# N901QS: 2022 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: 680A0307
- Year built: 2022
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 18, 2022
- Certificate issued: August 12, 2024
- Expires: August 31, 2031
- Mode S code: AC7452
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=901QS
- Page: https://openairdocs.org/aircraft/N901QS

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 N901QS.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20260211001089I](https://openairdocs.org/incident/20260211001089I), Feb 11, 2026: Textron Aviation Inc 680A (N901QS), West Palm Beach, FL, Minor damage. Hit a herd of deer just prior to V1

## 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 DXTA2026101910256](https://openairdocs.org/sdr/DXTA2026101910256), Oct 18, 2026: FAN. FAILED. CLIMBING THROUGH FL300 WE HEARD AN OSCILLATING/BUZZING SOUND COMING FROM BEHIND THE GLARESHIELD LEFT SIDE. SHORTLY BEFORE LANDING, THERE WAS AN ASSOCIATED UNUSU
- [SDR DXTA2026021306860](https://openairdocs.org/sdr/DXTA2026021306860), Feb 10, 2026: FAIRING. DAMAGED. HIT A HERD OF DEER JUST PRIOR TO V1, AIRCRAFT NEEDS INSPECTION FOR ANY DAMAGE. BELLY FAIRING FRAME 6 AND BELLY FAIRING C CHANNEL. DAMAGE TO THE LT MLG DOOR. THE
- [SDR DXTA2025100805216](https://openairdocs.org/sdr/DXTA2025100805216), Oct 6, 2025: FILTER. ODOR. ODOR IN CABIN WITH APU RUNNING. CORRECTIVE ACTION: STARTED APU. WITH APU BLEED AIR ON, NOTICED A VERY FAINT SMELL. REMOVED AND REPLACED THE HEPA FILTER IAW CE68
- [SDR DXTA2025020302157](https://openairdocs.org/sdr/DXTA2025020302157), Jan 29, 2025: HANDLE. MALFUNCTIONED. MAIN DOOR HANDLE: THE DOOR HANDLE IS JAMMED IN THE OPEN POSITION AND WILL NOT LATCH THE DOOR CLOSED OR STOW. DUPLICATED SQUAWK. INNER HANDLE WAS TOUGH TO CLOSE 
- [SDR DXTA2024072912484](https://openairdocs.org/sdr/DXTA2024072912484), Jul 29, 2024: DOWNLOCK SWITCH. DEFECTIVE. GEAR DISAGREE L CAS ILLUMINED DURING GEAR EXTENSION ACCOMPANIED BY AN AMBER X IN THE LEFT GEAR INDICATOR POSITION. AMBER X TURNED RED WITH FULL FLAP EXTENSION A
- [SDR DXTA2024041611519](https://openairdocs.org/sdr/DXTA2024041611519), Apr 15, 2024: HANDLE. STUCK. MAIN DOOR HANDLE: MAIN CABIN DOOR CLOSES BUT THE DOOR HANDLE IS STUCK IN THE UP POSITION. //SIGNOFF// FOUND FWD MCD LOWER DOOR PIN TO FAR IN AND GETTING CAUGHT 
- [SDR DXTA2023032883330](https://openairdocs.org/sdr/DXTA2023032883330), Mar 28, 2023: UNKNOWN. UNKNOWN. WHEN OPENING THE MAIN CABIN DOOR FROM THE OUTSIDE THE DOOR DOES NOT FREE FALL OPEN. IT HAS TO BE PULLED FAIRLY HARD TO GET IT TO OPEN. WE APPLIED POWER TO THE A
- [SDR DXTA2023012579160](https://openairdocs.org/sdr/DXTA2023012579160), Jan 24, 2023: HINGE. BROKEN. ENTRANCE STAIR: CABIN DOOR, UP DOOR STEP INTERNAL HINGES BROKEN. TOP STEP IS ASKEW NOT WATER BARRIER. C/W REPLACEMENT OF MCD UPPER STEP HINGES PN: 325.00.708. S
- [SDR DXTA2022121976580](https://openairdocs.org/sdr/DXTA2022121976580), Dec 18, 2022: CONNECTOR. DISCONNECTED. CABIN EMERG LIGHT: READING LIGHT ABOVE SEAT 7 WILL NOT ILLUMINATE. GAINED ACCESS TO EMERGENCY LIGHTING READING LIGHT. FOUND CONENCTORS NOT FULLY FLUSH/CONNECTED
- [SDR DXTA2022112874750](https://openairdocs.org/sdr/DXTA2022112874750), Nov 25, 2022: LIGHT. DEFECTIVE. CABIN EMERG LIGHT: EMER LIGHT ABOVE SEAT 7 INOP. REMOVED AND REPLACED EM ER/READING LIGHT ABOVE SEAT 7 WITH NJA PROVIDED NEW PART. OPERATIONAL CHECKS GOOD. ALL 
- [SDR DXTA2022052662670](https://openairdocs.org/sdr/DXTA2022052662670), May 26, 2022: MODULE. FAILED. FLAPS FAIL AMBER CAS: DURING LANDING FLAPS WERE SELECTED TO ONE WITH NO ISSUE. WHEN FLAPS TWO WAS SELECTED FLAPS FAILED. FLAPS WERE RESET PER THE CHECKLIST. WHE

## Service difficulty reports on N901QS not matched to an aircraft (25)

They name N901QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR CWQR20160502014](https://openairdocs.org/sdr/CWQR20160502014), May 2, 2016: TUBE. LEAKING. DURING A SCHEDULED MX, WHEN PERFORMING POST INSPECTION ENG RUNS, FOUND LT ENG BLEED AIR TUBE ASSEMBLY LEAKING AT THE BELLOWS & SMALL AREA OF DISCOLORATION, BUT 
- [SDR DXTA2014032805700](https://openairdocs.org/sdr/DXTA2014032805700), Mar 27, 2014: UNKNOWN. ODOR. DURING INITIAL POWER REDUCTION AT TOP OF DESCENT, A SULFUR BURNING ODOR WAS PRESENT FOR ABOUT 30 SECONDS. NO SMOKE OBSERVED & ODOR QUICKLY DISSIPATED. INSPECTED
- [SDR DXTA2013032505334](https://openairdocs.org/sdr/DXTA2013032505334), Mar 24, 2013: BULB. INOPERATIVE. ON FINAL WHEN GEAR SELECTED DOWN BOTH LT MAIN GREEN LIGHTS WERE INOPERATIVE. PERFORMED FLYBY OF TOWER CONFIRMED ALL GEAR DOWN. RAN GEAR WOULD NOT EXTEND CHECKLI
- [SDR DXTA2013021905293](https://openairdocs.org/sdr/DXTA2013021905293), Feb 18, 2013: WHEEL. WORN. VIOLENT NOSEWHEEL SHIMMY ON TAKEOFF ROLL. BEGAN RT AFTER TAKEOFF POWER APPLIED AND ABORTED AT APPROX 30 KTS. REMOVED BOTH NOSE WHEELS AND TIRE ASSEMBLIES AND IN
- [SDR DXTA2013011705246](https://openairdocs.org/sdr/DXTA2013011705246), Jan 16, 2013: CONNECTOR. DAMAGED. THE LANDING GEAR HANDLE WOULD NOT MOVE TO THE RETRACT POSITION AFTER TAKEOFF. RETURNED TO DEPARTURE WITH 3 GREEN SAFE LIGHTS. FOUND CONNECTOR JG019 FOR THE NLG 
- [SDR DXTA2012070205024](https://openairdocs.org/sdr/DXTA2012070205024), Jun 29, 2012: SKIN. CORRODED. ACCOMPLISH REPAIR FOR RT WING FUEL PANEL LANDS THAT ARE BEYOND MM SPECS. ACCOMPLISHED REPAIRS TO THE RT WING FUEL PANEL LANDS IAW REPORT NR: S-750-ATA57/09RD RE
- [SDR DXTA2012070605035](https://openairdocs.org/sdr/DXTA2012070605035), Jun 13, 2012: SKIN. DAMAGED. ACCOMPLISHED REPAIR FOR LT WING FUEL PANEL LANDS THAT ARE BEYOND MM SPECIFICATIONS. ACCOMPLISHED REPAIRS IAW MFG REPORT S-750-ATA57/09RD.
- [SDR DXTA2012040204939](https://openairdocs.org/sdr/DXTA2012040204939), Mar 30, 2012: UPLOCK SWITCH. FAILED. NOSE GEAR "BUMP IN THE NIGHT" TWICE ON CLIMB AT 29900'/300KIAS AND 34600'/300KIAS AND ONCE ON THE DESCENT AT 17900' AND 280KIAS. FOUND NOSE GEAR SWITCH MISSING 
- [SDR DXTA2010101204260](https://openairdocs.org/sdr/DXTA2010101204260), Oct 10, 2010: STRUT. DISCHARGED. AFTER TAKEOFF, LANDING GEAR HANDLE WOULD NOT RETRACT. A SYS PRESSURE GOOD. CHECKLIST COMPLIED WITH. FOUND NLG STRUT NOT FULLY EXTENDED WHEN ACFT JACKED. PERFORM
- [SDR DXTA2010020103965](https://openairdocs.org/sdr/DXTA2010020103965), Jan 29, 2010: SQUAT SWITCH. OUT OF LIMITS. AFTER TAKEOFF, LANDING GEAR HANDLE WAS FIRMLY STUCK IN DOWN DETENT AND COULD NOT BE MOVED. FOUND LT SQUAT SWITCH OUT OF LIMITS. ADJUSTED SWITCH RAN GEAR SEVERAL
- [SDR DXTA2009122403912](https://openairdocs.org/sdr/DXTA2009122403912), Dec 23, 2009: WINDSHIELD. FAILED. AT FL380 LT FWD WINDSHIELD SHATTERED. FOLLOWED BY WINDSHIELD HEAT INOP L AND WINDSHIELD O'TEMP L CAS MESSAGES. REMOVED AND REPLACED THE LT WINDSHIELD DUE TO THE
- [SDR DXTA2009102903834](https://openairdocs.org/sdr/DXTA2009102903834), Oct 28, 2009: SWITCH. INOPERATIVE. WITH GEAR HANDLE SELECTED DOWN, RIGHT MAIN GREEN GEAR LIGHT DOES NOT ILLUMINATED. GEAR BLOWN DOWN AND EMERGENCY EXTENSION HANDLE PULLED UNDER SINK. PERFORMED EM
- [SDR DXTA2009020503492](https://openairdocs.org/sdr/DXTA2009020503492), Feb 4, 2009: SENSOR. INOPERATIVE. LEFT ENGINE SHUT DOWN AFTER START. REPLACED NR 2 ENGINE CHANNELS A&B FADECS IAW CE 750 MM 26-12-00. OPERATIONAL CHECKS GOOD. FOUND FADEC FAULT TO BE T-2.5 SENSO
- [SDR DXTA200809123273](https://openairdocs.org/sdr/DXTA200809123273), Sep 12, 2008: ACTUATOR. INOPERATIVE. IN FLIGHT GOT RUDDER LIMIT FAIL B AMBER CAS MESSAGE. CONTROL PAGE SHOWED RUDDER LIMITED TO 44 PERCENT. REPLACED LOWER RUDDER LIMITER ACTUATOR (B) IAW MM 27-23-0
- [SDR DXT2008F00006](https://openairdocs.org/sdr/DXT2008F00006), Sep 12, 2008: LIMITER. MALFUNCTIONED. IN FLIGHT GOT RUDDER LIMIT FAIL B AMBER CAS MESSAGE. CONTROL PAGE SHOWED RUDDER LIMITED TO 44 PERCENT.
- [SDR DXTA200702391](https://openairdocs.org/sdr/DXTA200702391), Aug 8, 2007: BRAKE. UNKNOWN. BRAKING IS VERY POOR DURING LANDING ROLL. INSPECTED NR 4 BRAKE ASSEMBLY. FOUND WEAR TO BE WITHIN LIMITS. WEAR PIN IS PROTRUDING 1/16 FROM BRAKE HOUSING WITH PAR
- [SDR DXTA200702289](https://openairdocs.org/sdr/DXTA200702289), Jun 23, 2007: FUEL FILTER. BYPASSING. LT FUEL FILTER BYPASS AMBER CAS MESSAGE AS POWER WAS APPLIED FOR TAKEOFF. [07-12-07] ACCOMPLISHED INSPECTION OF BYPASS INDICATORS IAW 3007C MM 73-30-00-200-801.
- [SDR DXTA200702225](https://openairdocs.org/sdr/DXTA200702225), May 31, 2007: LANDING GEAR. VIBRATES. BAD NOSE WHEEL SHIMMY ON TAKEOFF ROLL. ABORTED TAKE OFF AT 50 KTS. [06-15-07] REPLACED LEFT & RIGHT NOSE WHEEL ASSY. IAW CE 750 MM CH 32-41-01 & 12-20-10 OP'S C
- [SDR DXTA200702205](https://openairdocs.org/sdr/DXTA200702205), May 18, 2007: ELASTOMER. WORN. EXCESSIVE NOSEWHEEL VIRBRATION DURING TAKEOFF, TAKE-OFF ABORTED. REPLACED BOTH NOSE TIRES WITH NEW AND REPLACED WORN NOSE GEAR ACTUATOR ELASTOMERS WITH NEW. TIG
- [SDR DXTA200702164](https://openairdocs.org/sdr/DXTA200702164), Apr 30, 2007: YAW DAMPER. MALFUNCTIONED. SEVERE NOSE WHEEL VIBRATION DURING TAKEOFF ROLL. TAKEOFF WAS ABORTED, LOWER YD TURNED ITSELF OFF. REMOVED AND REPLACED BOTH NOSE WHEEL ASSY. DUE TO HIGH VIBRATI
- [SDR DXTA200702031](https://openairdocs.org/sdr/DXTA200702031), Mar 16, 2007: UNKNOWN. NOISY. NOSEGEAR MAKES OCCASIONAL BUMPING NOISE IN FLIGHT.COMPLIED WITH GEAR BUMP TROUBLESHOOTING PER C750 MM 32-30-00. ALL CLEARANCES AND OPERATIONAL CHECKS TEST GOOD.
- [SDR DXTA200601244](https://openairdocs.org/sdr/DXTA200601244), Feb 15, 2006: WINDSHIELD. CRACKED. DURING CLIMB THRU FL200, ARCING & SPARKING IN CAPT'S FWD WSHIELD, LWR LT CORNER. TURNING OFF LT WSHIELD HEAT SWITCH STOPPED ARCING BUT OUTER WINDSHIELD CRACKED 
- [SDR DXTA200500716](https://openairdocs.org/sdr/DXTA200500716), May 11, 2005: PDU. INOPERATIVE. FLAPS FAIL CAS ILLUMINATED ON APPROACH. SLATS EXTENDED AND FLAPS FAILED AT 5 DEGREES. REMOVED AND REPLACED FLAP PDU IAW 750 MM CHAPTER 27-52-00. OPS CHECK GOOD.
- [SDR DXTA200500636](https://openairdocs.org/sdr/DXTA200500636), Mar 19, 2005: PRESSURE SWITCH. OUT OF ADJUST. AT FL 410 BAGGAGE DOOR SEAL CAS ACCOMPLISHED CHECKLIST AT FL 390 AMBER CABIN ALTITUDE FOLLOWED SHORTLY BY RED CABIN ALTITUDE LIGHT ILLUMINATED. PERFORMED EMERGE
- [SDR DXTA200500571](https://openairdocs.org/sdr/DXTA200500571), Feb 1, 2005: ODOR. DETECTED. CABIN AIR CONDITIONING HAS VERY STRONG ODOR, POSSIBLY DEICE FLUID FUMES. BOTH PAX COMPLAINED OF BURNING EYES AFTER 1+45 FLIGHT. ODOR IS SLIGHTLY LESS EVIDENT IN

## 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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