# N832QS: 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: 700-0076
- Year built: 2022
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 26, 2022
- Certificate issued: April 29, 2026
- Expires: April 30, 2033
- Mode S code: AB6137
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=832QS
- Page: https://openairdocs.org/aircraft/N832QS

From the FAA registry file of October 27, 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 N832QS.

## FAA accident and incident reports

None matched to N832QS.

## Service difficulty reports (8)

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 DXTA2026021906921](https://openairdocs.org/sdr/DXTA2026021906921), Feb 16, 2026: SQUAT SWITCH. FAULTED. GEAR DOOR OPEN CAS MESSAGE CAME ON NOSE LANDING GEAR WAS RATCHETTING IT FELT LIKE WHEN GEAR WAS SELECTED UP. REMOVED NLG SQUAT SWITCH.P/N: 6948001-2 NSN AND INS
- [SDR DXTA2025042903223](https://openairdocs.org/sdr/DXTA2025042903223), Apr 25, 2025: FLAP SYSTEM. FAULTED. FLAPS FAILED INFLIGHT IN THE FULL POSITION. RESET LIGHT EXTINGUISHED WHEN HANDLE MATCHED WITH POSITION PER CHECKLIST, BUT CAS MSG AND RESET LIGHT REDISPLAYED AF
- [SDR DXTA2024030711120](https://openairdocs.org/sdr/DXTA2024030711120), Mar 5, 2024: STRIKER. OUT OF ADJUST. WHEN CLOSING THE MAIN CABIN DOOR, THE HANDLE HITS SOMETHING INTERNALLY APPROXIMATELY HALF WAY THROUGH THE CLOSING MOTION, AND IS UNABLE TO ADVANCE FURTHER WITHO
- [SDR DXTA2024010210487](https://openairdocs.org/sdr/DXTA2024010210487), Jan 1, 2024: BATTERY. FAILED. EMERGENCY LIGHTS DO NOT ILLUMINATE WHEN PLACED IN THE ON POSITION. THE EMER LIGHTS DO ILLUMINATE WHEN PLACED IN THE ARMED POSITION. AS PER THE MAINTENANCE CONTR
- [SDR DXTA2023121410335](https://openairdocs.org/sdr/DXTA2023121410335), Dec 14, 2023: BATTERY. FAULTED. EMERGENCY LIGHTING: WITH THE EMER LIGHTS SWITCH SELECTED TO ARM, NO EMER LIGHTS ILLUMINATE. WHEN THE EMER SWITCH IS SELECTED TO ON, THE OVERHEAD LIGHT ABOVE SEA
- [SDR DXTA2023121310325](https://openairdocs.org/sdr/DXTA2023121310325), Dec 13, 2023: UNKNOWN. UNKNOWN. WITH THE EMER LIGHTS SELECTED TO ON OR ARM WITH THE MAIN BATTERIES OFF, ALL EMERGENCY LIGHTING IS INOPERATIVE. ARRIVED AT A/C HOOK UP BATTERIES. CONFIRMED FAULT
- [SDR DXTA2023120710250](https://openairdocs.org/sdr/DXTA2023120710250), Dec 6, 2023: UNKNOWN. UNKNOWN. WITH THE SHIP BATTERYS IN THE OFF POSITION AND THE EMER LIGHTS IN THE ARMED POSITION, THE EMER LIGHTS DO NOT COME ON. WITH THE SHIPS BATTERY'S IN THE ON POSITIO
- [SDR DXTA2023020679930](https://openairdocs.org/sdr/DXTA2023020679930), Feb 4, 2023: NOT REPORTED. NOT REPORTED. MAIN DOOR: HAD VERY HARD TIME CLOSING DOOR IN ASPEN. TOP STEP DOESN'T SEEM TO BE IN PLACE WHEN OPEN. // SIGNOFF// THE TECH INSPECT THE DOOR AND FOUND THE CABIN 

## Service difficulty reports on N832QS not matched to an aircraft (13)

They name N832QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA2016110706329](https://openairdocs.org/sdr/DXTA2016110706329), Nov 7, 2016: DUCT. BLOWN. LOUD BANG AND THE CABIN ALTITUDE STARTED TO CLIMB COULD NOT CONTROL PRESSURIZATION. EXECUTED EMERGENCY DESCENT AND PROCEDURES. CABIN OXYGEN MASKS WERE DEPLOYED.
- [SDR DXTA2013061805418](https://openairdocs.org/sdr/DXTA2013061805418), Jun 17, 2013: BRAKE ASSY. OUT OF ADJUST. BRAKES ARE STICKING AFTER PARKING BRAKE IS RELEASED. POWER LEVERS HAVE TO BE ADVANCED HALFWAY TO GET THEM TO RELEASE. ADJUSTED THE PARKING BRAKE IAW MM 32-40-51
- [SDR DXTA2012110805175](https://openairdocs.org/sdr/DXTA2012110805175), Nov 7, 2012: MASTER CYLINDER. MALFUNCTIONED. COPILOTS LT AND RT BRAKE PEDALS ALL THE WAY TO THE FLOOR ONLY GET A FEW HUNDRED LBS OF PSI SHOWING. CAPTAINS BRAKES ARE VERY TOUCHY. SERVICED AND BLED BOTH CO-P
- [SDR E81R201112222202](https://openairdocs.org/sdr/E81R201112222202), Dec 22, 2011: CIRCUIT BOARD. DAMAGED. INVESTIGATED PILOT REPORT OF BOTH MWS ANNUNCIATORS NOT ILLUMINATING AND FLASHING DURING PRE-FLIGHT TESTS OF ENG NR 1 AND ENGINE NR 2 ENGINE FIRE WARNING SYS TES
- [SDR DXTA2011112804797](https://openairdocs.org/sdr/DXTA2011112804797), Nov 24, 2011: PUMP. MALFUNCTIONED. DEPARTING AND CLIMBING PAST 12,000 FT, THE RT ENGINE OIL PRESSURE WENT ABOVE 46 PSI AND CONTINUED INCREASING. REDUCING ENGINE POWER DID NOT REDUCE PRESSURE INDI
- [SDR E81RJT230776](https://openairdocs.org/sdr/E81RJT230776), Jul 15, 2011: WIRE. MISINSTALLED. DURING INVESTIGATION OF ELECTRIC ELEVATOR TRIM SYS, OPERATION NOTED TRIM RATE AS CONTROLLED BY THE PEDESTAL FLAP LEVER BAULK SWITCH BM TO OPERATE IN REVERSE. EL
- [SDR DXTA2011071104654](https://openairdocs.org/sdr/DXTA2011071104654), Jul 11, 2011: WHEEL. WORN. ON TAKEOFF, FELT VIBRATION IN YOKE AND AIRFRAME ABOVE 100KTS. CONTINUED TILL ABOUT 2 SECONDS AFTER GEAR SELECTED UP. UPON LANDING, FELT VIBRATION AT TOUCHDOWN A
- [SDR DXTA2010121904366](https://openairdocs.org/sdr/DXTA2010121904366), Dec 16, 2010: TRANSDUCER. INTERMITTENT. "ENGINE 1 COMPUTER" ANNUNCIATOR CAME ON DURING CRUISE AT FL360. NOTICED REDUCED N1AND N2 SPEEDS (APPRX. 7 PERCENT LESS THAN ENG 2.) PERFORMED CHECKLIST AND PLAC
- [SDR DXTA2010031604035](https://openairdocs.org/sdr/DXTA2010031604035), Mar 15, 2010: LANDING GEAR. MALFUNCTIONED. ON APPROACH, GEAR SELECTED DOWN, THE NLG DID NOT EXTEND. HAD A RED NLG INDICATION & NO NOSE GEAR PIN WITH 2 GREEN MLG INDICATIONS. EXERCISED A GO AROUND TO WORK
- [SDR DXTA2009111603862](https://openairdocs.org/sdr/DXTA2009111603862), Nov 13, 2009: DOWNLOCK SWITCH. DEFECTIVE. ON DESCENT THROUGH APPROX 8,000 FT, GEAR WARNING HORN SOUNDED. GEAR LIGHT SHOWED L GEAR (RED), N GEAR (RED), R GEAR (RED) AND GREEN. THIS OCCURED DURING APU STA
- [SDR DXTA2009080503751](https://openairdocs.org/sdr/DXTA2009080503751), Aug 4, 2009: TERMINAL. LOOSE. GEAR SELECTED DOWN & NO GREEN GEAR INDICATIONS APPEARED. ANNUNCIATOR TEST BUTTON PUSHED TO CONFIRM RED & GREEN GEAR BULBS WERE OPERATIONAL. RECYCLED GEAR UP & D
- [SDR DXTA2009032703566](https://openairdocs.org/sdr/DXTA2009032703566), Mar 26, 2009: LINE. LEAKING. AFTER LANDING, (REVERSER) LIGHT ON, (FLAP FAULT) LIGHT ON AND HYD PRESSURE AT 2200 PSI. ON POST FLIGHT DISCOVERED LT TR DEPLOYED AND LT/REAR FUSELAGE COVERED IN
- [SDR DXTA200702604](https://openairdocs.org/sdr/DXTA200702604), Nov 11, 2007: BRAKE. DRAGGING. AFTER LANDING, AIRCRAFT BRAKES WERE APPLIED AT SLOW SPEED, AIRCRAFT VEERED LEFT DUE TO LEFT BRAKE GRABBING AND NOT RELEASING. LEFT BRAKE RELEASED AFTER REPEATED

## 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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