# N928QS: 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: 680A0356
- Year built: 2023
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 25, 2023
- Certificate issued: November 24, 2025
- Expires: November 30, 2032
- Mode S code: ACDD51
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=928QS
- Page: https://openairdocs.org/aircraft/N928QS

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 N928QS.

## FAA accident and incident reports

None matched to N928QS.

## Service difficulty reports (6)

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 DXTA2026072709000](https://openairdocs.org/sdr/DXTA2026072709000), Jul 25, 2026: DOWNLOCK SWITCH. FAULTED. GEAR DISAGREE L ON GEAR RETRACTION. TAKING OFF FROM DAL REMOVED AND REPLACED LT GEAR DOWNLOCK SWITCH WITH NEW IAW AMM 32-30-15, REMOVED AND REPLACED WITH NEW LH
- [SDR MISR202603027043](https://openairdocs.org/sdr/MISR202603027043), Feb 27, 2026: CONTROL VALVE. DEFECTIVE. COCKPIT TEMPERATURE WAS UNCONTROLLABLE IN NORMAL OR MANUAL MODE. COCKPIT DUCT TEMPERATURE REACHED A HIGH OF 241°F. CORRECTIVE ACTION: VERIFIED DISCREPANCY. VIS
- [SDR DXTA2024122401623](https://openairdocs.org/sdr/DXTA2024122401623), Dec 20, 2024: BATTERY. FAULTED. RH EXTERIOR EMERGENCY LIGHT DOES NOT ILLUMINATE. THE QRH PROCEDURE FOR CHARGING THE EMERGENCY BATTERY PACKS WAS FOLLOWED, AND LIGHTS WILL STILL NOT ILLUMINATE. 
- [SDR DXTA2024073000033](https://openairdocs.org/sdr/DXTA2024073000033), Jul 29, 2024: SWITCH. FAULTED. WHEN MED CLOSED, HAD YELLOW CABIN DOOR OPEN & CHECK DOORS CAUTIONS. ACCOMPLISHED CHECK DOORS QRH. NO LIGHTS FUNCTIONING ON DOOR LIFT PANEL. PUSHED CANCEL BUTTON
- [SDR DXTA2024052711867](https://openairdocs.org/sdr/DXTA2024052711867), May 24, 2024: WIRE HARNESS. FAILED. PASSENGER / CREW DOORS: CABIN DOOR RETRACTS INTERMITTENTLY AND CHECK DOORS. CABIN DOOR OPEN CAS MESSAGE WILL NOT GO OUT WITH DOOR CLOSED. REMOVED AND REPLACED C
- [SDR DXTA2024051311758](https://openairdocs.org/sdr/DXTA2024051311758), May 13, 2024: WIRE. DETACHED. FLOOR EMERG EXIT LIGHT: EMERGENCY FLOOR LIGHT IN THE LAVATORY IS INOPERATIVE. APPEARS AS THOUGH THE CONNECTOR HAS DISCONNECTED. ARRIVED AT AIRCRAFT AND VERIFIED

## Service difficulty reports on N928QS not matched to an aircraft (26)

They name N928QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA2019021402020](https://openairdocs.org/sdr/DXTA2019021402020), Feb 13, 2019: CONTROLLER. DEFECTIVE. WINDSHIELD HEAT FAIL L CAS ILLUMINATED. DURING DESCENT FROM FL400 THE WSHLD HEAT INOP L CAS MESSAGE ILLUMINATED WITH AN ASSOCIATED SMELL OF BURNT ELECTRICS. WE 
- [SDR 2018090901408](https://openairdocs.org/sdr/2018090901408), Sep 9, 2018: PUMP. LEAKING. HYDRAULIC FLUID LEAK - HYDRAULIC B FAIL. HYDRAULIC OIL ALL OVER RIGHT REAR OF AIRCRAFT. 0 QUANTITY AND 0 PSI. STRONG BURNING ODORS IN CABIN.//SIGNOFF// REMOVED 
- [SDR DXTA2018090901408](https://openairdocs.org/sdr/DXTA2018090901408), Aug 9, 2018: PUMP. FAILED. HYDRAULIC FLUID LEAK - HYDRAULIC B FAIL. HYDRAULIC OIL ALL OVER RIGHT REAR OF AIRCRAFT. 0 QUANTITY AND 0 PSI. STRONG BURNING ODORS IN CABIN.//SIGNOFF// REMOVED 
- [SDR 2017F00056](https://openairdocs.org/sdr/2017F00056), Apr 6, 2017: COWLING. WORN. LEFT ENGINE HARD COWL DAMAGE REPAIR. ENGINEERING MEMO REF: DQ7684M1 DATED APRIL 5, 2017.
- [SDR DXTA2016012406173](https://openairdocs.org/sdr/DXTA2016012406173), Jan 31, 2016: UNKNOWN. ODOR. AT 40000 FT STRONG BURNING ODOR COMING FROM COCKPIT & CABIN. ODOR DISSIPATED ON ITS OWN AFTER APPROX 5 MINUTES. NO EICAS MESSAGES, PACK SUPPLY TEMPS BOTH AROUND
- [SDR DXTA2014072405831](https://openairdocs.org/sdr/DXTA2014072405831), Jul 23, 2014: ACM. FAILED. ENROUTE AFTER POWER CHANGES, WOULD GET A BURNING OIL ODOR. BECAME MORE REGULAR. BY THE TIME OF LANDING, THE CABIN FILLED WITH SMOKE. TRIED ADJUSTING CABIN PACK 
- [SDR DXTA2014033005707](https://openairdocs.org/sdr/DXTA2014033005707), Mar 30, 2014: O-RING. LEAKING. WING TANK O FULL R CAS MESSAGE CAME ILLUMINATED IN FLIGHT. FUEL WAS VENTING OVERBOARD. ASYMMETRIC FLIGHT ATTITUDE STOPPED FLOW AT APPROXIMATELY 400 LBS LOSS. TR
- [SDR DXTA2014022405664](https://openairdocs.org/sdr/DXTA2014022405664), Feb 21, 2014: PDU. FAULTY. FLAPS FAILED AT APPROXIMATELY 6 DEGREES. RESET PROCEDURES DID NOT WORK. UPON POWER UP, NO FAULTS FOUND ON CONTROLLER, FLAPS WORKING NORMAL. CYCLED FLAPS & VERIF
- [SDR DXTA2013121305596](https://openairdocs.org/sdr/DXTA2013121305596), Dec 12, 2013: FLAPPER VALVE. FAULTY. WING TANK O FULL RT MESSAGE RECEIVED IN CRUISE FLIGHT 230 WITH APPROXIMATELY 2700 LBS IN EACH WING TANK & NO FUEL IN THE CTR TANK. FUEL WAS OBSERVED VENTING FRO
- [SDR DXTA2013091705508](https://openairdocs.org/sdr/DXTA2013091705508), Sep 17, 2013: FLOAT VALVE. FAILED. UPON LEVELING OFF AT FL400 "WING TANK O'FULL R" CAS MESSAGE DISPLAYED. COMPLIED WITH QRH AND NOTICED A LARGE AMOUNT OF FUEL EXITING RIGHT WING TIP AREA. AIRPLAN
- [SDR DXTA2013091805509](https://openairdocs.org/sdr/DXTA2013091805509), Sep 17, 2013: FUEL SYS. LEAKING. DURING LEVEL OFF AT FL400, WING TANK O'FULL R CAS MESSAGE DISPLAYED. COMPLIED WITH QRH AND NOTICED A LARGE AMOUNT OF FUEL EXITING RT WING TIP AREA. AIRPLANE LOS
- [SDR DXTA2013070805434](https://openairdocs.org/sdr/DXTA2013070805434), Jul 5, 2013: ACM. SEIZED. DURING DESCENT, 20 MINUTES BEFORE LANDING, BOTH CREWMEMBERS SMELLED ELECTRICAL SMOKE IN COCKPIT. AT THE SAME TIME, COULD NOT CONTROL THE CABIN PACK IN EITHER AU
- [SDR DXTA2012070905045](https://openairdocs.org/sdr/DXTA2012070905045), Jul 8, 2012: CONTROL HANDLE. CONTAMINATED. "FLAPS FAIL" MESSAGE WHEN FLAPS 5 SELECTED, AT 8000 FEET, 240 KNOTS. AFTER LANDING AND SHUTDOWN, RESET BUTTON RAISED FLAPS, NORMAL OPS WHEN CYCLED. NO CIRCUIT B
- [SDR DXTA2011080804688](https://openairdocs.org/sdr/DXTA2011080804688), Aug 7, 2011: UPLOCK SWITCH. INOPERATIVE. NOSE GEAR WOULD NOT COME UP DURING GEAR RETRACTION. BOTH GREEN NOSE GEAR AND RED UNLOCK LIGHTS REMAINED ILLUMINATED. LANDING GEAR CAME DOWN NORMALLY. R & R FUNC
- [SDR DXTA2011072504666](https://openairdocs.org/sdr/DXTA2011072504666), Jul 24, 2011: ACTUATOR. MALFUNCTIONED. ON TAKEOFF, GEAR HANDLE UP & RED UNLOCK LIGHT STAYED ILLUMINATED AS WELL AS NLG GREEN DOWNLOCK LIGHT. COULD HEAR NLG STILL EXTENDED. PUT HANDLE DOWN & RECEIVED 
- [SDR DXTA2011062404634](https://openairdocs.org/sdr/DXTA2011062404634), Jun 23, 2011: STEERING UNIT. MALFUNCTIONED. NOSE GEAR DID NOT RETRACT AFTER GEAR HANDLE WAS SELECTED UP. MAIN GEAR RETRACTED. NOSE GEAR GREEN LIGHT REMAINED ILLUMINATED AND RED GEAR UNSAFE LIGHT REMAINED 
- [SDR DXTA2010032304044](https://openairdocs.org/sdr/DXTA2010032304044), Mar 21, 2010: ACTUATOR. CONTAMINATED. ON DEPARTURE WHEN GEAR HANDLE SELECTED TO UP, THERE WAS A SIGNIFICANT NOSE GEAR RETRACTION DELAY. THE NOSE GEAR GREEN DOWN INDICATOR REMAINED ILLUMINATED AND RE
- [SDR DXTA2010031904041](https://openairdocs.org/sdr/DXTA2010031904041), Mar 18, 2010: STEERING UNIT. FAULTY. NOSE GEAR GREEN DOWN INDICATOR REMAINED ILLUMINATED AFTER GEAR HANDLE MOVED TO RETRACT POSITION. RED UNSAFE LIGHT LIGHT REMAINED ILLUMINATED, BOTH MAIN GEAR LIG
- [SDR DXTA2010031504032](https://openairdocs.org/sdr/DXTA2010031504032), Mar 12, 2010: VALVE. MALFUNCTIONED. AMBER CAS MESSAGE "WING TANK O'FULL - R" ILLUMINATED DURING LEVEL FLIGHT. NOTICED FUEL VENTING FROM THE RT WING TIP. VENTING STOPPED AFTER TURNING OFF BOTH CTR 
- [SDR 2010F00052](https://openairdocs.org/sdr/2010F00052), Feb 27, 2010: BLADES. DAMAGED. THIS ACFT HAD FOD DAMAGE NOTED DURING THE MX WALK-AROUND IN THE NR 2 ENGINE INLET, ENG SN 330606. THE DAMAGE CONSISTED OF 4 BENT BLADES AND 7 NICKED BLADES. NO 
- [SDR DXTA2010012203951](https://openairdocs.org/sdr/DXTA2010012203951), Jan 21, 2010: FUEL TANK. OVERSERVICED. AFTER BEING ESTABLISHED IN LEVEL FLIGHT FOR 20+ MINUTES AT FL260 - AMBER "WING TANK O'FULL R" EICAS MSG DISPLAYED. FOLLOWED CHECKLIST. NOTICED FUEL VENTING FROM
- [SDR DXTA2009120703880](https://openairdocs.org/sdr/DXTA2009120703880), Dec 6, 2009: LANDING GEAR. MALFUNCTIONED. NOSEWHEEL WOULD NOT RETRACT, GEAR UNSAFE LIGHT ON AND NOSE GEAR INDICATED DOWN. LOWERED GEAR, 3 GREEN, NO RED. PERFORMED LANDING GEAR SWING AND FOUND THE SYS WO
- [SDR DXTA2009042703618](https://openairdocs.org/sdr/DXTA2009042703618), Apr 25, 2009: STEERING UNIT. MALFUNCTIONED. NOSE GEAR DID NOT RETRACT AFTER T/O. WE HAD GREEN NOSE LIGHT AND RED UNLOCK LIGHT ILLUMINATED WHEN GEAR HANDLE WAS BROUGHT UP. ALL GEAR DOWN INDICATIONS WERE NO
- [SDR DXTA2009041303591](https://openairdocs.org/sdr/DXTA2009041303591), Apr 12, 2009: LANDING GEAR. MALFUNCTIONED. NOSE LANDING GEAR DID NOT RETRACT AFTER TAKEOFF. NOSE LANDING GEAR POSITION INDICATOR REMAINED GREEN WHEN GEAR HANDLE WAS BROUGHT UP. JACKED AIRCRAFT AND INSPEC
- [SDR DXTA2009011603471](https://openairdocs.org/sdr/DXTA2009011603471), Jan 16, 2009: GENERATOR. BURNED OUT. AFTER NR 2 ENGINE START, BUS CNTR 2 FAIL MESSAGE COME ON WTIH A TOTAL OF 13 AMBER AND CYAN CAS MESSAGES. NR 4 & NR 5 MONITORS, FMS NR 2, RMU NR 2, AND FLAPS FAI
- [SDR DXTA2009012203471](https://openairdocs.org/sdr/DXTA2009012203471), Jan 16, 2009: UNKNOWN. SMOKE. AFTER NR 2 ENG START, BUSS CONTROL 2 FAIL MESSAGE CAME ON WITH A TOTAL OF 13 AMBER AND CYAN CAS MESSAGES. NR 4 AND NR 5 MONITORS, FMS NR 2, RMU NR 2, AND FLAPS 

## 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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