# N867QS: 2024 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: 700-0120
- Year built: 2024
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 23, 2024
- Certificate issued: August 14, 2025
- Expires: August 31, 2032
- Mode S code: ABEA47
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=867QS
- Page: https://openairdocs.org/aircraft/N867QS

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 N867QS.

## FAA accident and incident reports

None matched to N867QS.

## Service difficulty reports (7)

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 DXTA2026072108923](https://openairdocs.org/sdr/DXTA2026072108923), Jul 19, 2026: DOOR. DIRTY. AFTER LANDING IN DAL, WITH PASSENGERS ON BOARD, UNABLE TO OPEN MAIN CABIN DOOR. HANDLE WENT ABOUT 1/2 TRAVEL, & JAMMED. HANDLE WOULD NOT BUDGE, IN OR OUT. WITH 
- [SDR DXTA2026012906674](https://openairdocs.org/sdr/DXTA2026012906674), Jan 25, 2026: CONTROL HANDLE. FAULTED. UPON SELECTION OF LANDING GEAR HANDLE DOWN, GEAR DISAGREE LRN WAS DISPLAYED AND NONE OF THE LANDING GEAR EXTENDED. THE QRH WAS REFERENCED AND AFTER THE THIRD CY
- [SDR DXTA2026012606674](https://openairdocs.org/sdr/DXTA2026012606674), Jan 25, 2026: LANDING GEAR. MALFUNCTIONED. UPON SELECTION OF LANDING GEAR HANDLE DOWN, "GEAR DISAGREE LRN" WAS DISPLAYED AND NONE OF THE LANDING GEAR EXTENDED. THE QRH WAS REFERENCED AND AFTER THE THIRD 
- [SDR 2025FA0000830](https://openairdocs.org/sdr/2025FA0000830), Dec 16, 2025: BEAM. CORRODED. RT THRUST REVERSER OUTBOARD BEAM SHOWS SIGNS OF CORROSION.
- [SDR 2025FA0000829](https://openairdocs.org/sdr/2025FA0000829), Dec 16, 2025: THRUST REVERSER. CORRODED. RT THRUST REVERSER INBOARD BEAM SHOWS SIGNS OF CORROSION.
- [SDR 2025FA0000828](https://openairdocs.org/sdr/2025FA0000828), Dec 16, 2025: REVERSER HALF. CORRODED. LEFT THRUST REVERSER UPPER DOOR SHOWS SIGNS OF CORROSION.
- [SDR DXTA2025011401949](https://openairdocs.org/sdr/DXTA2025011401949), Jan 13, 2025: HANDLE. BINDING. MAIN DOOR HANDLE: MAIN DOOR HANDLE STICKS OUT APPROX 1/4" WHEN CLOSED. CORRECTIVE ACTION: PENETRANT AND LUBE ADDED TO HANDLE AND BEARINGS. OPS CHECK GOOD. IAW C

## Service difficulty reports on N867QS not matched to an aircraft (19)

They name N867QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA2014042905747](https://openairdocs.org/sdr/DXTA2014042905747), Apr 25, 2014: RADOME. DAMAGED. BIRD STRIKE ON RT SIDE OF ACFT AT NOSE. REMOVED AND REPLACED RADOME ASSEMBLY IAW MM 53-50-14. OPS CHECK GOOD.
- [SDR DXTA2012032604429](https://openairdocs.org/sdr/DXTA2012032604429), Mar 23, 2012: APU. ODOR. AFTER TAKEOFF, SHORTLY AFTER TURNING THE MAV'S ON AND THE APU COMPLETELY OFF THERE WAS A STRONG ODOR THAT SMELLED LIKE OIL. THERE WAS NO SMOKE. TURNED MAV'S TO 
- [SDR DXTA2012032249270](https://openairdocs.org/sdr/DXTA2012032249270), Mar 21, 2012: WATER SEPARATOR. ODOR. AFTER ENGINE START UP, A FAINT ODOR OF OIL FUMES WAS NOTICED IN THE COCKPIT. DURING TAXI, THE ODOR CONTINUED, BUT WAS ATTRIBUTED TO THE PROXIMITY OF OTHER JETS.
- [SDR DXTA2012032204927](https://openairdocs.org/sdr/DXTA2012032204927), Mar 21, 2012: WARNING LIGHT. ILLUMINATED. CRUISING AT FL390 "FADEC 2" LIGHT ILLUMINATED ON MWP FOLLOWED IMMEDIATELY BY A ROLL BACK TO FLIGHT IDLE OF NR 2 ENGINE. CREW COMPLETED CHECKLIST ITEMS. EIED 2 D
- [SDR DXTA2012020604863](https://openairdocs.org/sdr/DXTA2012020604863), Feb 3, 2012: DOWNLOCK SWITCH. MALFUNCTIONED. DURING APPROACH AFTER SELECTING GEAR DOWN, WITH A NORMAL 3 GREEN INDICATION, THE RT MAIN RED UNSAFE LIGHT BEGAN FLICKERING FAINTLY. REPLACED THE RT MLG DOWNLOCK
- [SDR DXTA2011111604792](https://openairdocs.org/sdr/DXTA2011111604792), Nov 15, 2011: SERVO. FAILED. ELECTRIC TRIM FAILED IN FLIGHT. NOTHING WAS INDICATED ON ANY OF THE SCREENS THAT THE TRIM WAS NOT WORKING. AUTOPILOT STILL WORKED NORMALLY. DURING APPROACH, WHE
- [SDR DXTA2011080104671](https://openairdocs.org/sdr/DXTA2011080104671), Jul 31, 2011: HOSE. LEAKING. RT SIDE BRAKES INOPERATIVE. BRAKE PEDAL GOES TO THE FLOOR WITH LITTLE RESISTANCE AND ONLY 200 LBS OF PRESSURE. WHEN THE BRAKE IS APPLIED INDEPENDENTLY, IT WILL 
- [SDR DXTA2011080104676](https://openairdocs.org/sdr/DXTA2011080104676), Jul 31, 2011: BRAKE. INOPERATIVE. CAPTAINS SIDE RT BRAKE IS INOPERATIVE. BRAKE PEDAL GOES TO THE FLOOR WITH LITTLE RESISTANCE AND ONLY 200 LBS OF PRESSURE. WHEN THE BRAKE IS APPLIED INDEPENDENTL
- [SDR DXTA2011030304486](https://openairdocs.org/sdr/DXTA2011030304486), Mar 2, 2011: BRAKE SYS. WEAK. LEFT PILOTS RIGHT BRAKE PEDAL SOFT AND SPONGY, ONLY PRODUCING 800-900 PSI. SERVICED AND BLED BRAKES, OPS CHECKED GOOD IAW MM 32-40-00.
- [SDR E81RJW304273](https://openairdocs.org/sdr/E81RJW304273), Feb 22, 2011: TRANSDUCER. FAILED. INVESTIGATED FLIGHT CREW REPORT OF REPEATED MACH TRIM AND ELEVATOR TRIM FAIL ANNUNCIATOR INDICATIONS DURING DESCENT. DURING TROUBLESHOOTING FOUND ELEVATOR TRIM 
- [SDR DXTA2010070204136](https://openairdocs.org/sdr/DXTA2010070204136), Jul 1, 2010: SWITCH. MALFUNCTIONED. ON DEPARTURE, SQUAT AND STALL IDENT MWS LIGHTS ILLUMINATED AND ACFT DID NOT PRESSURIZE. INSTALLED NEW WEIGHT ON WHEELS SWITCH, LT MLG IAW MM CHAPTER 32-10-12. P
- [SDR DXTA200802838](https://openairdocs.org/sdr/DXTA200802838), Feb 4, 2008: EEC. MALFUNCTIONED. WHEN APPLYING TAKEOFF POWER LT ENGINE LAGS BEHIND R BY APPROX 15-20 PERCENT. REMOVED AND REPLACED LT DEEC WITH AN INSPECTED DEEC AND OPERATIONAL CHECKED OK IAW 
- [SDR DXTA200702643](https://openairdocs.org/sdr/DXTA200702643), Dec 2, 2007: SQUAT SWITCH. MALFUNCTIONED. AFTER T/O, LANDING GEAR WOULD NOT RETRACT, SQUAT AND STALL IDENT WARNING LIGHTS CAME ON. REPLACED LT & RT MLG WOW SWITCH . ROUTED WIRE TO TERMINAL BLOCKS "JK" A
- [SDR DXTA200601406](https://openairdocs.org/sdr/DXTA200601406), May 25, 2006: APU. OVERSERVICED. AFTER TAKEOFF, DURING FIRST 15 MIN'S OF FLIGHT, AND DURING LAST 10 TO 15 MIN'S OF FLIGHT, STRONG ACRIDLY SWEET, BURNED SMELL FILLED CABIN. ALL PAX /CREW SMELLED
- [SDR DXTA200500853](https://openairdocs.org/sdr/DXTA200500853), Jul 22, 2005: WARNING LIGHT. ILLUMINATED. DURING CLIMB-OUT, A LOUDER THAN NORMAL WIND NOISE WAS HEARD ON THE RIGHT SIDE OF THE COCKPIT. THE CABIN ALTITUDE CLIMBED AS HIGH AS 11500'. THE CABIN ALT LIGHT 
- [SDR DXTA200500750](https://openairdocs.org/sdr/DXTA200500750), Jun 2, 2005: PUMP. INOPERATIVE. NR 2 ENGINE FUEL ANNUNCIATOR ILLUMINATED AT 40 KNOTS ON T/O STATIC POWER, ARMED APR AT BRAKE RELEASED, T/O ABORTED. REMOVED INOP FUEL PUMP & INSTALLED AN OVERHA
- [SDR DXTA200500749](https://openairdocs.org/sdr/DXTA200500749), Jun 1, 2005: FUEL FILTER. CONTAMINATED. ON T/O RT ENGINE FUEL ANNUNICATOR ILLUMINATED. REMOVED RT ENGINE FUEL FILTER ELEMENT, P/N NR 897513-1 AND FILTER HOUSING O-RING P/N NR M25988/1-134 AND INSTALLE
- [SDR DXTA200500710](https://openairdocs.org/sdr/DXTA200500710), May 6, 2005: BULB. BURNED OUT. 2 EMERGENCY EXIT LIGHTS ABOVE DOOR AND ONE LOCATED AT THE ENTRANCE NOT ILLUMINATED DURING EMERGENCY LIGHT SYSTEM TEST. REPLACED 2 EACH BULBS IAW RAC DWG 149-349
- [SDR DXTA200500643](https://openairdocs.org/sdr/DXTA200500643), Mar 26, 2005: WARNING LIGHT. ILLUMINATED. DURING T/O ROLL AT 80 KTS ENG 2 FUEL ANNUNCIATORS ILLUMINATED. T/O ABORTED, ANNUNCIATOR EXTINGUISHED WHEN POWER REDUCED, THEN RE-ILLUMINATED AFTER RUNNING NR 2 

## 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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