR THRESHOLD IS CRACKED. REPLACED CRACKED THRESHOLD WITH NEW INNER THREASHOLD. WORK ACCOMPLISHED PER SRM 51-30-03, 51-30-06, 51-40-09. - [SDR DXTA2012083005111](https://openairdocs.org/sdr/DXTA2012083005111), Aug 30, 2012: BUNGEE. FAILED. WHILE TAXIING FOR 1ST FLIGHT CREW COULD HEAR INTERMITTENT GROANING TYPE OF NOISE IN NOSE GEAR AREA WHILE MAKING LEFT, RIGHT TURNS AND HEADING STRAIGHT AHEAD. BR - [SDR DXTA2012081005085](https://openairdocs.org/sdr/DXTA2012081005085), Aug 9, 2012: UNKNOWN. ODOR. NOTICED A ELECTRICAL BURNING ODOR. NO SMOKE, NO TRIPPED CIRCUIT BREAKERS AND NO MALFUNCTIONS. ODOR DID DECREASE IN INTENSITY, BUT LINGERED FOR THE REST OF FLIGH - [SDR DXTA2012070505031](https://openairdocs.org/sdr/DXTA2012070505031), Jul 4, 2012: MOTOR. INOPERATIVE. "LO BRK PRESS" AND "ANTI SKID INOP" ANNUCIATORS ILLUMINATED AFTER LANDING AND BRAKES FAILED ON RUNWAY AT LOW SPEED. EMER BRAKE USED TO STOP ON RUNWAY AND ACFT T - [SDR 2010F00060](https://openairdocs.org/sdr/2010F00060), Mar 5, 2010: INDICATOR. MALFUNCTIONED. CLIMBING THROUGH FL340, 17 MINUTES INTO FLIGHT, AMBER HEADING MISCOMPARE ILLUMINATED RT SIDE WAS 7 DEGREES HIGHER THAN LT. CONTINUED CLIMB TO FL400 WHILE ACCOMP - [SDR 2010F00049](https://openairdocs.org/sdr/2010F00049), Feb 25, 2010: INDICATOR. MALFUNCTIONED. HDG MISCOMPARE LIGHT ILLUMINATED CLIMBING THROUGH FL370. DISAGREED BY 35-40 DEGREES. STARTED TO ALIGN IN A TURN, CONTINUED TO DIVERGE AFTER TURN BUT ONLY DISAGR - [SDR CWQR200706](https://openairdocs.org/sdr/CWQR200706), Jul 25, 2007: PLATE. RUSTED. DURING A PHASE 1-4 INSPECTION, NOTICED A RUST STAIN COMING FROM THE LOWER RUDDER BEARING PLATE ASSY (LOWEST HINGE POINT). UPON DISASSEMBLE, FOUND THE DRAIN HOLE - [SDR DXTA200702029](https://openairdocs.org/sdr/DXTA200702029), Mar 16, 2007: BRAKE. INOPERATIVE. LOST BRAKE PRESSURE DURING LANDING ROLL. CONFIRMED N2 PRESSURE AT BOTH PILOT STATIONS. USED EMER PRESS LEVER TO STOP. - [SDR DXTA200601591](https://openairdocs.org/sdr/DXTA200601591), Sep 4, 2006: B-NUT. LEAKING. BRAKE PEDALS WENT SOFT AND MUSHY ON CAPT AND CO-PILOTS SIDE ON LANDING. FOUND LEAKING B-NUT LEFT BRAKE. RE-TIGHTENED B-NUT AND BLED BRAKES BOTH SIDES IAW CE560 - [SDR DXTA200501120](https://openairdocs.org/sdr/DXTA200501120), Nov 28, 2005: WARNING LIGHT. ILLUMINATED. DURING TAKEOFF POWER UP, LT FUEL BOOST PUMP LIGHT ILLUMINATED. TAKEOFF ROLL WAS STARTED AND ABORTED. - [SDR DXTA200501039](https://openairdocs.org/sdr/DXTA200501039), Oct 26, 2005: LANDING GEAR. MALFUNCTIONED. WENT TO LOWER THE GEAR AND THE LEFT MAIN GREEN LIGHT NEVER ILLUMINATED. ALSO HAD A RED GEAR UNSAFE LIGHT, A WARNING HORN AND THE HYD PRESS ANNUNCIATOR STAYED IL - [SDR DXTA200300050](https://openairdocs.org/sdr/DXTA200300050), Jun 18, 2003: BLEED VALVE. CLOSED. DURING TAKEOFF ROLL, WINDSHIELD HEAT AND MASTER WARNING ANNUNCIATORS ILLUMINATED. VALVES WERE CLOSED AND SWITCHES WERE OFF. - RAN AIRCRAFT AND DUPLICATE SQUAWK. ## 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.