# N932QS: 2023 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: 680A0361
- Year built: 2023
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 20, 2023
- Certificate issued: September 10, 2026
- Expires: September 30, 2033
- Mode S code: ACEE86
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=932QS
- Page: https://openairdocs.org/aircraft/N932QS

From the FAA registry file of October 28, 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 N932QS.

## FAA accident and incident reports

None matched to N932QS.

## 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 2026FA0000643](https://openairdocs.org/sdr/2026FA0000643), Aug 15, 2026: STRINGER. DEBONDED. DISBOND, LH WING, UPPER SKIN BOND ASSY, S-2 @ CWS 117.60 AND S-3 @ CWS 201.25. THE SKIN AND COMMON STRINGERS MAY ALSO EXHIBIT A GRADUAL DEVIATION FROM CONTOUR I
- [SDR DXTA2026060808359](https://openairdocs.org/sdr/DXTA2026060808359), Jun 5, 2026: BATTERY PACK. DEFECTIVE. RIGHT HAND WING INSPECTION LIGHT IS VERY DIM WHEN PAX SAFETY AND BATTERIES ON OR WHEN BATTERIES OFF AND EMERGENCY LIGHTS ARMED. LIGHT IS BRIGHT WHEN SELECTING W
- [SDR DXTA2026010806441](https://openairdocs.org/sdr/DXTA2026010806441), Jan 4, 2026: ACTUATOR. FAULTY. AFTER EXTENDING THE GEAR THE NOSE GEAR GREEN INDICATER DID NOT ILLUMINATE FOLLOWED BY A GEAR DISAGREE N AMBER CAS MESSAGE. THE GEAR FELT AND SOUNDED AS IF IT WA
- [SDR DXTA2025092305029](https://openairdocs.org/sdr/DXTA2025092305029), Sep 20, 2025: UPLOCK SWITCH. DEFECTIVE. DURING APPROACH PUT GEAR HANDLE DOWN & IMMEDIATELY GOT A GEAR DISAGREE L AMBER CAS MESSAGE & A YELLOW X ON LT GEAR INDICATOR. TERMINATED APPROACH & RAN THRU EME
- [SDR DXTA2025091904997](https://openairdocs.org/sdr/DXTA2025091904997), Sep 17, 2025: BATTERY PACK. NO TEST. DURING PREFLIGHT, POWER ON CHECKLIST, EMER LTS CHECK, THE FLOOR EMEGENCY EXIT LIGHT AT SEAT 8 WOULD NOT ILLUMINATE. ALL OTHER LIGHTS EXCEPT SEAT 5 WORKED AS DES
- [SDR DXTA2025070204087](https://openairdocs.org/sdr/DXTA2025070204087), Jun 29, 2025: SWITCH. DEFECTIVE. ON APPROACH AFTER SELECTING LANDING GEAR DOWN RECEIVED AN AMBER CAS PARK BRAKE ON. RAN THE QRH AND MESSAGE REMAINED. CALLED MAINTENANCE AND AT THEIR SUGGESTION 
- [SDR DXTA2025061003802](https://openairdocs.org/sdr/DXTA2025061003802), Jun 6, 2025: CONTROL MODULE. DEFECTIVE. MLG: UPON GEAR EXTENSION WE RECEIVED AN AMBER GEAR DISAGREE L AND OR R AND OR N CAS MESSAGE. EMER/ABNORMAL PROCEDURE COMPLETED AND GEAR EXTENDED VIA THAT PROCED
- [SDR DXTA2024110401002](https://openairdocs.org/sdr/DXTA2024110401002), Oct 30, 2024: DISCONNECT UNIT. DEFECTIVE. DURING CONTROL CHECK CAP`S YOKE TURNED RT, THEN LT, THEN BACK TO CENTER, COPILOTS YOKE STAYED IN A FULL LT TURN WHEN CAPS WAS BROUGHT BACK TO CENTER. DURING TAX
- [SDR DXTA2024050811704](https://openairdocs.org/sdr/DXTA2024050811704), May 7, 2024: WARNING MESSAGE. FALSE INDICATION. GIA FAIL 2 AMBER CAS: GSD FAIL 2 CAS MESSAGE DISPLAYED. CRUISE FLIGHT AT FL430, ALL FLIGHT CONDITIONS NORMAL, NO ICING, VFR. COMPLIED WITH THE GAD FAIL 2 ABNORM
- [SDR DXTA2024010210464](https://openairdocs.org/sdr/DXTA2024010210464), Dec 29, 2023: SWITCH. FAILED. RED PUSH BUTTON FOR MAIN ENTRY DOOR IS STUCK AND WILL NOT ALLOW SOLENOID TO ALLOW EGRESS. LINE SERVICE OPENED AIRCRAFT FROM OUTSIDE. ACCESSED MED SWITCH. BYPASS

## Service difficulty reports on N932QS not matched to an aircraft (18)

They name N932QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA2010043004080](https://openairdocs.org/sdr/DXTA2010043004080), Apr 29, 2010: LATCH. DISLODGED. SHORTLY AFTER TAKEOFF - WHILE CLIMBING IN MODERATE TURBULENCE - FELT A THUD, HEARD A POP AND GOT AN AMBER 'NOSE DOOR OPEN R' EICAS MESSAGE. AFTER LANDING, FOUND
- [SDR DXTA2010021903996](https://openairdocs.org/sdr/DXTA2010021903996), Feb 18, 2010: TERMINAL. LOOSE. DURING APPROACH TO IAD WE NOTICED A SMOKE LIKE ODOR IN THE COCKPIT. IT SEEMED TO INTENSIFY AS APPROACHED THE RUNWAY. NFORMED APPROACH AND THEY DECLARED AN EMERG
- [SDR DXTA2009112503870](https://openairdocs.org/sdr/DXTA2009112503870), Nov 24, 2009: CONNECTOR. LOOSE. NOSE WHEEL DOWN AND LOCKED LIGHT FAILED TO ILLUMINATE AFTER GEAR EXTENTION - RETRACTED GEAR IAW GO AROUND CHECKLIST. RAN GEAR, WON`T EXTEND CHECKLIST AND PULLED
- [SDR DXTA2009041703603](https://openairdocs.org/sdr/DXTA2009041703603), Apr 16, 2009: STEERING UNIT. FAULTY. NOSE WHEEL SHIMMY AT 30 KTS WAS EXCESSIVE. ABORTED T/O NO FASTER THAN 60 KTS. TRIED TO HAVE BACK PRESSURE ON YOKE TO EASE NOSE WHEEL SHIMMY, HAD NO EFFECT. REMO
- [SDR DXTA2009012203472](https://openairdocs.org/sdr/DXTA2009012203472), Jan 19, 2009: A/C PACK. SMOKE. ON THE GROUND , ENGINE OFF, APU RUNNING, CABIN FILLED UP WITH SMOKE. SMOKE CAME OUT OF THE CABIN WEMACS. SMOKE STOPPED WHEN CABIN PAC WAS TURNED OFF.
- [SDR DXTA200803071](https://openairdocs.org/sdr/DXTA200803071), May 19, 2008: BULB. INOPERATIVE. LT MAIN GEAR INDICATOR LIGHT NOT ILLUMINATED WHEN GEAR HANDLE IS DOWN. RELAMPED LT MLG LIGHT IAW MM 33-10-00. CYCLED LANDING GEARS SEVERAL TIMES, ALL ANNUNCIATO
- [SDR DXTA200802976](https://openairdocs.org/sdr/DXTA200802976), Apr 1, 2008: ACM. FROZEN. CANNOT CONTROL TEMP ON CABIN PAC. CABIN FILLED WITH SMOKE. REMOVED & REPLACED FORWARD ACM IAW MM 21-51-00. OPS & LEAK CHECKS ARE GOOD.
- [SDR DXTA20082976](https://openairdocs.org/sdr/DXTA20082976), Apr 1, 2008: A/C PACK. MALFUNCTIONED. CANNOT CONTROL TEMP ON CABIN PAC. CABIN FILLED WITH SMOKE.
- [SDR DXTA200702517](https://openairdocs.org/sdr/DXTA200702517), Oct 1, 2007: FLAP SYSTEM. MALFUNCTIONED. FLAPS WOULD NOT EXTENDED IN FLIGHT, PRESSING FLAPS RESET BUTTON & PULLING FLAP CONTROL CB DID NOT FIX THE PROBLEM. PERFORMED AN OPERATIONAL CHECK OF THE FLAP SL
- [SDR DXTA200601561](https://openairdocs.org/sdr/DXTA200601561), Aug 19, 2006: CONTROL MODULE. DEFECTIVE. ON GROUND WITH APU RUNNING ENGINES SHUTDOWN L ENG FIRE CAS MASTER WARNING AND L FIRE LIGHT ILLUMINATED FOR 1 MINUTE THEN EXTINGUISHED CYCLE REPEATS EVERY MINUTE
- [SDR DXTA200601387](https://openairdocs.org/sdr/DXTA200601387), May 10, 2006: ACM. SEIZED. ON GROUND WITH APU RUNNING AFTER SELECTING MAX COOL THERE WAS A LOUD POP FOLLOWED BY SMOKE IN THE COCKPIT. RAN AIRCRAFT. FOUND COCKPIT ACM TURBINE SEIZED. REMOV
- [SDR DXTA200601280](https://openairdocs.org/sdr/DXTA200601280), Mar 3, 2006: SEAL. LEAKING. LANDING GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION AFTER TAKEOFF. INSPECTED NOSE LANDING GEAR AND FOUND GEAR EXTENSION BEYOND ALLOWABLE LIMITS. REMOVED LOWER
- [SDR DXTA200601279](https://openairdocs.org/sdr/DXTA200601279), Mar 3, 2006: HANDLE. INOPERATIVE. LANDING GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION AFTER TAKEOFF.
- [SDR DXTA200601273](https://openairdocs.org/sdr/DXTA200601273), Feb 8, 2006: FLOAT VALVE. STUCK. DURING FLIGHT "WING O-FULL L" CAS MESSAGE ILLUMINATED, LOST 300 LBS IN 5 MINUTES. DURING POST FLIGHT INSPECTION, THE FUEL WAS STILL LEAKING OUT ON THE GROUND. I
- [SDR DXTA200501115](https://openairdocs.org/sdr/DXTA200501115), Nov 27, 2005: WARNING LIGHT. FALSE ACTIVATION. "BAGGAGE SMOKE" ILLUMINATED ON EICAS AFTER TAKEOFF. COMPARTMENT WAS ISOLATED AND WE RETURNED FOR LANDING. ONCE ON THE GROUND THERE WAS NO SIGN OF SMOKE OR FIRE 
- [SDR DXTA200501065](https://openairdocs.org/sdr/DXTA200501065), Nov 6, 2005: SMOKE DETECTOR. DEFECTIVE. BAGGAGE SMOKE MASTER WARNING CAME ON DURING DESENT AT 2500 FT, CLEARED ITSELF AFTER CANCELLING THE MASTER WARNING. FUNCTIONAL TEST OF BAGGAGE SMOKE DETECTION CR
- [SDR DXTA200500989](https://openairdocs.org/sdr/DXTA200500989), Sep 28, 2005: ACM. FAULTY. AFTER LANDING AT TEB, CABIN FILLED WITH SMOKE. OVERHEAD GASPERS ON RIGHT SIDE, TOO HOT TO TOUCH. TAILCONE COMPARTMENT SHOWED FORWARD PAC OIL BOWL BLACK WITH FOA
- [SDR DXTA200400481](https://openairdocs.org/sdr/DXTA200400481), Dec 17, 2004: STRUT. LOW. AFTER TAKEOFF LANDING GEAR HANDLE WOULD NOT MOVE OUT OF THE DOWN POSITION. JACKED A/C FOUND NOSE STRUT SERVICE LOW. SERVICED NOSE STRUT AS REQUIRED. PERFORMED G

## 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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