# N834QS: 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: 700-0079 - Year built: 2022 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 14, 2022 - Certificate issued: April 1, 2026 - Expires: April 30, 2033 - Mode S code: AB68A5 - Owner type: Co-owned, fractional ownership - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=834QS - Page: https://openairdocs.org/aircraft/N834QS 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 N834QS. ## FAA accident and incident reports None matched to N834QS. ## 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 DXTA2026071308773](https://openairdocs.org/sdr/DXTA2026071308773), Jul 9, 2026: SHUTOFF VALVE. FAILED. INTERMITTENT AMBER FUEL FW S/O FAIL R CAS MESSAGE. THE RT ENGINE DID NOT SHUT DOWN. REMOVED RIGHT FUEL SHUTOFF VALVE AND INSTALLED RIGHT FUEL SHUTOFF VALVE, OPS - [SDR 2025F00131](https://openairdocs.org/sdr/2025F00131), May 22, 2025: THRUST REVERSER. CORRODED. THRUST REVERSER CORROSION. ACCOMPLISHED CORROSION REMOVAL AND REPAIR TO LH AND RH THRUST REVERSER BEAMS AND PIVOT DOORS INNER AIR WASHED SURFACES IAW SAFRAN NAC - [SDR DXTA2025040102862](https://openairdocs.org/sdr/DXTA2025040102862), Mar 30, 2025: STRIKER. OUT OF ADJUST. MAIN DOOR: MAIN CABIN DOOR IS BINDING WHEN HANDLE IS RELEASED AND NOT FREEFALLING OPEN. WHEN VIEWED FROM INSIDE, APPEARS TO BE BINDING ON THE LEFT SIDE. IN ADDI - [SDR DXTA2025013102144](https://openairdocs.org/sdr/DXTA2025013102144), Jan 28, 2025: SENSOR. DEFECTIVE. LEFT MLG BRAKE: DURING TAXI AN AMBER BRAKE TEMP CAS MESSAGE DISPLAYED VERY BRIEFLY AND THEN A WHITE BRAKE TEMP FAULT CAS MESSAGE DISPLAYED FOR SEVERAL MINUTES. - [SDR DXTA2024123001705](https://openairdocs.org/sdr/DXTA2024123001705), Dec 26, 2024: SENSOR. INOPERATIVE. REPEAT WRITE UP- AFTER T/O COULD NOT RETRACT GEAR (HANDLE LOCKED DOWN) ABMER GROUND DETECT FAULT CAS, AMBER T/R FAIL L AND R CAS, WHITE BRAKE FAULT CAS. AFTER C - [SDR DXTA2024100800782](https://openairdocs.org/sdr/DXTA2024100800782), Oct 7, 2024: SHIM. OUT OF POSITION. MAIN DOOR: MAIN CABIN DOOR WOULD NOT OPEN AFTER LANDING. PASSENGER DEPLANED THROUGH BAGGAGE DOOR. DOOR OPENED WITH INE CREWMEMBER OUTSIDE PULLING AND ONE INSIDE - [SDR DXTA2024080112492](https://openairdocs.org/sdr/DXTA2024080112492), Jul 31, 2024: HANDLE. BINDING. THE MAIN DOOR IS VERY HARD TO OPEN. ON THE OUTSIDE, THE HANDLE OPENS FULLY, BUT YOU HAVE TO PULL HARD TO GET IT TO MOVE. ON THE INSIDE, THE HANDLE IS HARD TO MO - [SDR DXTA2024061011996](https://openairdocs.org/sdr/DXTA2024061011996), Jun 7, 2024: FILTER. DEFECTIVE. AFTER TAKEOFF WHILE CLIMBING THROUGH 1,000FT, AN ACRID ODOR IS DETECTED COMING THROUGH THE INSTRUMENT PANEL GASPERS. ODOR SUBSIDES AFTER CLIMBING THROUGH 4,000F - [SDR DXTA2024020510805](https://openairdocs.org/sdr/DXTA2024020510805), Feb 4, 2024: HANDLE. BINDING. MAIN DOOR: MAIN CABIN DOOR HANDLE IS BINDING WHEN OPENING AND CLOSING DOOR. OPENING DOOR AFTER A LONG FLIGHT IS ESPECIALLY DIFFICULT. OPEN AND CLOSED CABIN DOOR - [SDR DXTA2024010910566](https://openairdocs.org/sdr/DXTA2024010910566), Jan 9, 2024: BATTERY. NO TEST. EMERGENCY BATTERY CHARGES BUT WILL NOT KEEP CHARGE. EMERGENCY LIGHT WILL NOT ILLUMINATE 2 HRS AFTER ACFT SHUTDOWN. GAINED ACCESS TO THE #1 & 4 BATTERY PACKS & S - [SDR DXTA2023121110284](https://openairdocs.org/sdr/DXTA2023121110284), Dec 8, 2023: UNKNOWN. UNKNOWN. EMERGENCY LIGHTS FAILED TO TEST ON POWER ON CHECKLIST. COMPLIED WITH NJA TASK CARD TC·FLT-33-1001. ALL EMERGENCY LIGHTS OPERATED CORRECTLY WITH NO DEFECTS NOTED - [SDR DXTA2023011078210](https://openairdocs.org/sdr/DXTA2023011078210), Jan 10, 2023: CONNECTOR. DISCONNECTED. CABIN EMERG LIGHT: FLOOR EMER LIGHT AT SEAT 5 INOP. FOUND THE CONNECTOR DISCONNECTED. RECONNECTED AND OPS CHECKS GOOD. WORK DONE IN REF TO CE-700 AMM 33-50-00. ## Service difficulty reports on N834QS not matched to an aircraft (16) They name N834QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR 2018F00028](https://openairdocs.org/sdr/2018F00028), Oct 27, 2017: SKIN PANEL. CORRODED. UPPER WING SKIN CORRODED. - [SDR DXTA2017062306416](https://openairdocs.org/sdr/DXTA2017062306416), Jun 23, 2017: UNKNOWN. ODOR. IMMEDIATELY AFTER TAKEOFF, CREW DETECTED A STRONG ELECTRICAL BURNING ODOR AND RETURNED TO DEPARTURE. NO SMOKE PRESENT. TURNED OFF AIR CONDITIONING, FORWARD, AFT - [SDR DXTR2017012901](https://openairdocs.org/sdr/DXTR2017012901), Jan 29, 2017: SERVICE DOOR. DELAMINATED. THE OUTBOARD EDGE OF THE HYDRAULIC ACCESS DOOR HAS DELAMINATION, THE DAMAGE MEASURES APPROXIMATELY 3.0 INCHES LONG. ACCOMPLISHED MINOR REPAIR OF HYDRAULIC ACCES - [SDR 2017F00124](https://openairdocs.org/sdr/2017F00124), Jan 28, 2017: SKIN. GOUGED. THE LT SIDE OF THE FUSELAGE HAS SEVERAL GOUGES. DAMAGE IS LOCATED AT BS 253.4 ABOVE STRINGER WL 104.8. ACCOMPLISHED MAJOR REPAIR IAW AQRD ERO 880379. - [SDR DXTR2017012801](https://openairdocs.org/sdr/DXTR2017012801), Jan 28, 2017: SKIN. GOUGED. THE LT SIDE OF THE FUSELAGE HAS SEVERAL GOUGES. DAMAGE IS LOCATED AT FS 253.4 JUST ABOVE STRINGER WL 104.8. ACCOMPLISHED MAJOR REPAIR IAW AQRD ERO-880379. - [SDR DXTA201404105726](https://openairdocs.org/sdr/DXTA201404105726), Apr 10, 2014: SWITCH. INOPERATIVE. AFTER EXTENDING GEAR, LOW BRAKE PRESSURE & ANTISKID LIGHT REMAINED ILLUMINATED. RAN CHECKLIST WHICH REQUIRED CHECKING CIRCUIT BREAKERS. BOTH THE SKID CONTROL & - [SDR DXTA2011052604592](https://openairdocs.org/sdr/DXTA2011052604592), May 25, 2011: PRESSURE SWITCH. FAILED. LEVELING AT 45,000, RECEIVED RED "CABIN ALT" & "MASTER WARNING" LIGHTS. MASTER WARNING LIGHT CANCELLED, CABIN ALT LIGHT STAYED ON. PAX MASKS DID NOT DROP. CABIN - [SDR 2010FA0001114](https://openairdocs.org/sdr/2010FA0001114), Oct 5, 2010: ROLLER. WORN. THE PN LISTED IN LINE 5 IS A 5000 LANDING REPLACEMENT ITEM AS REQUIRED IN CHAPTER 4 OF THE MM. THESE DEFECTIVE ROLLERS WERE FOUND WHILE PERFORMING OTHER WORK TH - [SDR DXTA2009080703754](https://openairdocs.org/sdr/DXTA2009080703754), Aug 7, 2009: BLOWER. SMOKE. DURING FLIGHT CREW OBSERVED WHAT SOUNDS LIKE A FAN HUMMING SOUNDS COMPARABLE TO WHAT IT SOUNDS LIKE WHEN ENGINES ARE OUT OF SYNCH. UPON LANDING PAX INFORMED US - [SDR DXTA20082950](https://openairdocs.org/sdr/DXTA20082950), Mar 19, 2008: PITOT SYSTEM. CONTAMINATED. ON TAKEOFF ROLL F/O AIRSPEED MISCOMPAIRED WITH CAPT A/S, TAKEOFF WAS ABORTED. DRAINED OUT EXCESS WATER FROM THE PITOT PROBES AND STATIC PROBES, AND PERFORMED AN - [SDR DXTA200802784](https://openairdocs.org/sdr/DXTA200802784), Jan 21, 2008: INDICATOR. INOPERATIVE. ON TAKEOFF CAPT'S AIRSPEED GAVE NO INDICATION, RED AIRSPEED ENUNCIATION SHOWED ON AIRSPEED INDICATOR. SIMULATED AIRSPEED WITH PITOT/STATIC TEST SET AND COULD NO - [SDR DXTA200702616](https://openairdocs.org/sdr/DXTA200702616), Nov 17, 2007: PIN. OUT OF ADJUST. MAIN CABIN DOOR IS VERY DIFFICULT TO OPEN FROM INSIDE AFTER FLIGHT. FOUND LOWER AFT DOOR PIN OUT OF ADJUSTMENT, ADJUSTED AFT LOWER DOOR PIN IAW CE560 M/M CH 52- - [SDR DXTA200601596](https://openairdocs.org/sdr/DXTA200601596), Sep 9, 2006: PRESSURE SWITCH. FAILED. DURING TAKEOFF UPON APPLICATION OF TAKEOFF POWER THE LEFT FUEL FILTER BYPASS LIGHT ILLUMINATED. TAKEOFF WAS ABORTED. CHANGED FUEL FILTER AND DIFFERENTIAL FUEL S - [SDR DXTA200601527](https://openairdocs.org/sdr/DXTA200601527), Jul 30, 2006: WARNING LIGHT. ILLUMINATED. ON TAKEOFF. ADVANCED THROTTLES TO 88.7 PERCENT. UPON REACHING 88.7 PERCENT THE RT ENGINE FUEL FILTER BYPASS ANNUNCIATOR ILLUMINATED. ITEM IS UNDER INVESTIGATION - [SDR DXTA200601225](https://openairdocs.org/sdr/DXTA200601225), Feb 1, 2006: SWITCH. LOOSE. TAIL CONE DOOR ANNUNCIATOR ILLUMINATED ON THE TAKEOFF ROLL. TAKEOFF ABORTED. DUPLICATED DISCREPANCY: FOUND DOOR LOCK SW WAS LOOSE AND OUT OF ADJUSTMENT. SECURED - [SDR DXTA200501171](https://openairdocs.org/sdr/DXTA200501171), Dec 30, 2005: LINE. FAILED. AFTER LANDING POWER BRAKE AND ANTISKID MASTER CAUTION ILLUMINATED AFTER 1 SECONDS. AFTER 10 SECONDS OF ILLUMINATION TOTAL BRAKE FAILURE OCCURRED. EMERGENCY BRAK ## 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.