# N830QS: 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: 700-0073
- Year built: 2022
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 13, 2022
- Certificate issued: February 5, 2026
- Expires: February 28, 2033
- Mode S code: AB59C9
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=830QS
- Page: https://openairdocs.org/aircraft/N830QS

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 N830QS.

## FAA accident and incident reports

None matched to N830QS.

## 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 DXTA2025102105362](https://openairdocs.org/sdr/DXTA2025102105362), Oct 18, 2025: PCB. FAULTY. DURING DESCENT YELLOW CAS MESSAGE, "ELEC EMER L," DISPLAYED. SEVERAL MINUTES LATER YELLOW CAS MESSAGE, "BATTERY DISCHARGE L," ALSO DISPLAYED. FOLLOWED QRH PROCE
- [SDR DXTR2025072901](https://openairdocs.org/sdr/DXTR2025072901), Jul 28, 2025: CAP SEAL. FRACTURED. WHILE ACCOMPLISHING LT MLG LUBRICATION TASK CARD AMM 12-20-10-612, AND WHILE LUBRICATING INBOARD END OF LT MLG ACTUATOR, FOUND THE END CAP ASSY P/N: 7441511-20 
- [SDR DXTA2025040903018](https://openairdocs.org/sdr/DXTA2025040903018), Apr 9, 2025: HANDLE. OUT OF ADJUST. WHEN CLOSING MAIN DOOR FROM INSIDE CABIN DOOR OPEN CAS AND AMBER DOOR OPEN LIGHT DOESN'T EXTINGUISH UNLESS DOOR HANDLE IS PUSHED DOWN. WHEN OPENING DOOR FROM IN
- [SDR DXTA2025031802737](https://openairdocs.org/sdr/DXTA2025031802737), Mar 17, 2025: BATTERY PACK. DEFECTIVE. EMERGENCY LIGHTING: EMERGENCY LIGHTS FAIL THE PREFLIGHT TEST. NO EMERGENCY LIGHTS WORK WITH SWITCH IN THE ARM POSITION. ALL LIGHTS WORK WITH THE SWITCH IN THE O
- [SDR DXTA2024092600659](https://openairdocs.org/sdr/DXTA2024092600659), Sep 24, 2024: DOOR. UNKNOWN. WHEN CLOSING MAIN CABIN DOOR, AMBER DOOR OPEN LIGHT AND CAS REMAIN ILLUMINATED. POWER CYCLE WORKED TO CLEAR MALFUNCTION, BUT REOCCURED 2 LEGS LATER. PERFORMED M
- [SDR DXTR2024062502](https://openairdocs.org/sdr/DXTR2024062502), Jun 25, 2024: STRUCTURE. CORRODED. LEFT THRUST REVERSER UPPER BUCKET, LOCATED ON O/B SIDE NEEDS PAINT TOUCH-UP. REPAIR OF PAINT & CORROSION PER AQRD EWO-5998 REV. IR. & AQRD 912781 REV. A. REPAIR
- [SDR DXTR20224062501](https://openairdocs.org/sdr/DXTR20224062501), Jun 25, 2024: FRAME. CORRODED. R/H T/R I/B FRAME BETWEEN BUCKETS NEEDS PAINT TOUCH-UP. REPAIR OF PAINT & CORROSSION PER AQRD EWO-5999 REV. IR. & AQRD 912781 REV. A. REPAIRED C/W ON 8130-3 UND
- [SDR DXTA2024021210872](https://openairdocs.org/sdr/DXTA2024021210872), Feb 11, 2024: GDU. FAULTED. DURING DECENT GSD FAIL 1,2 AND 3 DISPLAYED ALONE WITH MULTIPLE CORRESPONDING SYSTEM, FAILURE MESSAGES. AVIONICS INTEGRATION (IAC, NIC PROC, MAU, GEA, IAPS): DUR
- [SDR DXTA2023081793310](https://openairdocs.org/sdr/DXTA2023081793310), Aug 17, 2023: UNKNOWN. UNKNOWN. MAIN DOOR: MAIN CABIN DOOR HANDLE WILL NOT MOVE FROM THE OPEN POSITION. IT IS MECHANICALLY JAMMED. DOOR CANNOT BE LATCHED CLOSED. ARRIVED AT AIRCRAFT IN HANGAR 
- [SDR 2023F00066](https://openairdocs.org/sdr/2023F00066), Feb 23, 2023: ARM. GOUGED. COPILOTS RUDDER PEDAL ADJUSTMENT ARM GOUGED. ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ38345M1 DATED FEBRUARY 22, 2023; 700-0073 COPILOTS RUDDER PEDAL 
- [SDR DXTA2022102472710](https://openairdocs.org/sdr/DXTA2022102472710), Oct 23, 2022: WIRE HARNESS. DAMAGED. MAIN DOOR: "CABIN DOOR OPEN" ILLUMINATED INFLIGHT. LIGHT WAS INTERMITTENT IN TURBULENCE. REMOVED AND REPLACED CABIN THRESHOLD WIRING HARNESS PN: 8250171-1 NSN. 

## Service difficulty reports on N830QS not matched to an aircraft (12)

They name N830QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA2018052501003](https://openairdocs.org/sdr/DXTA2018052501003), May 25, 2018: SEAL. WORN. PRESSURIZATION FAILURE AT FL410. SOUND OF AN AIR LEAK. NOISE QUICKLY GOT LOUDER, BECAME WHISTLING FOLLOWED BY LOUDER WHISTLING AND AIRFLOW. CABIN RATE HELD MOME
- [SDR DXTA2017062506417](https://openairdocs.org/sdr/DXTA2017062506417), Jun 25, 2017: DOWNLOCK SWITCH. UNSERVICEABLE. AFTER TAKEOFF, TRIED TO RETRACT THE GEAR. ALL GEAR WOULD COME UP. AND LIGHTS EXTINGUISH. AFTER ABOUT 10 SECONDS THE GEAR UNSAFE AND GREEN NOSE GEAR LIGHT WOULD 
- [SDR DXTA2015012105967](https://openairdocs.org/sdr/DXTA2015012105967), Jan 22, 2015: UNKNOWN. ODOR. AFTER DEPARTURE WITH THROTTLES IN CLIMB DETENT, HAD STRONG ELECTRICAL BURNING ODOR THROUGHOUT CABIN. OVERHEAD FAN WAS OFF & FREON A/C WAS OFF. THERE WAS A LIGHT
- [SDR DXTA2014012305967](https://openairdocs.org/sdr/DXTA2014012305967), Jan 22, 2015: UNKNOWN. ODOR. AFTER DEPARTURE WITH THROTTLES IN CLIMB DETENT, HAD STRONG ELEC BURNING SMELL THROUGHOUT CABIN. OVERHEAD FAN WAS OFF & FREON A/C WAS OFF. THERE WAS A LIGHT HAZE
- [SDR CWQR20140614002](https://openairdocs.org/sdr/CWQR20140614002), Jun 14, 2014: DOOR SEAL. DEFECTIVE. PERFORMED EMER EXIT DOOR OPERATIONAL CHECK IAW FORM FC-000-52-100901, DATED 4/20/2014. EMER DOOR FAILED OPERATIONAL TEST. REPLACED EMER EXIT DOOR RAIN SEAL, OPE
- [SDR DXTA2013010705236](https://openairdocs.org/sdr/DXTA2013010705236), Dec 21, 2012: RETAINER. BENT. WHEN GEAR WAS RETRACTED, UNSAFE WARNING LIGHT REMAINED ILLUMINATED. HYD PRESSURE ANNUNCIATOR WAS ALSO ILLUMINATED. WHEN GEAR WAS EXTENDED, ALL INDICATIONS NORMA
- [SDR 2012FA0000188](https://openairdocs.org/sdr/2012FA0000188), Feb 1, 2012: INLET GUIDE VANE. DISCONNECTED. DURING A ROUTINE MX CHECK, FOUND THE INLET AIR GUIDE DISCONNECTED AND LOOSE IN THE UPPER TAILCONE AREA. THE APU AIR INLET GUIDE AND "FIRE PROTECTION" FLANGE WAS
- [SDR CWQR200909](https://openairdocs.org/sdr/CWQR200909), Nov 23, 2009: DUCT. CHAFED. DURING PHASE B INSP, WE FOUND SIGNS OF CHAFING ON A WIRE BUNDLE AS IT PASSES THROUGH A LIGHTENING HOLE LOCATED BELOW THE PWR J-BOX MOUNTED ON THE AFT SIDE OF TH
- [SDR DXTA2009110203840](https://openairdocs.org/sdr/DXTA2009110203840), Oct 31, 2009: WHEEL. DAMAGED. ON LANDING, STRUCK METAL OBJECT ON RUNWAY. NOSE TIRE FLAT AND DAMAGE TO NOSE WHEEL. EXTENSIVE REPAIRS TO NLG BOX AND RE-SKINNING OF BELLY PERFORMED.
- [SDR DXTA200803126](https://openairdocs.org/sdr/DXTA200803126), Jun 15, 2008: WIRE. SHORTED. WHILE TAXIING FOR DEPARTURE, POWER BRAKE CIRCUIT BREAKER POPPED FOLLOWED BY A "LO BRAKE PRESS/ANTISKID INOP" CAUTION LIGHT AND LOSS OF BRAKING PRESSURE. REPLACE
- [SDR DXTA200803110](https://openairdocs.org/sdr/DXTA200803110), Jun 11, 2008: POWERPACK. MALFUNCTIONED. "LO BRK PRESS AND ANTISKID INOP" ANNUNCIATOR ILLUMINATED IN FLIGHT. STOPPED AIRCRAFT WITH EMER BRAKE. REMOVED & REPLACED BRAKE POWER PACK ASSY. BLED SYS. LEAK &
- [SDR DXTA200803072](https://openairdocs.org/sdr/DXTA200803072), May 20, 2008: MOTOR. INOPERATIVE. LOW BRAKE PRESS ANNUNCIATOR ILLUMINATED UP ON REACHING HOLD LINE. GAINED ACCESS TO ANTI-SKID MOTOR. REMOVED AND REPLACED MOTOR. OPS CK GOOD IAW MM 32-42-06. REM

## 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

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