# N837QS: 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: 700-0082 - Year built: 2022 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: November 25, 2022 - Certificate issued: January 2, 2026 - Expires: January 31, 2033 - Mode S code: AB73CA - Owner type: Co-owned, fractional ownership - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=837QS - Page: https://openairdocs.org/aircraft/N837QS 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 N837QS. ## FAA accident and incident reports None matched to N837QS. ## Service difficulty reports (11) 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 DXTA2026100509987](https://openairdocs.org/sdr/DXTA2026100509987), Oct 1, 2026: WIRE HARNESS. DEFECTIVE. DURING CLIMB OUT WE RECEIVED A GROUND DETECT FAULT SIX TIMES. SHORTEST CAS MESSAGE WAS 5 SEC WHILE THE LONGEST WAS ABOUT 30 SEC. WE RAN THE QRH AND DIVERTED TO - [SDR DXTA2025100305157](https://openairdocs.org/sdr/DXTA2025100305157), Oct 1, 2025: SENSOR. FAULTED. RECURRING MALFUNCTION. ORIGINAL DISCOVERY T2PL6D00D5PN2 09/27/25 CLOSED WO T2PL6D00D5PN5 09/30/25. THIS FLIGHT, 09/30/25, AGAIN OBSERVED CAS MESSAGE "FUEL SCAV - [SDR DXTA2025093005121](https://openairdocs.org/sdr/DXTA2025093005121), Sep 27, 2025: SENSOR. FAULTED. DURING DESCENT, THE FUEL SCAV FAIL-R AMBER CAS MESSAGE ILLUMINATED. THE CHECKLIST WAS RUN AND TURNING ON BOTH FUEL PUMPS PER THE CHECKLIST RESULTED IN THE AMBER - [SDR DXTA2025082504707](https://openairdocs.org/sdr/DXTA2025082504707), Aug 23, 2025: LIGHT. DIM. EMERGENCY LIGHTS IN ARM POSITION WITH PAX SAFTEY BUTTON ON, INTERIOR MAIN CABIN DOOR EXIT, BUKHEAD EXIT, AND OVERWING EXIT LIGHTS ARE DIM AND FLICKER. EXTERIOR - [SDR DXTA2025012902106](https://openairdocs.org/sdr/DXTA2025012902106), Jan 25, 2025: APU. ODOR. WHEN THE APU WAS STARTED AND BLEED AIR IS ON THERE IS AN OILY MUSTY SMELL COMING FROM THE BLEED AIR. TURN BLEED AIR OFF AND IT DISIPATES. CAN NOTICE A VERY SLIG - [SDR DXTA2024111401128](https://openairdocs.org/sdr/DXTA2024111401128), Nov 12, 2024: STRIKER. LOOSE. MAIN DOOR: MAIN CABIN DOOR HANDLE DIFFICULT TO OPEN AND CLOSE. DOOR HANDLE BINDS MIDWAY WHEN OPENING AND CLOSING THE DOOR FROM INSIDE AND OUTSIDE THE AIRCRAFT. - [SDR DXTA2024111101104](https://openairdocs.org/sdr/DXTA2024111101104), Nov 9, 2024: UNKNOWN. ODOR. APU BLEED AIR: WITH APU RUNNING - MUSTY, OILY SMELL IS NOTICEABLE IN CABIN. SMELL DISSIPATES WITH APU OFF. CORRECTIVE ACTION; INSPECTED ALL THE DUCTING AROUND T - [SDR DXTA2024091900575](https://openairdocs.org/sdr/DXTA2024091900575), Sep 17, 2024: PCB. FAILED. ENGINE FIRE L RED CAS: AT FL310 RED L ENG FIRE LIGHT BEGAN TO FLICKER THEN FLASH AND THEN SOLID FOLLOWED BY ENG FIRE L CAS. AFTERWARS RECEIVED AMBER FIRE DETECT - [SDR DXTA2024091700550](https://openairdocs.org/sdr/DXTA2024091700550), Sep 15, 2024: PCB. DEFECTIVE. ENGINE FIRE L RED CAS: THROUGH APPROX FL 280 WE ENCOUNTERED A FLICKERING (NOT FLASHING) RED ENGINE FIRE L. SHORTLY AFTERWARDS IT EXATINQUISHED AND WE GOT A YELL - [SDR DXTA2024020910838](https://openairdocs.org/sdr/DXTA2024020910838), Feb 8, 2024: BATTERY. DEFECTIVE. EMERGENCY LIGHTS DURING POWER ON CHECKLIST DO NOT WORK. REMOVED AND REPLACED FWD #1 EMERGENCY LIGHT PACK. OPS CHECICS GOOD, REF CE-700 AMM 33-50-07. BATTERY PN - [SDR DXTA2024020610812](https://openairdocs.org/sdr/DXTA2024020610812), Feb 5, 2024: G SWITCH. DEFECTIVE. EMERGENCY LIGHTING: EMERGENCY LIGHT BATTERIES NOT HOLDING THEIR CHARGE. NOT WORKING ON ON OR ARM. REMOVED AFT BAGGAGE WALL TO ACCESS AFT SWITCHES/BATTERYS. R&R ## Service difficulty reports on N837QS not matched to an aircraft (27) They name N837QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DXTA2017073106431](https://openairdocs.org/sdr/DXTA2017073106431), Jul 31, 2017: ENGINE. OVERHEATED. DURING TAKE OFF, RIGHT ITT WENT TO APPROXIMATELY 740 DEGREES FOR ABOUT 2 SECONDS SOON AFTER LIFT OFF. IMMEDIATELY REDUCED THRUST ON RIGHT ENGINE AND ITT RETURNE - [SDR EBVR20170608001](https://openairdocs.org/sdr/EBVR20170608001), Jun 8, 2017: WIRE. BURNED. WHEN PRESSURIZATION, THE KNOB WAS SELECTED TO ANY POSITION OTHER THAN NORMAL, THE NORMAL AND EMERGENCY PRESSURIZATION CIRCUIT BREAKERS TRIPPED. FOUND DURING POS - [SDR EBVR20170606001](https://openairdocs.org/sdr/EBVR20170606001), Jun 6, 2017: BRACKET. CORRODED. CORRODED AILERON QUADRANT BRACKET. REPLACED THE CORRODED AILERON QUADRANT BRACKET IAW EO ERO-896682. REV IR. - [SDR DXTA2016121706343](https://openairdocs.org/sdr/DXTA2016121706343), Dec 17, 2016: UNKNOWN. ODOR. THE WINDSHIELD AIR OVERHEAT LIGHT ILLUMINATED DURING DESCENT IN ICING CONDITIONS. THE RAT WAS 5 DEGREES. COULD ALSO SMELL A BURNING ODOR. PERFORMED MULTIBLE OPS - [SDR DXTR2016111301](https://openairdocs.org/sdr/DXTR2016111301), Nov 13, 2016: BLOCK. WORN. LT & RT RUDDER PHENOLIC RUB BLOCKS ARE WORN OUT OF LIMITS ALLOWING THE CABLES TO CONTACT THE ALUMINUM AIRCRAFT STRUCTURE. REPAIRED IAW ERO-870610. - [SDR DXTR2016110701](https://openairdocs.org/sdr/DXTR2016110701), Nov 7, 2016: DOUBLER. DAMAGED. AFT VERTICAL STABILIZER DOUBLER AT WL 160.00 DAMAGED. REPAIRED IAW ERO-868612. - [SDR DXTR2016110401](https://openairdocs.org/sdr/DXTR2016110401), Nov 4, 2016: SKIN. DENTED. LT WING LOWER LEADING EDGE SKIN HAS A 5" LONG DENT CENTERED AT APPROXIMATELY WS 139.07. ACCOMPLISHED REPAIR IAW REPORT S-560-0685/04RD. - [SDR DXTR2016103102](https://openairdocs.org/sdr/DXTR2016103102), Oct 31, 2016: SKIN. GOUGED. LT FUSELAGE SKIN AT WING FAIRING SCRATCHED (GOUGED) APPROXIMATE LOCATION FS 254.00 WL.100. SKIN THICKNESS IN THIS AREA IS 0.040". REPAIRED IAW ENGINEERING ORDER - [SDR DXTR2016103101](https://openairdocs.org/sdr/DXTR2016103101), Oct 31, 2016: DRAG ANGLE. CRACKED. LEFT WING FWD UPPER DRAG ANGLE HAS A CRACK APPROXIMATELY 0.20" LONG. COMPLIED WITH ERO-867731 REVISION 1R. - [SDR CWQR20160307011](https://openairdocs.org/sdr/CWQR20160307011), Mar 7, 2016: RHEOSTAT. BURNED. REPLACED FLIGHT COMPARTMENT FLOOD LIGHT RHEOSTAT DUE TO DEAD SPOTS ON RHEOSTAT. DURING OPERATIONAL CHECK OF NEW RHEOSTAT, WHEN SELECTING DIM, THE RHEOSTAT HEATE - [SDR DXTA2016010806159](https://openairdocs.org/sdr/DXTA2016010806159), Jan 11, 2016: LANDING GEAR. MALFUNCTIONED. LANDING GEAR WOULD NOT RETRACT. HANDLE IN THE UP POSITION INDICATIONS WERE, 3 GREEN, 1 RED UNSAFE & HYD PRESS ALL ILLUMINATED. NO GEAR MOVEMENT NOTED. CYCLED HA - [SDR DXTA2015072306046](https://openairdocs.org/sdr/DXTA2015072306046), Jul 21, 2015: COMPRESSOR. SHUTDOWN. AIR CONDITIONING COMPRESSOR SHUT ITSELF OFF WHILE ON THE GROUND WITH GROUND POWER UNIT, IMMEDIATELY CREATED A SMOKY ODOR INSIDE THE CABIN. BLACK SMOKE WAS VISIB - [SDR DXTR2014061002](https://openairdocs.org/sdr/DXTR2014061002), Jun 5, 2014: SKIN. DENTED. FOUND DENT NEAR NOSE JACK PAD, FWD PRESSURE BULKHEAD AREA. ACCOMPLISHED NDT EDDY CURRENT & ULTRASONIC INSPECTION AT LT LOWER FORWARD PRESSURE BULKHEAD AREA AROU - [SDR DXTR2014011701](https://openairdocs.org/sdr/DXTR2014011701), Jan 3, 2014: WIRE HARNESS. CHAFED. FOUND SEVERAL FUEL PROBE WIRES CHAFING IN SEVERAL SPOTS IN LT WING FUEL TANK FROM WHAT APPEARS TO BE THE RESULT OF TIE RAP RUBBING. R & R CHAFED WIRES & INSTALL - [SDR DXTR2013120201](https://openairdocs.org/sdr/DXTR2013120201), Dec 2, 2013: DOOR. UNKNOWN. DURING PREPARATION FOR A PHASE 5 INSPECTION, TECHNICIANS WERE UNABLE TO FREELY OPEN THE EMERGENCY EXIT DOOR WITHOUT EXERTING EXTREME FORCE. THIS IS THE SECOND E - [SDR DXTR2013062101](https://openairdocs.org/sdr/DXTR2013062101), Jun 21, 2013: DOOR. STUCK. DURING COMPLIANCE OF INSPECTION TASK 041008 CHAPTER 4 EMERGENCY EXIT DOOR FRAME "INSPECTION TIME LIMITS" TASK 53-10-09-212, TECHNICIANS WERE UNABLE TO FREELY OP - [SDR DXTA2013012405259](https://openairdocs.org/sdr/DXTA2013012405259), Jan 23, 2013: VALVE. INOPERATIVE. IN CRUISE AT 45,000, ACM O'HEAT AND EMERGENCY PRESSURE ANNUNCIATORS ILLUMINATED. THE EMERGENCY PRESSURE VALVE DID NOT OPEN AUTOMATICALLY. CABIN STARTED RISING A - [SDR DXTA2011071804659](https://openairdocs.org/sdr/DXTA2011071804659), Jul 17, 2011: MODULE. FAILED. ON GROUND WITH GPU, AVOINICS AND AIR CONDITIONING ON, CABIN BEGAN TO FILL WITH AN ACIDIC WHITE SMOKE. AIR CON COMPRESSOR LIGHT WAS STILL ON. SHUT OFF ENTIRE ELE - [SDR DXTA20101104333](https://openairdocs.org/sdr/DXTA20101104333), Nov 28, 2010: WARNING LIGHT. MALFUNCTIONED. NOSE GEAR RED UPLOCK LIGHT FAILED TO EXTINGUISH DURING TAKEOFF GEAR RETRACTION. - [SDR DXTA2010011103941](https://openairdocs.org/sdr/DXTA2010011103941), Jan 8, 2010: RUDDER PEDAL. OBSTRUCTED. WHILE TAXIING TO A RT TURN, THERE WAS A LOUD BANG FROM THE RUDDER PEDAL AREA. THERE WAS ALSO REDUCED RUDDER PEDAL TRAVEL AND FREEDOM OF MOVEMENT. INSPECTED RUDD - [SDR DXTA200803129](https://openairdocs.org/sdr/DXTA200803129), Jun 17, 2008: TIRE. FAILED. RT MAIN TIRE BLEW ON TAKEOFF ROLL, ABORTED T/O. REMOVED AND REPLACED RT MLG WHEEL AND TIRE ASSY WITH REPAIRED ASSY. SERVICED TIRE TO 163 PSI WITH NITROGEN. WORK - [SDR DXTA200802757](https://openairdocs.org/sdr/DXTA200802757), Jan 9, 2008: LANDING GEAR. INOPERATIVE. LANDING GEAR WOULD NOT RETRACT AFTER TAKE-OFF. PLACED AIRCRAFT ON JACKS. INSTALLED ROBO MULE TO RIGHT ENGINE TO PERFORMED LANDING GEAR OPERATIONAL CHECKS. INSPE - [SDR DXTA200702636](https://openairdocs.org/sdr/DXTA200702636), Nov 29, 2007: LAMP. INOPERATIVE. YAW DAMPNER WOULD NOT ENGAGE ON DEPARTURE. PERFORMED AND CHECK AND FOUND BOTH LAMP IN THE SWITCH/IND BURNED. RELALMPED AND PERFORMED A GOOD OPERATIONAL CHECK RE - [SDR DXTA200701984](https://openairdocs.org/sdr/DXTA200701984), Mar 1, 2007: CONNECTOR. DIRTY. WHEN GEAR SELECTED DOWN WE HAS A NOSE AND LT MAIN DOWN INDICATION BUT NO RT AND A GEAR UNLOCK LIGHT STAYED ON. GEAR RETRACTED ON GO AROUND. WHEN RETRACTED ON GO - [SDR DXTA200501027](https://openairdocs.org/sdr/DXTA200501027), Oct 16, 2005: WARNING LIGHT. ILLUMINATED. UPON GEAR EXTENSION GOING INTO SUN, THE GEAR LIGHTS INDICATED 2 GREEN 1 RED. THE LT MAIN WAS NOT INDICATING GREEN. TURNED OUT OF THE VALLEY TO RUN THE EMERGENCY - [SDR DXTA200501000](https://openairdocs.org/sdr/DXTA200501000), Oct 4, 2005: STATIC PORT. CONTAMINATED. DURING TAKEOFF ROLL THE RIGHT AIRSPEED TAPE ADVANCED PRIOR TO THE LEFT, AFTER LEFT TAPE BEGAN TO ADVANCE IAW ANNUNCIATOR APPEARED ON BOTH PFD'S. TAKEOFF ABORTED - [SDR DXTA200500759](https://openairdocs.org/sdr/DXTA200500759), May 31, 2005: LANDING GEAR. MALFUNCTIONED. NOSE GEAR WILL NOT RETRACT. PERFORMED LANDING GEAR HYDRO SYSTEMS ADJUSTMENT TEST IAW 560 MM 32-01-00. OPS CHECK GOOD. INSPECTED NOSE GEAR, NO DEFECTS FOUND. ## 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.