# N815QS: 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: 700-0050
- Year built: 2021
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 28, 2021
- Certificate issued: July 29, 2023
- Expires: July 31, 2030
- Mode S code: AB1D5E
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=815QS
- Page: https://openairdocs.org/aircraft/N815QS

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 N815QS.

## FAA accident and incident reports

None matched to N815QS.

## 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 DXTA2026050607946](https://openairdocs.org/sdr/DXTA2026050607946), May 4, 2026: WIRE HARNESS. UNSECURE. EMERGENCY EXIT LIGHT MOUNTED ON LEFT GALLEY/PASSENGER BULKHEAD IS NOT ILLUMINATED WITH THE EMERGENCY LIGHTS SWITCH IN EITHER THE ON OR ARMED POSITION. REMOVED T
- [SDR DXTA2026032407354](https://openairdocs.org/sdr/DXTA2026032407354), Mar 21, 2026: GPS. FAULTED. AT 45,000 FEET WE LOST GPS 2 FOR ABOUT 10 MIN. AFTER ABOUT 10 MIN WE LOST GPS 1 AND HAD CASCADING FAILURES. WE LOST THE SHAKER, PUSHER, AUTO PILOT FAILURE, AUTO
- [SDR DXTA2026030407101](https://openairdocs.org/sdr/DXTA2026030407101), Mar 3, 2026: WIRE SPLICE. DAMAGED. WHILE CLOSING THE MAIN CABIN DOOR, THE HANDLE MOVES FREELY DOESN'T FEEL LIKE THE CAMS ARE ENGAGING. THE HANDLE ALSO WILL MOVE TO THE OPEN POSITION WITHOUT PRESS
- [SDR 2026FA0000147](https://openairdocs.org/sdr/2026FA0000147), Feb 27, 2026: THRUST REVERSER. CORRODED. R/H ENGINE UPPER TR BUCKET, LOWER TR BUCKET, AND INBD TR SIDE BRACE HAS VISIBLE CORROSION. LEVEL 2 CORROSION FOUND. ACCOMPLISHED SAFRAN REPAIR SCHEME NO. 907-62
- [SDR 2026F00017](https://openairdocs.org/sdr/2026F00017), Feb 27, 2026: BRACE. CORRODED. LEFT ENGINE UPPER THRUST REVERSER BUCKET. LOWER THRUST REVERSER BUCKET, AND OTBD THRUST REVERSER SIDE BRACE HAD VISIBLE CORROSION. LEVEL 2 CORROSION FOUND. ACCO
- [SDR DXTA2026013006692](https://openairdocs.org/sdr/DXTA2026013006692), Jan 26, 2026: ANTENNA. DEFECTIVE. WHILE DESCENDING FROM 9000 TO 8000 THE GEAR WARNING HORN AND THE RED CAS LANDING GEAR AND RED MASTER WARNING FLASHED AND THE GEAR INDICATIONS WERE RED. THIS CON
- [SDR DXTA2026012106619](https://openairdocs.org/sdr/DXTA2026012106619), Jan 20, 2026: LIGHT SYS. MALFUNCTIONED. FORWARD CABIN EMERGENCY EXIT LIGHT NOT ILLUMINATING IN THE AUTO POSITION. PERFORMED EMERGENCY LIGHTING ADUSTMENT/TEST IAW MM 33-50-00. ALL EMERGENCY LIGHTS OPER
- [SDR DXTA2025112405789](https://openairdocs.org/sdr/DXTA2025112405789), Nov 21, 2025: MONITORING UNIT. UNSERVICEABLE. AFTER TAXING IN AND SHUTTING DOWN THE ENGINES, WITH THE APU ONLINE. WE COULD NOT OPEN THE MAIN CABIN DOOR. THE AIRCRAFT WAS NOT PRESSURIZED AND NO DOOR STATUS L
- [SDR DXTA2024082900370](https://openairdocs.org/sdr/DXTA2024082900370), Aug 28, 2024: SIGN. INOPERATIVE. EMERG EXIT SIGN/LIGHT: WITH EMER LTS SWITCH IN THE ARM POSITION AND THE PAX SAFETY SWITCH ON, THE EXIT SIGN LIGHT ON THE LEFT FORWARD CABIN BULKHEAD DOES NOT IL
- [SDR DXTA2024070812287](https://openairdocs.org/sdr/DXTA2024070812287), Jul 7, 2024: BATTERY PACK. NO TEST. EMERGENCY LIGHTS FAIL PREFLIGHT TEST. BATTERY WILL CHARGE AFTER ACCOMPLISHING QRH PROCEDURE BUT IS DEAD THE NEXT DAY AFTER AIRCRAFT IS PARKED OVERNIGHT. DUE TO 
- [SDR DXTA2024030711123](https://openairdocs.org/sdr/DXTA2024030711123), Mar 5, 2024: STRIKER. OUT OF RIG. MAIN ENTRY DOOR HANDLE IS DIFFICULT TO MOVE INTO THE DOOR CLOSED POSITION FROM INSIDE THE CABIN. OPERATIONAL CHECK WAS NOT SATISFACTORY THE TECH INSPECT THE DOO

## Service difficulty reports on N815QS not matched to an aircraft (13)

They name N815QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA2014041605732](https://openairdocs.org/sdr/DXTA2014041605732), Apr 15, 2014: DEEC. MALFUNCTIONED. DURING INITIAL CLIMB, CREW FELT LATERAL YAW, NOTICED RT N1 SURGING 3 OR 4 PERCENT. DIMINISHED AT MID POWER SETTING BUT STILL SLIGHTLY NOTICEABLE. CREW DECLARED 
- [SDR DXTA2013053105405](https://openairdocs.org/sdr/DXTA2013053105405), May 30, 2013: AILERON SYS. LACK OF LUBE. DURING GROUND FLIGHT CONTROL CHECK, AIRLERON MOVEMENT APPEARED STIFF BETWEEN MID TO FULL TRAVEL. INFLIGHT, THE STIFFNESS INCREASED SPECIFICALLY WHEN ROLLING TO 
- [SDR DXTA2012120705202](https://openairdocs.org/sdr/DXTA2012120705202), Dec 6, 2012: RESERVOIR. UNDERSERVICED. ACFT NORMAL BRAKING SYSTEM INOPERATIVE. DURING TAXI OUT BRAKES WERE VERY MUSHY AND HAD MINUMAL PRESSURE. WITH EITHER THE CAPT BRAKES APPLIED OR THE CO-PILOTS BR
- [SDR DXTA2011112804799](https://openairdocs.org/sdr/DXTA2011112804799), Nov 25, 2011: UPLOCK SWITCH. OUT OF ADJUST. REPEAT WRITE UP. DURING DESCENT AT APPROX 310 KTS, NOTICED LT GEAR RED UNSAFE LIGHT ILLUMINATED, SLOWED TO 220 KTS AND LIGHT EXTINGUISHED. APPROX 5 MINUTES LATE
- [SDR DXTA2008110303331](https://openairdocs.org/sdr/DXTA2008110303331), Oct 31, 2008: UPLOCK SWITCH. OUT OF ADJUST. RIGHT GEAR RED LIGHT CAME ON IN FLIGHT. AT SPEEDS ABOVE 240 KTS CAME ON. BELOW 240 KTS LIGHT WENT OUT. COMING IN TO LAND WHEN WE PUT FLAPS AT 15 DEG LIGHT CAME 
- [SDR DXTA200802760](https://openairdocs.org/sdr/DXTA200802760), Jan 10, 2008: UNKNOWN. FUMES. AIRCRAFT INTERIOR HAS A TOXIC FUME ODOR TO IT, CAUSING BREATHING DISCOMFORT AND EYE IRRITATION. CLEANED AIRCRAFT CARPET. VENTILATED AIRCRAFT. NO TOXIC FUME ODOR
- [SDR DXT2007F00001](https://openairdocs.org/sdr/DXT2007F00001), Sep 29, 2007: ENGINE. POWER LOSS. DURING TAKEOFF ROLL AT APPROXIMATELY V1 OF 111KIAS, THE NR 2 COMPUTER FAILED (STEADY LIGHT) IT WAS ACCOMPANIED BY A ROLL BACK OF THE NR 2 ENGINE AND A SUBSEQUEN
- [SDR DXTA200702510](https://openairdocs.org/sdr/DXTA200702510), Sep 29, 2007: COMPUTER. MALFUNCTIONED. DURING TAKEOFF ROLL AT APPROXIMATELY V1 OF 111KIAS, THE NR2 COMPUTER FAILED (STEADY LIGHT) IT WAS ACCOMPANIED BY A ROLL BACK OF THE NR2 ENGINE AND A SUBSEQUENT 
- [SDR DXTA200702244](https://openairdocs.org/sdr/DXTA200702244), Jun 6, 2007: CLAMP. LEAKING. APPROX 5 MIN AFTER TAKEOFF, REAR BAY OVERHEAT LIGHT CAME ON. [06-15-07] RAN AIRCRAFT AT POWER AND FOUND NR 1 MAV LEAKING AT BOTH CLAMPS. O/B CLAMP WAS LEAKING D
- [SDR DXTA200702069](https://openairdocs.org/sdr/DXTA200702069), Apr 2, 2007: SWITCH. OUT OF ADJUST. AT 40 KTS ON T/O AILERON/ELEVATOR TRIM LIGHT ILLUMINATED, REJECTED T/O, ELEVATOR TRIM WAS SET FOR PROPER TRIM SETTING AT 21.5 ADJUSTED LT AND RT ELEVATOR OUT OF
- [SDR DXTA200601671](https://openairdocs.org/sdr/DXTA200601671), Oct 19, 2006: ENGINE. BIRD INGESTION. ON TAKEOFF ABOUT 20 SECONDS AFTER MAVS SELECTED OPEN (700 MSL) A CHEMICAL ODOR FOLLOWED BY A BURNING OF THE EYES AT 1500 MSL. THE MAV'S WERE SELECTED CLOSED AND
- [SDR DXTA200601667](https://openairdocs.org/sdr/DXTA200601667), Oct 17, 2006: UNKNOWN. ODOR. AFTER TAKEOFF AND SWITCHING ON MAIN AIR VALVES, NOTICED A BURNING ODOR AND SMOKE. BOTH SEEMED TO FOLLOW THROTTLE MOVEMENT, HIGH POWER = MORE ODOR, LOW POWER = L
- [SDR DXTA200501104](https://openairdocs.org/sdr/DXTA200501104), Nov 23, 2005: INTAKE DUCT. CONTAMINATED. COCKPIT AND CABIN FILLED WITH SMOKE UPON ROTATION AT TAKEOFF. INSPECTED ACFT TO INCLUDE BOTH ENGS, ALL GEAR WELLS, INSIDE RADOME -HELL HOLE- COCKPIT & CABIN WIT

## 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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