# N838QS: 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: 700-0083
- Year built: 2022
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 15, 2022
- Certificate issued: January 23, 2026
- Expires: January 31, 2033
- Mode S code: AB7781
- Owner type: Co-owned
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=838QS
- Page: https://openairdocs.org/aircraft/N838QS

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 N838QS.

## FAA accident and incident reports

None matched to N838QS.

## Service difficulty reports (5)

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 DXTR2024070401](https://openairdocs.org/sdr/DXTR2024070401), Jul 4, 2024: THRUST REVERSER. CORRODED. RH TR INNER SURFACE LEVEL 1 CORROSION. ACCOMPLISHED MINOR REPAIR IAW AQRD RFTS-111168
- [SDR DXTR2024070400001](https://openairdocs.org/sdr/DXTR2024070400001), Jul 4, 2024: SKIN. CORRODED. RH & LH THRUST REVERSER BUCKET SKIN CONTAINS LEVEL 1 CORROSION. ACCOMPLISHED MINOR REPAIR IAW AQRD RFTS 111171.
- [SDR DXTA2024050611682](https://openairdocs.org/sdr/DXTA2024050611682), May 4, 2024: BATTERY. NO TEST. EMERGENCY LIGHTING WORKS IN THE ON MODE, BUT DOES NOT WORK IN THE ARMED MODE. ACCOMPLISHED CHECKLIST (25X )TWICE PER THE CHECKLIST. PROBLEM STILL EXISTED, CONTA
- [SDR DXTA2024041111466](https://openairdocs.org/sdr/DXTA2024041111466), Apr 10, 2024: SENSOR. FAULTED. AT APPROXIMATELY 1720Z IN CRUISE FLT AT FL430 DESCENDING TO FL370 IN MODERATE TURBULENCE, CONTROL LOCK ON WHITE CAS MESSAGE ILLUMINATED. FLT CONTROLS BECAME LOC
- [SDR DXTA2024020510795](https://openairdocs.org/sdr/DXTA2024020510795), Feb 2, 2024: BATTERY. FAILED. EMER LTS DON'T HOLD CHARGE. REMOVED DEFECTIVE AFT EMERGENCY LIGHT BATTERY PACKS LEFT AND RIGHT AND INSTALLED CUSTOMER SUPPLIED REPAIRED LEFT BATTERY PACK AND RI

## Service difficulty reports on N838QS not matched to an aircraft (13)

They name N838QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA200802949](https://openairdocs.org/sdr/DXTA200802949), Mar 18, 2008: ROD END. OUT OF ADJUST. DURING INTIAL CLIMB AT 17000 FT + 270 KIAS, MAX FWD ELEVATOR TRIM WAS REQUIRED. ADJUSTED ELEVATOR ROD ENDS OUT .5 TURN AND LUBRICATED TRIM JACKS. PERFORMED ELEV
- [SDR DXTA20082883](https://openairdocs.org/sdr/DXTA20082883), Feb 15, 2008: TRIM SYSTEM. OUT OF RIG. DURING CLIMB (APPROXIMATELY 16,000-18,000) TRIM SYS REACHED FWD NOSE DOWN POSITION AND PILOT WAS HOLDING FWD PRESSURE ON YOKE. RIGGED ELEVATOR TRIM JACKS AND EL
- [SDR DXTA200802789](https://openairdocs.org/sdr/DXTA200802789), Jan 22, 2008: SOLENOID VALVE. INOPERATIVE. NR 2 ENGINE COMPUTER ANNUNCIATOR LIGHT ON STEADY. REPLACED LT ENGINE SURGE VALVE SOLENOID "A" IAW TFE 731-5BR LMM CH 76-10-01. OPERATIONAL CHECK SATISFACTORY IA
- [SDR DXTA200702594](https://openairdocs.org/sdr/DXTA200702594), Nov 4, 2007: BRAKE ASSY. WEAK. BOTH PILOT AND COPILOT BRAKES ARE SPONGY. PEDALS TRAVEL HALF WAY BEFORE ANY BRAKING ACTION. PERFORMED OPS CHECK OF BRAKE SYSTEM. NO DISCREPANCIES NOTED IAW 32-4
- [SDR DXTA200702426](https://openairdocs.org/sdr/DXTA200702426), Jul 28, 2007: MASTER CYLINDER. UNDERSERVICED. MAIN BRAKES FEEL SOFT, MORE PRESSURE THAN NORMAL NEEDED TO STOP AIRCRAFT. CHECKED ALL BRAKE WEAR INDICATORS CHECKED GOOD. SERVICED MASTER CYLENDERS AND BLED BRA
- [SDR DXTA200702128](https://openairdocs.org/sdr/DXTA200702128), Apr 21, 2007: BRAKE. MALFUNCTIONED. BRAKES NEED ALMOST FULL PEDAL DEFLECTION FOR MAXIMUM BRAKING. NOT SURE IF MAX BRAKING WAS NEEDED IT WOULD BE AVAILABLE. [4-27-07] BLED ALL 4 BRAKE ASSEMBLIES OP
- [SDR DXTA200701927](https://openairdocs.org/sdr/DXTA200701927), Feb 9, 2007: COMPUTER. MALFUNCTIONED. AUTO PILOT PITCHED OVER FROM LEVEL FLIGHT AT FL360 AND MACH .78 OR 260 KTS IND. WE LOST 450 FT UPON THE VIOLENT PITCHING MOMENT AND VERY ABRUPT TAIL FLUTTER. TH
- [SDR DXTA200701881](https://openairdocs.org/sdr/DXTA200701881), Jan 26, 2007: WARNING SYSTEM. ACTIVATED. AT 300FT ON FINAL, GOT GPWS WARNING (TOO LOW GEAR, PULL UP). NOSE GEAR INDICATOR WENT BLANK. DID EMERG PROCEDURES INCLUDING PULLING GPWS AND HORN C/BS. DID LOW 
- [SDR DXTA200701861](https://openairdocs.org/sdr/DXTA200701861), Jan 17, 2007: UPLOCK SWITCH. OUT OF ADJUST. ON FINAL APPROACH AT ABOUT 1000 FT NOSE GEAR LIGHT WENT OUT. DESCENDING DOWN FOR A FLY BY WE GOT THE AUDIBLE WARNING "PULL UP NO GEAR". ON GO AROUND THE LIGHT C
- [SDR DXTA200601462](https://openairdocs.org/sdr/DXTA200601462), Jun 29, 2006: BRAKE. MALFUNCTIONED. CAPTAINS SIDE BRAKE PEDALS ARE VERY MUSHY. MUST PRESS PEDALS ALMOST FULLY TO GET BRAKE PRESSURE.
- [SDR DXTA200500723](https://openairdocs.org/sdr/DXTA200500723), May 13, 2005: LIGHT. INOPERATIVE. FLOOR LEVEL EMERGENCY LIGHT ACROSS FROM EMERGENCY EXIT INOP. REMOVED AND REPLACED FLOOR LEVEL EMERGENCY LIGHT IAW HAWKER 800XP AMMA 33-20-00, OPS CHECK GOOD.
- [SDR DXTA200500695](https://openairdocs.org/sdr/DXTA200500695), Apr 23, 2005: STRUT. UNDERSERVICED. RIGHT MAIN LANDING GEAR DID NOT FULLY RETRACT AFTER TAKEOFF, CONFIRMED BY FLY BY OF TOWER CONTROLLER. RE-SERVICED RIGHT MLG STRUT IAW HAWKER 800XP AMM 12-32-00,
- [SDR DXTA200400300](https://openairdocs.org/sdr/DXTA200400300), Apr 22, 2004: NUT. MISSING. ON PREFLIGHT DISCOVERED 10 NUTS MISSING ON THE LEFT INBOARD MAIN WHEEL, ONLY 2 NUTS HOLDING WHEEL TOGETHER. REMOVED AND REPLACED NR 1 AND NR 2 MLG WHEEL ASSEMBL

## 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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