# N873QS: 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: 700-0130 - Year built: 2024 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: November 8, 2024 - Certificate issued: December 19, 2024 - Expires: December 31, 2031 - Mode S code: AC02EA - Owner type: Co-owned, fractional ownership - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=873QS - Page: https://openairdocs.org/aircraft/N873QS 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 N873QS. ## FAA accident and incident reports None matched to N873QS. ## 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 DXTA2026040107457](https://openairdocs.org/sdr/DXTA2026040107457), Mar 29, 2026: BATTERY PACK. DEFECTIVE. NONE OF THE EMERGENCY LIGHTS ILLUMINATE WHEN SWITCH IS ON WITH MAIN BATTERIES OFF. LIGHTS OPS NORMAL ALL OTHER CONDITIONS. REMOVED THE FAULTY NR 1 BATTERY & INS - [SDR DXTA2025020302154](https://openairdocs.org/sdr/DXTA2025020302154), Jan 29, 2025: RELAY. FAULTY. CARGO & ACCESSORY COMPARTMENTS: ON THE GROUND WITH APU RUNNING, NOTICED A STRONG ELECTRICAL BURNING ODOR WHEN ENTERING THE BAGGAGE COMPARTMENT. NO VISIBLE SMOKE - [SDR DXTA20240110394](https://openairdocs.org/sdr/DXTA20240110394), Dec 4, 2024: SENSOR. DEFECTIVE. A/I WING HOT L AMBER CAS: UPON ENTERING THE TERMINAL AREA AT PBI WITH THE ENGINE ANTI ICE OFF. WE FIRST RECIEVED THE AMBER A/I WING O/T LEFT. IMEDIATLEY FOLLOWE ## Service difficulty reports on N873QS not matched to an aircraft (34) They name N873QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DXTA2013040905351](https://openairdocs.org/sdr/DXTA2013040905351), Apr 6, 2013: WIRE. BROKEN. GEAR LIGHTS WOULD NOT ILLUMINATE WHEN GEAR WAS SELECTED DOWN FOR LANDING. LIGHTS WERE TESTED AND WORKED. GEAR WAS CYCLED AND CHECKLIST WAS RUN. BACKUP SYSTEMS S - [SDR DXTA2011101104750](https://openairdocs.org/sdr/DXTA2011101104750), Oct 10, 2011: MASTER CYLINDER. LEAKING. LEFT PILOT, RT BRAKE SOFT, WITH FULL APPLICATION RT BRAKE INDICATES 400 PSI. RT PILOT BRAKES ARE NORMAL. R & R PILOTS LT AND RT BRAKE MASTER CYLINDERS REF MM 27 - [SDR DXTA2010072104168](https://openairdocs.org/sdr/DXTA2010072104168), Jul 20, 2010: INDICATOR. MALFUNCTIONED. COPILOTS HEADING INDICATOR WON'T AUTO SLAVE AND FLIGHT DIRECTOR DISAPPEARS. R & R NR 2 AHRS IAW AMM 34-20-05. PERFORMED COMPASS SWING, FOUND THE NR 2 AHRS UNIT - [SDR 2010F00058](https://openairdocs.org/sdr/2010F00058), Mar 4, 2010: CABIN PRESSURE. MALFUNCTIONED. ACFT WOULD NOT PRESSURIZE AFTER LIFTOFF. MAIN VALVES BOTH ON, DUMP VALVE CLOSED, CB'S ALL IN, AND AUTO PRESS SWITCH IN AUTO. CLIMBED TO 10000 BEFORE TURNING BAC - [SDR DXTA2009102003818](https://openairdocs.org/sdr/DXTA2009102003818), Oct 19, 2009: COFFEEMAKER. ODOR. PASSENGER NOTED ELECTRICAL BURNING ODOR COMING FROM THE FORWARD GALLEY. REMOVE GALLEY CIRCUIT BROKEN PANEL AND THREE EACH ACCESS PANEL TO GAIN ACCES TO GALLEY W - [SDR DXTA2008101403305](https://openairdocs.org/sdr/DXTA2008101403305), Oct 13, 2008: WARNING LIGHT. ILLUMINATED. ON GEAR RETRACTION RIGHT MAIN GEAR RED INDICATOR REMAINED LIT. - [SDR DXTA200809193278](https://openairdocs.org/sdr/DXTA200809193278), Sep 19, 2008: TRIM SYSTEM. UNKNOWN. AIRCRAFT RUNS OUT OF FWD TRIM NEAR VMO AT 25000 FT AND 310 KNOTS, THE TRIM WAS AT THE FWD STOP. UNABLE TO MOVE TRIM WHEEL FWD. T/S ELEVATOR TRIM BY COMPLYING WI - [SDR DXTA200803278](https://openairdocs.org/sdr/DXTA200803278), Sep 19, 2008: TRIM SYSTEM. FAULTY. AIRPLANE RUNS OUT OF FORWARD TRIM NEAR VMO AT 25000 FEET AND 310 KNOTS THE TRIM WAS AT THE FORWARD STOP. - [SDR DXTA200809063263](https://openairdocs.org/sdr/DXTA200809063263), Sep 6, 2008: SEQUENCE VALVE. OUT OF SEQUENCE. RT RED GEAR INTANSIT LIGHT REMAINED ILLUMINATED FOLLOWING GEAR RETRACTION AFTER TAKEOFF. DURING FLYBY TOWER INDICATED RT GEAR WAS PARTIALLY EXTENDED- AFTER GEAR - [SDR DXTA200809063262](https://openairdocs.org/sdr/DXTA200809063262), Sep 6, 2008: BUSHING. OUT OF ALIGNMENT. (M2B) - INSTALLED OH RT SEQUENCE VALVE MM 32-30-41 ALSO FOUND MISALIGNED BUSHING ON FWD LUG OF SIDESTAY. ALIGNED BUSHING FOR PROPER CLEARANCE. NO DAMAGE NOTED. - [SDR DXTA200808253247](https://openairdocs.org/sdr/DXTA200808253247), Aug 25, 2008: WARNING LIGHT. ILLUMINATED. RIGHT RED GEAR IN TRANSIT LIGHT REMAINED ON AFTER RETRACTING THE GEAR ON TAKEOFF. AIRCRAFT WAS JACKED AND AN OPERATIONAL CHECK OF THE LANDING GEAR COMPLETED, IA - [SDR DXTA200803247](https://openairdocs.org/sdr/DXTA200803247), Aug 25, 2008: INDICATOR. MALFUNCTIONED. RT RED GEAR IN TRANSIT LIGHT REMAINED ON AFTER RETRACTING THE GEAR ON TAKEOFF. - [SDR DXTA200802993](https://openairdocs.org/sdr/DXTA200802993), Apr 13, 2008: UPLOCK SWITCH. INOPERATIVE. RT MLG INDICATOR RED LIGHT STAYED ON. TROUBLESHOT SYSTEM. REMOVED AND REPLACED RT MLG DOOR UPLOCK SWITCH WITH NEW SWITCH IAW MM 32-60-00. REMOVED RT MLG DOOR FO - [SDR DXTA200802985](https://openairdocs.org/sdr/DXTA200802985), Apr 7, 2008: VALVE. MALFUNCTIONED. ON TO RT MLG DID NOT FULLY RETRACT. TROUBLESHOT BY REMOVING RT MLG REVERSING VALVE IN-LINE FILTER AND NON-RETURN VALVE. CLEANED AND INSPECTED. REASSEMBLED WITH - [SDR DXTA20082985](https://openairdocs.org/sdr/DXTA20082985), Apr 7, 2008: LANDING GEAR. MALFUNCTIONED. ON TAKEOFF, RT MLG DID NOT FULLY RETRACT . - [SDR DXTA200702699](https://openairdocs.org/sdr/DXTA200702699), Dec 20, 2007: ROLLER. MALFUNCTIONED. AFTER T/O AND GEAR RETRACTION THE RT MAIN GEAR RED LIGHT STAYED ON. FOUND RT IB GEAR DOOR (MAIN) UPLOCK ROLLER TO BE OUT OF RIG. RIGGED DOOR IAW HAWKER 800XP MM - [SDR DXTA200702646](https://openairdocs.org/sdr/DXTA200702646), Dec 3, 2007: SEQUENCE VALVE. MALFUNCTIONED. RT MAIN GEAR DOOR REMAINS OPEN WITH GEAR RETRACTED-TOWER VERIFIED GEAR DOOR-RT MAIN INDICATOR HAD RED LIGHT. REMOVED AND REPLACED RT MLG DOOR SEQUENCE VALVE IAW - [SDR DXTA200702628](https://openairdocs.org/sdr/DXTA200702628), Nov 25, 2007: SWITCH. OUT OF RIG. RT MAIN GEAR RED INDICATION REMAINED ILLUMINATED AFTER GEAR RETRACTION AND ALL GREEN INDICATORS WERE EXTINGUISHED. PERFORMED NUMEROUS OPS CHECKS OF GEAR WITHOUT - [SDR DXTA200702618](https://openairdocs.org/sdr/DXTA200702618), Nov 19, 2007: WARNING LIGHT. MALFUNCTIONED. RT MAIN GEAR RED INDICATION STAYED ILLUMINATED AFTER GEAR RETRACTION. ALL GREEN INDICATION WERE EXTINGUSHED. CHECKED RESISTANCE AND VOLTAGE ON MAIN GEAR DOWN LO - [SDR DXTA200702613](https://openairdocs.org/sdr/DXTA200702613), Nov 16, 2007: UPLOCK SWITCH. MALFUNCTIONED. RT MAIN GEAR (RED INDICATION) STAYED ILLUMINATED AFTER GEAR RETRACTION. ALL GREEN INDICATORS WERE EXTINGUISHED. GEAR DEPLOYED NORMALLY WITH ALL INDICATIONS IN T - [SDR DXTA200702193](https://openairdocs.org/sdr/DXTA200702193), May 14, 2007: UPLOCK SWITCH. INOPERATIVE. ON LANDING GEAR RETRACTION, THE RIGHT RED 'R' GEAR ANNUNCIATOR REMAINED ILLUMINATED. ALL OTHER GEAR INDICATIONS INCLUDING THE STANDBY WERE EXTINGUISHED. LANDING - [SDR DXTA200500901](https://openairdocs.org/sdr/DXTA200500901), Aug 15, 2005: LINK. WORN. ON DEPARTURE LEFT MAIN GEAR WOULD NOT RETRACT WITH ASSOCIATED RED GEAR UNSAFE LIGHT ILLUMINATED ON PANEL. REMOVED AND REPLACED LT SEQUENCE VALVE LINK AND TWO BU - [SDR DXTA200500780](https://openairdocs.org/sdr/DXTA200500780), Jun 17, 2005: LANDING GEAR. MALFUNCTIONED. LEFT MAIN GEAR WOULD NOT RETRACT NORMALLY AFTER TAKEOFF. ITEM IS UNDER INVESTIGATION. - [SDR DXTA200500755](https://openairdocs.org/sdr/DXTA200500755), Jun 5, 2005: LANDING GEAR. MALFUNCTIONED. LT MAIN GEAR WOULD NOT RETRACT FULLY. AFTER 6 MINUTES THE RED LIGHT WENT OUT BUT BASED ON POWER AND FUEL FLOW SETTINGS AND SPEEDS REFLECTED EXTRA DRAG. ON PUTTI - [SDR DXTA200500753](https://openairdocs.org/sdr/DXTA200500753), Jun 3, 2005: ACTUATOR. MALFUNCTIONED. LT MLG CAME UP ABOUT HALF WAY AND STOPPED. SAME INDICATION AS PREVIOUS WRITE-UP. LT MLG RED LIGHT. NO OTHER LIGHTS OR HORN. LANDED AT 22000 LBS WEIGHT. CHANGED - [SDR DXTA200500751](https://openairdocs.org/sdr/DXTA200500751), Jun 2, 2005: LANDING GEAR. MALFUNCTIONED. LT MLG WOULD NOT COME UP AFTER DEPARTURE. JACKED ACFT AND PERFORMED EXTENSION AND RETRACTION CHECKS PER HAWKER 800 XP MM CHAPTER 32-30-00. COULD NOT DUPLICATE L - [SDR DXTA200500666](https://openairdocs.org/sdr/DXTA200500666), Mar 30, 2005: FLAP. MALFUNCTIONED. FLAPS STOPPED MOVING AT APPROX 5 DEGREE POSITION (BOTH SIDES AT 5 DEGREE) DURING APPROACH INTO RIL WITH INTERMITTENT LIGHT ICING CONDITION, THEN WOULD NOT EXTEN - [SDR DXTA200500635](https://openairdocs.org/sdr/DXTA200500635), Mar 19, 2005: WARNING LIGHT. ILLUMINATED. WHEN GEAR WAS RETRACTED ON TAKEOFF RIGHT RED LIGHT WAS ILLUMINATED. GROUND PERSONNEL NOTED THAT THE GEAR APPEARED DOWN. ITEM IS UNDER INVESTIGATION. - [SDR DXTA200500606](https://openairdocs.org/sdr/DXTA200500606), Feb 21, 2005: CONTROL SYSTEM. MALFUNCTIONED. ELEVATOR/AILERON TRIM LIGHT ILLUMINATED AS POWER LEVERS WERE ADVANCED. RAN TRIMS FULL TRAVEL BOTH WAYS WOULD NOT EXTINGUISH. - [SDR DXTA200500560](https://openairdocs.org/sdr/DXTA200500560), Jan 25, 2005: LATCH. BROKEN. AFTER RETRACTION RT MAIN GEAR UNSAFE LIGHT REMAINED ILLUMINATED (RED LIGHT). RETRACTED GEAR AT 30 TIMES AT DIFFERENT PRESSURES NO DEFECTS NOTED. WIGGLED WIRES A - [SDR DXTA200500541](https://openairdocs.org/sdr/DXTA200500541), Jan 14, 2005: FILTER ELEMENT. CLOGGED. LEFT ENG FUEL LOOKUP LIGHT ILLUMINATED ON TAKEOFF ROLL FOLLOWING APPLICATION OF TAKEOFF POWER. REMOVED AND REPLACED LT & RT ENGINE FUEL FILTERS USING CUSTOMER S - [SDR DXTA200500525](https://openairdocs.org/sdr/DXTA200500525), Jan 10, 2005: WARNING LIGHT. ILLUMINATED. FOLLOWING GEAR RETRACTION THE RT MAIN GEAR UNSAFE LIGHT REMAINED ILLUMINATED, IT TOOK 2 GEAR RECYCLES TO EXTINGUISH THE UNSAFE CONDITION. ITEM IS UNDER INVESTIG - [SDR DXTA200400383](https://openairdocs.org/sdr/DXTA200400383), Sep 7, 2004: VALVE. MALFUNCTIONED. UPON GEAR RETRACTION THE RT GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED, COULD ALSO HEAR WIND NOISE. REMOVED AND REPLACED THE RT REVERSING VALVE IAW MM CHAPTER 2 - [SDR DXTA200400382](https://openairdocs.org/sdr/DXTA200400382), Sep 3, 2004: UPLOCK SWITCH. OUT OF ADJUST. UPON GEAR RETRACTION, THE RT MAIN GEAR INDICATION (RED) STAYED ON. OPS CHECKED GEAR AND FOUND NO FAULT, ADJUSTED RT UPLOCK INDICATOR SWITCH TO INCREASE MOVEMENT ## 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.