# N814QS: 2021 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: 700-0049
- Year built: 2021
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 16, 2021
- Certificate issued: September 11, 2026
- Expires: September 30, 2033
- Mode S code: AB19A7
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=814QS
- Page: https://openairdocs.org/aircraft/N814QS

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 N814QS.

## FAA accident and incident reports

None matched to N814QS.

## Service difficulty reports (10)

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 DXTA2026080309062](https://openairdocs.org/sdr/DXTA2026080309062), Jul 30, 2026: PROXIMITY SWITCH. FAULTED. FLIGHT, KHYA-KFLL, ON ARRIVAL INTO KFLL AT FL190 WE RECEIVED A AMBER CABIN DOOR OPEN CAS MESSAGE. NO AUDIBLE SIGN OF A DOOR OPEN OR CRACKED OPEN, NO PRESSURIZAT
- [SDR DXTA2025052203580](https://openairdocs.org/sdr/DXTA2025052203580), May 21, 2025: CONTROL COLUMN. NOISE. WHEN MOVING CONTROL COLUMNS FORWARD AND AFT, THERE IS A VERY NOTICABLE SQUEAKING AND SUBTLE STIFFNESS/BINDING FEELING IN THE CONTROLS. ARRIVED AT A/C AND VERIFI
- [SDR DXTA2024112201237](https://openairdocs.org/sdr/DXTA2024112201237), Nov 17, 2024: LIGHT. MALFUNCTIONED. STARBOARD OVERWING EMERGENCY LIGHT IS INOP. POWERED UP AIRCRAFT AND TURNED ON EMERGENCY LIGHTS. ALL EMER LIGHTS ILLUMINATED. UNABLE TO DUPLICATE DISCREPANCY. TA
- [SDR DXTA2024112101185](https://openairdocs.org/sdr/DXTA2024112101185), Nov 17, 2024: LIGHT. INOPERATIVE. STARBOARD OVERWING EMERGENCY LIGHT IS INOP. POWER UP AIRCRAFT AND TURNED EMERGENCY LIGHTS ON . ALL EMERGENCY LIGHTS ILLUMINATED . UNABLE TO DUPLICATE DISCREPANC
- [SDR DXTA2024010810533](https://openairdocs.org/sdr/DXTA2024010810533), Jan 6, 2024: UNKNOWN. UNKNOWN. AMBER BRAKE 50% DEGRADED ON TAXI OUT. NO PSI ON OUTBOARD SYSTEM NORMAL BRAKING.
- [SDR DXTA2023121510344](https://openairdocs.org/sdr/DXTA2023121510344), Dec 14, 2023: CIRCUIT BOARD. DEFECTIVE. WHEN ATTEMPTING TO MOVE AIRCRAFT, FOUND MAIN CABIN DOOR WILL NOT CLOSE ELECTRICALLY. REMOVED FAULTY CED MONITOR PCB AND INSTALLED INSPECTED PCB IAW CE-700 AMM C
- [SDR 2023FA0000412](https://openairdocs.org/sdr/2023FA0000412), Aug 13, 2023: SCREEN. DEBONDED. PROTRUDING WIRE MESH AND PARTIAL DAMAGE TO THE FWD AND AFT EDGES OF THE ACOUSTING MESH ON INNER BARREL OF RH INLET ASSEMBLY. REPAIR WAS ACCOMPLISHED WITH GKN TE
- [SDR 2023FA0000411](https://openairdocs.org/sdr/2023FA0000411), Aug 11, 2023: THRUST REVERSER. CORRODED. ACCOMPLISHED SAFRAN REPAIR SCHEME NO. RS907-622 REVISION A, PROCEDURE TO REPAIR CORROSION DAMAGE AND RESTORING SURFACE PROTECTION ON THE BEAM INNER SKIN DATED 2
- [SDR DXTA2023062689340](https://openairdocs.org/sdr/DXTA2023062689340), Jun 26, 2023: UNKNOWN. UNKNOWN. CAPTAIN COCKPIT WINDOW: COCKPIT LEFT SIDE WINDOW CRACKED DURING APPOACH PASSING 12,000 FT. /REMOVED FAILED/CRACKED LH COCKPIT SIDE WINDOW 9914809-1 S/N 20024H09
- [SDR 2022FA0000465](https://openairdocs.org/sdr/2022FA0000465), Aug 21, 2022: WINGLET. DAMAGED. LEFT WING WING TIP: DURING PRE-FLIGHT INSPECTION, FOUND BURN MARK AND DAMAGE THAT LOOKS LIKE POSSIBLE LIGHTNING STRIKE DAMAGE ON UPPER LEFT WINGLET

## Service difficulty reports on N814QS not matched to an aircraft (18)

They name N814QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA2016072706273](https://openairdocs.org/sdr/DXTA2016072706273), Jul 27, 2016: ACTUATOR. UNSERVICEABLE. RIGHT MAIN GEAR INDICATOR DID NOT ACTUATE NORMALLY. RIGHT MAIN GEAR DOWN LIGHT WAS NOT ON. LANDING GEAR WILL NOT EXTEND CHECKLIST COMPLETED AND RIGHT MAIN GEAR 
- [SDR DXTA2016031906205](https://openairdocs.org/sdr/DXTA2016031906205), Mar 19, 2016: SEAL. LEAKING. RT ENG FIRE LIGHT ILLUMINATED IN FLT. DISCHARGED LT FIRE BOTTLE. FIRE LIGHT EXTINGUISHED. NO SIGN OF FIRE ON PREFLIGHT. CRASH & FIRE CREWS REPORTED NO HOT SPOTS
- [SDR DXTR2015040901](https://openairdocs.org/sdr/DXTR2015040901), Apr 2, 2015: SKIN. DAMAGED. ANOMALY FOUND AT BS 205 AND WL 94-96 SKIN JOINT DURING PHASE 49 INSPECTION WHICH APPEARS TO BE A SCRATCH APPROXIMATELY 2" IN LENGTH. COMPLIED WITH MFG ENGINEERI
- [SDR DXTA2014032405697](https://openairdocs.org/sdr/DXTA2014032405697), Mar 23, 2014: UNKNOWN. MALFUNCTIONED. ON LANDING ROLL BELOW 60 KNOTS, PILOTS RT BRAKE PEDAL WENT TO THE FLOOR. RIGHT PILOT GOT THE AIRPLANE SLOWED TO TAXI SPEED, THEN HIS RT PEDAL WAS INTERMITTENTLY
- [SDR DXTA2014013005632](https://openairdocs.org/sdr/DXTA2014013005632), Jan 29, 2014: SEAL. DAMAGED. RIGHT ENG FIRE LIGHT ON IN FLIGHT. PERFORMED ENG FIRE LIGHT ON MEMORY ITEMS LIGHT EXTINGUISHED AFTER APPROXIMATELY 3 SECONDS AFTER EFFECTED ENG THROTTLE WAS RED
- [SDR DXTA2013100705528](https://openairdocs.org/sdr/DXTA2013100705528), Oct 5, 2013: FIRE LOOP. MISROUTED. DURING CLIMB THRU FL230, RT ENGINE FIRE LIGHT AND WARNING BELL CAME ON. RETARDED RT THROTTLE TO IDLE IAW THE CHECKLIST AND BELL AND LIGHT EXTINGUISHED. FOUND LE
- [SDR DXTA2013091105498](https://openairdocs.org/sdr/DXTA2013091105498), Sep 10, 2013: SEAL. LEAKING. IN FLIGHT, RT ENGINE FIRE LIGHT AND WARNING BELL ACTIVATED. RETARDED THROTTLE TO IDLE AND BELL AND LIGHT EXTINGUISHED. LANDED WITH ENGINE IN IDLE, NO OTHER ABNO
- [SDR DXTA2013082605484](https://openairdocs.org/sdr/DXTA2013082605484), Aug 23, 2013: SEAL. LEAKING. AT 25,000 FT, RT ENGINE FIRE BELL AND LIGHT SOUNDED AND ILLUMINTED. PERFORMED ENGINE FIRE CHECK LIST DECLARED EMERGENCY AND LANDED WITHOUT FURTHER EVENT. INSPEC
- [SDR DXTA2010110504290](https://openairdocs.org/sdr/DXTA2010110504290), Nov 4, 2010: GPS. FAILED. RT CIRCUIT BREAKER PANEL "WARN" CIRCUIT BREAKER POPPED IN FLIGHT. FOUND GPS TO BE CAUSE OF PROBLEM. R & R GPS. OPS CHECKED GOOD AT THIS TIME. ALL WORK DONE IAW 
- [SDR DXTA200810123302](https://openairdocs.org/sdr/DXTA200810123302), Oct 12, 2008: FIRE DETECTOR. FALSE INDICATION. RT ENG FIRE LIGHT ILLUMINATED IN FLT, DISCHARGED FIRST BOTTLE, LIGHT EXTINGUISHED. LIGHT RE-ILLUMINATED & WOULD NOT EXTINGUISH AFTER SECOND BOTTLE DISCHARGED. A
- [SDR DXTA2008101303302](https://openairdocs.org/sdr/DXTA2008101303302), Oct 12, 2008: WARNING LIGHT. ILLUMINATED. RIGHT ENG FIRE LIGHT ILLUMINATED IN FLIGHT DISCHARGED FIRST BOTTLE, LIGHT EXTINGUISHED. LIGHT RE-ILLUMINATED AND WOULD NOT EXTINGUISH AFTER SECOND BOTTLE DISCHA
- [SDR DXTA200809193279](https://openairdocs.org/sdr/DXTA200809193279), Sep 19, 2008: TRIM SYSTEM. OUT OF LIMITS. AUTO PILOT KICKS OFF WHEN IN CLIMB OR TURN. ACFT CONTROLS APPEAR TO BE LOADED WHEN AUTOPILOT KICKS OFF. PERFORMED OPS CHECK OF AUTOPILOT DISENGAGEMENT SYS TO EN
- [SDR DXTA200803279](https://openairdocs.org/sdr/DXTA200803279), Sep 19, 2008: AUTOPILOT SYS. MALFUNCTIONED. AUTO PILOT KICKS OFF WHEN IN CLIMB OR TURN.
- [SDR DXTA200803069](https://openairdocs.org/sdr/DXTA200803069), May 19, 2008: PRESSURE SWITCH. INOPERATIVE. WHILE TAKING THE RUNWAY FOR DEPARTURE THE LOW BRAKE PRESSURE - ANTI-SKID ANNUNCIATOR LIGHT ILLUMINATED. REMOVED DEFECTIVE PUMP MOTOR PRESSURE SWITCH AND INSTALL
- [SDR DXTA20082939](https://openairdocs.org/sdr/DXTA20082939), Mar 14, 2008: PCB. INOPERATIVE. LANDING GEAR DID NOT EXTEND WHEN GEAR HANDLE WAS PUT DOWN. REPLACED PCB NZ014 PER CE560 ENCORE & MM 24-51-01, REPLACED LANDING GEAR CONTROL HANDLE ASSY. PER CE5
- [SDR DXTA20082912](https://openairdocs.org/sdr/DXTA20082912), Mar 3, 2008: INDICATOR. LOOSE. ELEVATOR TRIM POSITION INDICATOR INOP. INDICATES INCORRECT TRIM POSITION. FOUND TRIM LOOSE. SHIMMED & RESECURED INDICATOR IAW MM 27-31-00. OPERATIONAL AND TRAVE
- [SDR DXTA20082897](https://openairdocs.org/sdr/DXTA20082897), Feb 24, 2008: ANTI-SKID SYS. MALFUNCTIONED. ON TAXI OUT LOW BRAKE PRESS AND ANTI-SKID INOP LIGHT ILLUMINATED. NORMAL BRAKING WAS INEFFECTIVE. EMERGENCY BRAKE WAS USED TO STOP THE AC. GAINED ACCESS TO ANTI
- [SDR DXTA200802743](https://openairdocs.org/sdr/DXTA200802743), Jan 3, 2008: WARNING LIGHT. UNKNOWN. WHEN THE GEAR WAS CYCLED DOWN NORMALLY (GEAR HANDLE TO DOWN POSITION) THERE WAS NONE OF THE 3 GREEN DOWN INDICATORS. JACKED ACFT, CONNECTED HYDRAULIC MULE. EXTE

## 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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