# N829QS: 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: 700-0072 - Year built: 2022 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 11, 2022 - Certificate issued: April 3, 2026 - Expires: April 30, 2033 - Mode S code: AB53B9 - Owner type: Co-owned, fractional ownership - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=829QS - Page: https://openairdocs.org/aircraft/N829QS 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 N829QS. ## FAA accident and incident reports None matched to N829QS. ## Service difficulty reports (15) 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 DXTA2026100509984](https://openairdocs.org/sdr/DXTA2026100509984), Oct 1, 2026: SWITCH. OUT OF POSITION. AFTER RECEIVING TAXI INSTUCTIONS, TOE BRAKES APPLIED & RELEASED PARKING BRAKE. BRAKES SLIGHTLY SPONGY. ACFT BEGAN ROLLING WITHOUT RELEASING BRAKES OR POWER. REC - [SDR DXTA2026052608173](https://openairdocs.org/sdr/DXTA2026052608173), May 20, 2026: UPLOCK SWITCH. FAULTY. IN CRUISE FLIGHT AT FL430, WE HEARD A LOUD WIND NOISE AND FELT A SLIGHT VIBRATION. SHORTLY AFTER, WE RECEIVED A GEAR DOOR OPEN AMBER MESSAGE FOLLOWED BY A GEAR - [SDR DXTA2025050203297](https://openairdocs.org/sdr/DXTA2025050203297), Apr 30, 2025: GASKET. FAILED. PNEUMATIC INDICATION: AMBER CAS BLEED O'PRESS L ANNUNCIATION SHORTLY AFTER TAKEOFF. EMERGENCY/ABNORMAL CHECKLIST 13D COMPLETED. CORRECTIVE ACTION: REFER TO STEP - [SDR DXTA2025040602974](https://openairdocs.org/sdr/DXTA2025040602974), Apr 6, 2025: APU. ODOR. CABIN ODOR: UPON ENTERING AIRCRAFT WITH APU OFF, THERE IS A STRONG ODOR WHICH SMELLS JUST LIKE DIRTY COALESCER SOCKS. WITH APU RUNNING AND ALSO DURING CRUISE FL - [SDR 2025F00031](https://openairdocs.org/sdr/2025F00031), Feb 3, 2025: STRUCTURE. CORRODED. R/H THRUST REVERSER HAS CORROSION ON LOWER BUCKET ASSEMBLY. REFERENCE SAFRAN REPAIR SCHEME NO> 907-623, REV B, DATED 01/03/2024 - [SDR 2025F00029](https://openairdocs.org/sdr/2025F00029), Feb 3, 2025: STRUCTURE. CORRODED. L/H THRUST REVERSER HAS CORROSION ON LWR BUCKET ASSEMBLY. REFERENCE SAFRAN REPAIR SCHEME NO. 907-623, REV B, DATED 01/03/2024. - [SDR 2025F00030](https://openairdocs.org/sdr/2025F00030), Feb 3, 2025: STRUCTURE. CORRODED. L/H THRUST REVERSER HAS CORROSION ON UPR BUCKET ASSEMBLY. REFERENCE SAFRAN REPAIR SCHEME NO. 907-623, REV B, DATED 01/03/2024. - [SDR DXTA2024123001720](https://openairdocs.org/sdr/DXTA2024123001720), Dec 27, 2024: RETAINING RING. BROKEN. HINGE PIN ON LIFTING BAR MECHANISM ON FORWARD SIDE OF DOOR IS MISSING/BROKEN ON FIRST FLIGHT OF DAY AFTER AIRCRAFT CLEANING PERFORMED OVERNIGHT. FOUND SOME HARD - [SDR DXTR2024061601](https://openairdocs.org/sdr/DXTR2024061601), Jun 16, 2024: STRUCTURE. CORRODED. R/H T/R BUCKET HAS SIGNS OF CORROSION BEGINNING TO FORM... ACCOMPLISHED MINOR PERMANENT REPAIR IAW RFTS-111031 DATED 06/16/2024. - [SDR DXTR2024061201](https://openairdocs.org/sdr/DXTR2024061201), Jun 5, 2024: THRUST REVERSER. CORRODED. LH T/R BUCKET HAS CORROSION ON OUTBD SIDE, L/H T/R TO BE REMOVED AND SENT OUT TO BE REPAIRED PER CUSTOMER REQUEST. REMOVED L/H T/R ASSY IAW CE700 MM 78-30-00. P - [SDR DXTA2022110273120](https://openairdocs.org/sdr/DXTA2022110273120), Nov 1, 2022: PCB. DAMAGED. MAIN DOOR: MAIN CABIN DOOR AMBER CAS MSG CYCLES MULTIPLE TIMES OFF AND ON WHEN DOOR CLOSED. RAN QRH MANY TIMES AND ALSO COMPLETE SHUT DOOR WITH NO AUCCESS. THIS - [SDR DXTA2022090969990](https://openairdocs.org/sdr/DXTA2022090969990), Sep 8, 2022: NONE. NONE. MAIN DOOR: WITH BATTERIES CONNECTED, MAIN CABIN DOOR DOES NOT OPEN WHEN UNLATCHED. DOOR MUST BE MANUALLY MOVED TEN INCHES (TOP EDGE) BEFORE DOOR BEGINS TO OPEN. - [SDR DXTA2022090769850](https://openairdocs.org/sdr/DXTA2022090769850), Sep 7, 2022: NONE. NONE. MAIN DOOR: RECEIVED CABIN DOOR OPEN MESSAGE AFTER LANDING. RAN CHECKLIST MULTIPLE TIMES MESSAGE WOULD NOT CLEAR. AMBER LIGHT ON MAIN CABIN DOOR REMAINED ON . - [SDR DXTA2022081668150](https://openairdocs.org/sdr/DXTA2022081668150), Aug 17, 2022: SIGN. INOPERATIVE. EMERG EXIT SIGN/LIGHT: EMERGENCY EXIT SIGN ABOVE SEAT THREE ILLUMINATES INTERMITTENTLY IN ON POSITION AND WHEN SWITCHED TO ARM POSITION LIGHT EXTINGUISHES//CORR - [SDR DXTA2022071165550](https://openairdocs.org/sdr/DXTA2022071165550), Jul 8, 2022: PAWL. OUT OF ADJUST. MAIN DOOR: MAIN CABIN DOOR AMBER CAS CYCLED DOOR NUMEROUS TIMES // SIGNOFF// MAIN CABIN DOOR AMBER CAS CYCLED DOOR NUMEROUS TIMES FOUND CABIN DOOR PAWL SWITCH S ## Service difficulty reports on N829QS not matched to an aircraft (13) They name N829QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR JGVR20180830002](https://openairdocs.org/sdr/JGVR20180830002), Aug 30, 2018: SKIN. CORRODED. FOUND AND BLENDED CORROSION N LT AND RT UPPER WING CENTER SPAR CAP FWD AND AFT SKIN SEAMS FROM WING ROOT TO APPROX. WS 85. PERFORMED NDT AND REPORTED FOR DISPOS - [SDR JGVR20180830001](https://openairdocs.org/sdr/JGVR20180830001), Aug 30, 2018: SKIN. CORRODED. FOUND AND BLENDED CORROSION ON THE EXTERNAL FUSELAGE SKIN BETWEEN THE MAIN CABIN DOOR AND THE AFT COCKPIT WINDOW AT APPROXIMATELY WL 149 AND FS 155.5. BLENDED C - [SDR DXTA2018080901285](https://openairdocs.org/sdr/DXTA2018080901285), Aug 8, 2018: MOTOR. FAILED. ON THE GROUND, FUMES DETECTED IN THE CABIN. FOUND BLACK SMOKE COMING FROM HELL HOLE. SECURED THE ELECTRIC POWER AND DISCONNECTED THE BATTERY AND GPU. REMOVED AN - [SDR EBVR20171016001](https://openairdocs.org/sdr/EBVR20171016001), Oct 16, 2017: SKIN. DELAMINATED. LEFT INBOARD FLAP ASSEMBLY DELAMINATED. REPAIRED THE FLAP ASSEMBLY IAW ERO-907978, REV IR. - [SDR DXTR2016101901](https://openairdocs.org/sdr/DXTR2016101901), Oct 19, 2016: WEB. GOUGED. THE OUTBOARD WEB ON THE LT WING HAS A GOUGE IN THE METAL. DAMAGE MEASURES APPROXIMATELY 0.75 INCHES LONG & IS 0.007 INCHES DEEP AT THE DEEPEST POINT. - [SDR DXTA2015092906094](https://openairdocs.org/sdr/DXTA2015092906094), Sep 28, 2015: ENTERTAIN SYS. OVERHEATED. AREA AROUND SEAT 6 SMELLED OF OVERHEATED ELECTRONICS. XM CONTROL HEAD & RT CABIN AC OUTLET WERE EXTREMELY HOT. BOTH CREW MEMBERS CONFIRMED THE HOT AREAS. COULD - [SDR DXTA2014050505763](https://openairdocs.org/sdr/DXTA2014050505763), May 4, 2014: TIRE. OUT OF ROUND. AIRCRAFT TAXIED NORMALLY, AFTER ADVANCING THROTTLES & COMMENCING TAKEOFF ROLL, ACFT DEMONSTRATED SIGNIFICANT VIBRATION FELT IN NOSE WHEEL AREA & RT GEAR WELL. P - [SDR DXTA2013010405232](https://openairdocs.org/sdr/DXTA2013010405232), Dec 22, 2012: RECEIVER. FAILED. THE CREW REPORTED, ENROUTE, AND AT ALTITUDE, DETECTED AN ELECTRICAL ODOR. NO SMOKE VISIBLE. INTERIOR MASTER WAS SHUTOFF AND THE ODOR WENT AWAY. FOUND SATELLITE - [SDR DXTA2012032204928](https://openairdocs.org/sdr/DXTA2012032204928), Mar 21, 2012: BRAKE SYS. MALFUNCTIONED. LEFT BRAKE PEDAL EXTENDS FARTHER THAN RT BRAKE PEDAL WHEN BRAKING, BEFORE BECOMING EFFECTIVE. SAME ON PILOT AND CO-PILOT SIDES. BLED LT BRAKE, OPS CHECKED GOOD. - [SDR DXTA2012031204917](https://openairdocs.org/sdr/DXTA2012031204917), Mar 11, 2012: BRAKE. WEAK. LEFT BRAKE ON PILOTS AND COPILOTS SIDE IS SPONGY AND THE PEDAL TRAVELS APPROX 2" TO 3" FURTHER THAN THE RT. RT BRAKE ALSO GRABS BEFORE THE LT. BRAKES BLED FOR I - [SDR CWQR2011110926](https://openairdocs.org/sdr/CWQR2011110926), Nov 9, 2011: TORQUE TUBE. CRACKED. DURING A SCHEDULED INSPECTION, FOUND THE NLG DOOR TORQUE TUBE CRACKED AT THE MOUNT BOLT PIVOT PLATE IN 2 PLACES. R & R TORQUE TUBE. - [SDR DXTA2010072904181](https://openairdocs.org/sdr/DXTA2010072904181), Jul 28, 2010: MOTOR. FAILED. NOTICED ELECTRIC BURNING ODOR IN AIRPLANE WHILE ON GROUND WITH GPU CONNECTED, AIR CONDITIONING ON, AND BOTH FANS OPERATING. NOTICED SMOKE COMING FROM AIR CONDIT - [SDR DXTA2009121103893](https://openairdocs.org/sdr/DXTA2009121103893), Dec 10, 2009: INDICATOR. MALFUNCTIONED. LT MLG LIGHT DID NOT COME ON UPON EXTENDING THE GEAR. THE RED GEAR UNSAFE LIGHT WAS NOT ON. RAN THE EMERGENCY GEAR EXTEND CHECKLIST, PULLED KNOB AND BLEW BOTTLE ## 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.