# N836QS: 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: 700-0081
- Year built: 2022
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 3, 2022
- Certificate issued: November 18, 2025
- Expires: November 30, 2032
- Mode S code: AB7013
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=836QS
- Page: https://openairdocs.org/aircraft/N836QS

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 N836QS.

## FAA accident and incident reports

None matched to N836QS.

## Service difficulty reports (6)

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 DXTA2025062704019](https://openairdocs.org/sdr/DXTA2025062704019), Jun 23, 2025: TRANSDUCER. FAULTED. HYDRAULIC INDICATING (DPI): HYD B OVERTEMP CAS MESSAGE ON CLIMB OUT. HYD SYNOPTIC HAD AMBER DASHES INSTEAD OF THE TEMP READOUT. REMOVED AND REPLACED HYD SYSTEM 
- [SDR DXTA2025041703123](https://openairdocs.org/sdr/DXTA2025041703123), Apr 16, 2025: HANDLE. DIRTY. MAIN DOOR HANDLE: PLEASE EVALUATE MAIN CABIN DOOR. OPENING HAS BECOME DIFFICULT. LAST TIME CLOSING THE DOOR TOOK MULTIPLE ATTEMPTS AND RESETS USING THE CHECKLIS
- [SDR 2024FA0000971](https://openairdocs.org/sdr/2024FA0000971), Dec 18, 2024: ANTENNA. ERODED. VHF COMM. ANTENNA LEADING EDGE EROSION.
- [SDR 2024FA0000970](https://openairdocs.org/sdr/2024FA0000970), Dec 18, 2024: THRUST REVERSER. CORRODED. R/H THRUST REVERSER I/B AND O/B INNER EXHAUST BEAMS HAS CORROSION.
- [SDR 2024FA0000969](https://openairdocs.org/sdr/2024FA0000969), Dec 18, 2024: THRUST REVERSER. CORRODED. L/H THRUST REVERSER I/B AND O/B INNER EXHAUST BEAMS HAS CORROSION.
- [SDR DXTA2024030111056](https://openairdocs.org/sdr/DXTA2024030111056), Feb 29, 2024: BATTERY. FAILED. EMERGENCY LIGHTS BATTERY IS DEAD. DID BATTERY CHARGE PROCEDURE TWICE. BATTERY WOULD MOT LAST 3 MINUTES. C/W TASK, REMOVED #1 L/H EMERGENCY BATTERY PACK PN: CBS2

## Service difficulty reports on N836QS not matched to an aircraft (12)

They name N836QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA2011020804457](https://openairdocs.org/sdr/DXTA2011020804457), Feb 7, 2011: UPLOCK SWITCH. OUT OF RIG. DEPARTING, HAD A RT MAIN GEAR RED UNSAFE LIGHT WHEN LANDING WAS RETRACTED. TROUBLESHOT SYS AND DETERMINED THE RT MLG UNLOCK SWITCH WAS UNSAFE. WHILE DOING OPS C
- [SDR DXTA2011012504432](https://openairdocs.org/sdr/DXTA2011012504432), Jan 24, 2011: UPLOCK SWITCH. MALFUNCTIONED. UPON GEAR RETRACTION AFTER TAKEOFF, RT MLG RED UNSAFE LIGHT REMAINED ILLUMINATED. AFTER COMPLETING EMERGENCY CHECKLIST, LANDING GEAR WAS LOWERED WITH 3 GREEN AN
- [SDR DXTA2011011804418](https://openairdocs.org/sdr/DXTA2011011804418), Jan 17, 2011: WARNING LIGHT. FALSE ACTIVATION. RED GEAR LIGHT REMAINED ON ONCE GEAR WAS RETRACTED AFTER DEPARTURE. SWUNG GEAR AND CHECKED INDICATIONS WITH NO DEFECTS NOTED. CHECKED, CLEANED AND LUBRICATED RT
- [SDR DXTA2010121304363](https://openairdocs.org/sdr/DXTA2010121304363), Dec 12, 2010: DOWNLOCK SWITCH. DIRTY. RIGHT MLG RED UNSAFE LIGHT ON AFTER INITIALLY RETRACTING THE GEAR. INSPECTED, CLEANED AND LUBED RT NORMAL & STANDBY DOWNLOCK SWITCHES, JACKED ACFT AND CYCLED GE
- [SDR DXTA2009102903833](https://openairdocs.org/sdr/DXTA2009102903833), Oct 28, 2009: WARNING LIGHT. FALSE INDICATION. AFTER TAKE OFF FROM SLUSHY, SNOW COVERED AIRPORT, RETRACTED GEAR, RIGHT RED GEAR LIGHT REMAINED ON. CYCLED GEAR WITH SAME RESULT. GEAR EXTENDED NORMALLY FOR LAN
- [SDR DXTA2009101903816](https://openairdocs.org/sdr/DXTA2009101903816), Oct 18, 2009: BULB. BURNED OUT. UPON POSTFLIGHT CREW DISCOVERED STRONG ACRID ELECTRICAL ODOR IN LAVATORY AREA. FLOURSECENT LAVATORY DOWNLIGHT WAS FLICKERING ON ANF OFF. FOUND LAV FLUORESCENT B
- [SDR DXTA20082921](https://openairdocs.org/sdr/DXTA20082921), Mar 8, 2008: POTENTIOMETER. OUT OF TOLERANCE. WHILE ENROUTE FD WAS PITCHING UP AND DOWN CAUSING PLANE TO PORPISE. ALTITUDE VARIED BY AS MUCH AS +-150 FEET. TROUBLESHOT PROBLEM TO FLAP/FLIGHT DIRECTOR BIASIN
- [SDR DXTA200702619](https://openairdocs.org/sdr/DXTA200702619), Nov 19, 2007: CONNECTOR. DAMAGED. DURING CRUISE AT F300, AIRCRAFT PITCHED UP ABOUT 15 DEGREES AND AUTOPILOT KICKED OFF. RESEATED PIN (C) OF CONNECTOR GND 28 SYSTEM GROUND CHECKS GOOD IAW DWG NR 
- [SDR DXTA200701878](https://openairdocs.org/sdr/DXTA200701878), Jan 25, 2007: FLAP SYSTEM. MALFUNCTIONED. WHEN FLAPS SET AT 15 DEG AIRPLANE BANKS RT AT 5000FT AT 190KTS. RAN AND OPERATED FLAPS WITH PROTRACTOR. HOOKED UP TO BOTH FLAP'S. BOTH FLAPS WITHIN .1 DEGREE DU
- [SDR DXTA200601771](https://openairdocs.org/sdr/DXTA200601771), Nov 30, 2006: FLAP SYSTEM. MALFUNCTIONED. WHEN FLAPS 15 DEGREES WERE SELECTED FOR LANDING (A/S 190 KTS) THE FLAPS ONLY EXTENDED 3 TO 4 DEGREES. (STALL INDENT) LIGHT ILLUMINATED HYD PSI NORMAL, ALL OTHER
- [SDR DXTA200500682](https://openairdocs.org/sdr/DXTA200500682), Apr 15, 2005: PRESSURE SWITCH. FAILED. NR 1 (LEFT) FUEL LIGHT CAME ON DURING T/O ACCELERATION AT ABOUT 92-95 PERCENT N1, ABORT SPEED WAS BETWEEN 70-80 KTS. TROUBLESHOT SYSTEM. VERIFIED FLIGHT SQK. SW
- [SDR DXTA200400326](https://openairdocs.org/sdr/DXTA200400326), Jun 23, 2004: FUEL FILTER. MALFUNCTIONED. DURING TAKEOFF ROLL BOTH ENGINE FUEL ANNUNCIATOR LIGHTS ILLUMINATED, ABORTED TAKEOFF. DRAINED FUEL TANKS AND CHECKED FOR CONTAMINATION, NONE FOUND. REMOVED AND 

## 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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