# N986QS: 2025 Textron 680A

- Status: Valid registration
- Airframe: [Textron 680A](https://openairdocs.org/model/textron-680a) (registry code 2076814, 10 seats)
- Engine: [Pratt & Whitney Canada PW306D1](https://openairdocs.org/engine/pratt-whitney-canada-pw306d1) (registry code 51850)
- Data sheets: [TCDS T00012WI](https://openairdocs.org/tcds/T00012WI) (Textron Aviation Inc.), [TCDS E35NE](https://openairdocs.org/tcds/E35NE) (Pratt & Whitney Canada Corp.) (OpenAirDocs)
- Serial number: 680A0456
- Year built: 2025
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 25, 2025
- Certificate issued: December 24, 2025
- Expires: December 31, 2032
- Mode S code: ADC2DD
- Registered owners: [Bjs Wholesale Club Inc](https://openairdocs.org/faa-owner/BJS%20WHOLESALE%20CLUB%20INC), [Cox Financial Group Ltd](https://openairdocs.org/faa-owner/COX%20FINANCIAL%20GROUP%20LTD), [Sellars Craig](https://openairdocs.org/faa-owner/SELLARS%20CRAIG), [Stephan Damon](https://openairdocs.org/faa-owner/STEPHAN%20DAMON), [Family Entertainment Television Inc](https://openairdocs.org/faa-owner/FAMILY%20ENTERTAINMENT%20TELEVISION%20INC), [Mullen James](https://openairdocs.org/faa-owner/MULLEN%20JAMES)
- Location: [Oklahoma City, OK](https://openairdocs.org/faa-place/OK/Oklahoma%20City)
- Owner type: Co-owned, fractional ownership
- Owner's area on the map: 35.5467° N, 97.5646° W: Placed by OpenAirDocs at the center of ZIP code 73116, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=986QS
- Page: https://openairdocs.org/aircraft/N986QS

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): 3 in force

### Matched by airframe (Textron 680A)

- [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
- [AD 2018-07-13](https://openairdocs.org/ad/2018-07-13): Landing Gear · Textron 510, 680 and 680A. Effective May 15, 2018

### Matched by engine (Pratt & Whitney Canada PW306D1)

None in force.

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N986QS.

## FAA accident and incident reports

None matched to N986QS.

## Service difficulty reports (4)

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 DXTA2026100810074](https://openairdocs.org/sdr/DXTA2026100810074), Oct 6, 2026: HANDLE. BINDING. MED LATCHING HANDLE STICKS IN THE OPEN/UNLATCHED POSITION AND IS DIFFICULT TO MOVE TO THE DOWN AND LATCHED POSITION. CYCLED HANDLE WITH THE DOOR FULLY OPEN AND 
- [SDR DXTA2026092209784](https://openairdocs.org/sdr/DXTA2026092209784), Sep 18, 2026: PCB. DEFECTIVE. APPROXIMATELY 1.5 - 2 HOURS INTO FLIGHT AT FL450, WE RECEIVED THE AMBER CHECK DOORS AND CABIN DOOR OPEN MESSAGES IN CRUISE. WE COMPLIED WITH THE APPROPRIATE QRH
- [SDR DXTA2026033107456](https://openairdocs.org/sdr/DXTA2026033107456), Mar 29, 2026: POWER SUPPLY. DEFECTIVE. AFTER SHUT DOWN WITH THE BATTERIES DISCONNECTED AND THE EMERGENCY LIGHT SWITCH OFF, THE RIGHT OVERWING EMERGENCY LIGHT OUTSIDE. SEAT 3 EMERGENCY LIGHTING, AND M
- [SDR DXTA2026020906794](https://openairdocs.org/sdr/DXTA2026020906794), Feb 5, 2026: G SWITCH. FAULTED. EMER LIGHTS STAY ON WHEN SWITCH IS OFF. EXTERIOR WING INSPECTION LIGHTS, PATH LIGHTS BELOW SEAT 5 AND 8, LIGHT ABOVE SEAT 7, AND LIGHT AT EMERGENCY EXIT. CORREC

## Service difficulty reports on N986QS not matched to an aircraft (26)

They name N986QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA2016052006244](https://openairdocs.org/sdr/DXTA2016052006244), May 27, 2016: COALESCER BAG. ODOR. ON TAXI IN WE COULD SMELL SMOKE, TURNED PACS OFF. ON LATER TESTING IT SEEMS TO HAPPEN WHEN WE TURN THE COCKPIT PAC ON. RAN BOTH PACS WITH THE APU FOR ABOUT 3 HO
- [SDR DXTA2014082205863](https://openairdocs.org/sdr/DXTA2014082205863), Aug 21, 2014: COALESCER BAG. DIRTY. COCKPIT PAC AIR HAS DIRTY SOCK SMELL FROM WEMACS. R & R BOTH COCKPIT & CABIN COALESCE SOCKS. OPERATED PAC AIR, NO SMELL NOTED. OPERATION & LEAK CHECKS GOOD. ALL
- [SDR DXTA2014072105822](https://openairdocs.org/sdr/DXTA2014072105822), Jul 19, 2014: BRAKE ASSY. CONTAMINATED. WHEN THE BRAKES ARE COLD & FOR THE FIRST FLIGHT THEY SQUEAL LOUDLY WHEN APPLIED. AFTER A LANDING WHEN HOT THEY BECOME VERY GRABBY WHEN APPLIED. THEY ARE NOT PUL
- [SDR DXTA2013071505445](https://openairdocs.org/sdr/DXTA2013071505445), Jul 12, 2013: DOWNLOCK SWITCH. FAILED. DURING LANDING GEAR EXTENSION, NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE. GEAR WAS RECYCLED, NO HELP. THE TOWER SAID LOOKED LIKE GEAR WAS DOWN. AS EMERGENCY CHEC
- [SDR DXT2013F00000](https://openairdocs.org/sdr/DXT2013F00000), Jun 12, 2013: LANDING GEAR. VIBRATION. IN THE DECELERATION PHASE OF THE LANDING ROLLOUT, EXPERIENCED A NOSE WHEEL SHIMMY. ALSO, STANDBY ATTITUDE INSTRUMENT 5 DEGREES NOSE UP. ACFT WAS TAXIED IAW ATC.
- [SDR DXTA2013021105281](https://openairdocs.org/sdr/DXTA2013021105281), Feb 6, 2013: ACCESS PANEL. CORRODED. LT WING FUEL PANEL CORRODED.
- [SDR DXTA2011020904459](https://openairdocs.org/sdr/DXTA2011020904459), Feb 8, 2011: STRUT. LOW PRESSURE. LANDING GEAR JAMMED IN DOWN AND LOCKED POSITION AFTER TAKEOFF. HANDLE WOULD NOT MOVE. FOUND NOSE STRUT UNDER PRESSURE. SERVICED STRUT WITH N2 AND OIL, IAW MM 12
- [SDR DXTA2010111504307](https://openairdocs.org/sdr/DXTA2010111504307), Nov 14, 2010: FLAP SYSTEM. MALFUNCTIONED. ON DEPARTURE, FLAPS FAILED TO RETRACT COMPLETELY & STOPPED AT 5 DEGREES WITH SLATS EXTENDED. ON ARRIVAL, MECH NOTED BITE CODE 2. CHECKLIST FOLLOWED FOR FLAPS 5 
- [SDR DXTA2010062804132](https://openairdocs.org/sdr/DXTA2010062804132), Jun 26, 2010: ACM. SEIZED. ON GROUND, OAT 90F, DETECTED THE ODOR OF SOMETHING BURNING, FOLLOWED BY VISIBLE SMOKE IN COCKPIT. OBSERVED COCKPIT SOURCE TEMP TO BE CLIMBING RAPIDLY THROUGH 15
- [SDR DXTA2010061804125](https://openairdocs.org/sdr/DXTA2010061804125), Jun 17, 2010: STRUT. DISCHARGED. NOSE GEAR BUMPS, IN CRUISE FLIGHT, AFTER APROX 1 HOUR INTO THE FLIGHT. WE FELT AND HEARD 3 "BUMPS". PERFORMED MLG BUMP TROUBLESHOOTING CHECKLIST. ONLY FINDING W
- [SDR DXTA200907303746](https://openairdocs.org/sdr/DXTA200907303746), Jul 30, 2009: ACM. FAILED. CABIN PAC IS SMOKING / OVERHEATING. REPLACED CABIN ACM DUE TO INTERNAL FAILURE WITH REPAIRED UNIT. WORK PERFORMED IAW MM 21-51-00. LEAK & OPS CHECKS GOOD.
- [SDR DXTA2009063003709](https://openairdocs.org/sdr/DXTA2009063003709), Jun 29, 2009: COMPRESSOR. ODOR. DURING CRUISE, DETECTED "ENVIRONMENTAL" BURNING/SMOKE. IT CAME ON AND WENT AWAY 3 SEPARATE TIMES. THE FIRST 2 TIMES IT WAS FAINT. DID SOME PRELIM CHECKS AND DID
- [SDR DXTA2008121903411](https://openairdocs.org/sdr/DXTA2008121903411), Dec 19, 2008: PDU. INOPERATIVE. AMBER CAS MESSAGE FLAPS FAIL ILLUMINATED IN FLIGHT (NO BIT CODES AVAILABLE) AND WOULD NOT REST. FLAPS FAILED IN THE UP POSTION/ THE SLATS DID NOT EXTENDED. FLAP
- [SDR DXTA2008122203411](https://openairdocs.org/sdr/DXTA2008122203411), Dec 19, 2008: WARNING MESSAGE. ILLUMINATED. AMBER CAS MESSAGE FLAPS FAIL ILLUMINATED IN FLIGHT AND WOULD NOT RESET. FLAPS FAILED IN THE UP POSTION. THE SLATS DID NOT EXTENDED.
- [SDR DXTA200802833](https://openairdocs.org/sdr/DXTA200802833), Feb 1, 2008: WINDOW. BROKEN. PILOT FWD SIDE WINDOW SHATTERED IN FLIGHT. REMOVED PILOT FWD SIDE WINDOW P/N 9914379-5, S/N 99048H 9608 AND INSTALLED A NEW SERVICEABLE WINDOW P/N 9914379-7, S/
- [SDR DXTA200802812](https://openairdocs.org/sdr/DXTA200802812), Jan 30, 2008: ACTUATOR. MALFUNCTIONED. ON CLIMB OUT, PASSING THROUGH 10,000 FT AND 250 KIAS , RUDDER LIMIT FAIL-B CAS MESSAGE LIMIT WAS FAILED AT 26 PERCENT. TROUBLESHOT: REPLACED ACTUATOR A IAW MM C
- [SDR DXTA200702399](https://openairdocs.org/sdr/DXTA200702399), Aug 13, 2007: CLUTCH. SLIPPED. FLAPS INOP. RAN CHECKLIST, DID NOT RESET. 3 DEGREES RESET SWITCH DID NOT WORK. FLAPS FAIL AS SOON AS 5 DEGREES SELECTED. 5 DEGREE FLAPS DID NOT EXTEND. CLUTCH C
- [SDR DXTA200702277](https://openairdocs.org/sdr/DXTA200702277), Jun 18, 2007: UNKNOWN. UNKNOWN. AIRCRAFT CONSTANTLY ROLLS LT AND RT IN LEVEL CRUISE. WORSE AT HIGHER ALTITUDE AND HIGHER SPEED. [07-11-07] RESET RT AILERON DROOP TO SPEC. AND ADJUSTED AILERON 
- [SDR DXTA200702275](https://openairdocs.org/sdr/DXTA200702275), Jun 15, 2007: ROLL SERVO. INOPERATIVE. DURING DESCENT FROM CRUISE AUTOPILOT ROCKS WINGS BACK AND FORTH BETWEEN FL410 AND FL360 WITH A/P DISCONNECTED AIRCRAFT FLIES LEVEL WITH NO ROLL. REMOVED AND REP
- [SDR DXTA200702248](https://openairdocs.org/sdr/DXTA200702248), Jun 7, 2007: GROUND STUD. DAMAGED. DURING FLIGHT WITH AUTOPILOT ENGAGED AIRCRAFT ROLLS BACK AND FORTH AS IF SEARCHING FOR LEVEL FLIGHT. FOUND GROUND STUDS TG532 AND TG533 AT YSAC COMPUTERS NORMAL
- [SDR DXTA200702130](https://openairdocs.org/sdr/DXTA200702130), Apr 22, 2007: ROLL SERVO. INOPERATIVE. AILERON OSCILLATION BACK AND FORTH DURING CRUISE, WORSENING DURING DESENT WITH AUTOPILOT ON. SWITCHING FGC HAD NO EFFECT. REMOVED AND INSTALLED A NEW POWER SERV
- [SDR DXTA200400384](https://openairdocs.org/sdr/DXTA200400384), Sep 8, 2004: SENSOR. FAULTY. AT 80 KIAS AMBER MASTER WARNING ILLUMINATED WITH LOW AMBER OIL LEVEL LOW-R CAS MESSAGE, TAKEOFF ABORTED. EICAS INDICATES 1 QUART LOW AND SIGHT GAUGE INDICATES 1
- [SDR DXTA200400312](https://openairdocs.org/sdr/DXTA200400312), May 14, 2004: WARNING LIGHT. ILLUMINATED. ON TAKE-OFF AT 60 KNTS, (FUEL FILTER BYPASS L) CAS MESSAGE CAME ON, ABORTED TAKE-OFF. ITEM IS UNDER INVESTIGATION.
- [SDR DXTA200400262](https://openairdocs.org/sdr/DXTA200400262), Mar 15, 2004: WARNING LIGHT. ILLUMINATED. DURING TAKEOFF ROLL MASTER WARNING AND NO TAKEOFF CAS MESSAGE CAME ON AT APPROX 90 KNOTS, ABORTED TAKEOFF. ITEM IS UNDER INVESTIGATION.
- [SDR DXTA200300111](https://openairdocs.org/sdr/DXTA200300111), Sep 10, 2003: TORQUE LINK. WORN. AFTER TAKE OFF FROM SWF FOR PHL, LANGING GEAR WOULD NOT RETRACT, ACCOMPLISHED AIT TURN BACK TO SWF. - INSPECTED GEAR & FOUND THE NOSE GEAR TORQUE LINK CAM BOLT 
- [SDR 2002F00933](https://openairdocs.org/sdr/2002F00933), Sep 11, 2002: CONTROL VALVE. FAILED. DESCENDING THROUGH 18,000 FEET LIGHT THUMP AND LANDING GEAR UNLOCK LIGHT ILLUMINATED. THIS HAPPENED TWICE MORE AT 10,000 FEET AND 6,000 FEET. AIRCRAFT LANDED WI

## STCs that may be installed (OpenAirDocs) (16)

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 680A)

- [STC ST04765NY](https://openairdocs.org/stc/ST04765NY): Unprepared (Grass/Sod) Runway Operations. Textron Aviation Inc
- [STC ST00885LA](https://openairdocs.org/stc/ST00885LA): Installation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON, LLC d/b/a MASS Systems
- [STC ST12344IB](https://openairdocs.org/stc/ST12344IB): Replacement of the Halon Type 1211 portable fire extinguisher with Halotron BrX portable fire extinguisher with Halotron BrX portable fire extinguisher. Cessna Duesseldorf Citation Service Center GmbH
- [STC ST122244IB](https://openairdocs.org/stc/ST122244IB): Installation of Gogo Galileo system, including HDX Antenna. Alamo Engineering GmbH
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC ST11983SE](https://openairdocs.org/stc/ST11983SE): Installation of Starlink Aviation System. AeroMech Incorporated
- [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc
- [STC ST01117DE](https://openairdocs.org/stc/ST01117DE): Installation of the Gogo ATG C1. Peregrine
- [STC ST02037WI](https://openairdocs.org/stc/ST02037WI): Installation of Gogo Business Aviation AVANCE L5 System with MB 13 Antennas. Duncan Aviation Inc
- [STC ST04736NY](https://openairdocs.org/stc/ST04736NY): True Blue TS28 Emergency Battery Power Supply Replacement. Aerospace Design and Compliance LLC
- [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [STC ST04575AT](https://openairdocs.org/stc/ST04575AT): Installation of the Rockwell Collins ALT-1000+/ -4000+ with 5G Filtering. Chippewa Aerospace Inc
- [STC ST04367CH](https://openairdocs.org/stc/ST04367CH): Installation of a Medical Interior in accordance with LifePort Master Data List EGR-887-000-001, Revision (B), dated April 18, 2019 or later FAA approved revision and LifePort Master Drawing List MDL-887-00, Revision (D), dated April 11, 2019 or later FAA approved revision.". LifePort LLC
- [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
- [STC ST11071SC](https://openairdocs.org/stc/ST11071SC): Demonstration of aircraft critical equipment and antenna systems tolerance of radio frequency interference (RFI) from intentional or spurious transmissions from certain Portable Electronic Devices (PEDs). Liberty Partners Inc
- [STC ST11168SC](https://openairdocs.org/stc/ST11168SC): Installation of a Pratt & Whitney Flight Data Acquisition, Storage, and Transmission System (FAST). Pratt & Whitney Engine Services Inc

## Related

- Other Textron 680A aircraft: https://openairdocs.org/model/textron-680a/aircraft.md
- The Pratt & Whitney Canada PW306D1 engine: https://openairdocs.org/engine/pratt-whitney-canada-pw306d1.md

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