# N908QS: 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: 680A0322
- Year built: 2022
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 15, 2022
- Certificate issued: October 7, 2025
- Expires: October 31, 2032
- Mode S code: AC8E53
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=908QS
- Page: https://openairdocs.org/aircraft/N908QS

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 N908QS.

## FAA accident and incident reports

None matched to N908QS.

## Service difficulty reports (8)

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 DXTA2026100509976](https://openairdocs.org/sdr/DXTA2026100509976), Oct 1, 2026: WIRE. DAMAGED. TOE KICK LIGHT UNDER SEAT THREE DOES NOT WORK EITHER WITH THE EMERGENCY LIGHTING SYSTEM OR WITH THE INTERIOR LIGHTING SYSTEM SUSPECT THE LIGHT BAR IS BROKEN. FO
- [SDR DXTA2026052608164](https://openairdocs.org/sdr/DXTA2026052608164), May 20, 2026: UPLOCK SWITCH. FAULTED. R MAIN LANDING GEAR DISAGREE IN FLIGHT. CREW PERFORMED CHECKLIST, INCLUDING BOTTLE FOR BLOWDOWN AND REAR MAIN LANDING GEAR RELEASE. REMOVED UPLOCK LANDING GEAR 
- [SDR DXTA2025062504016](https://openairdocs.org/sdr/DXTA2025062504016), Jun 23, 2025: BATTERY PACK. INOPERATIVE. DURING POWER ON CHECKLIST, CHECKING THE EMERGENCY LIGHTS THE SEAT 3 PATHWAY LIGHT DOES NOT ILLUMINATE. WE CHARGED THE BATTERY ON TWO 30 MIN CHARGE CYCLES AND TH
- [SDR DXTA2025040302879](https://openairdocs.org/sdr/DXTA2025040302879), Mar 31, 2025: LIGHT. MALFUNCTIONED. UPON MULTIPLE POWER UP CYCLES EMERGENCY LIGHTS HAVE NOT OPERATED CORRECTLY. FIRST FLIGHT TODAY LIGHTS DID NOT WORK WHEN TESTED IN EITHER THE ON OR ARM POSITIONS
- [SDR DXTA2025012002039](https://openairdocs.org/sdr/DXTA2025012002039), Jan 19, 2025: LANDING GEAR. ICED. NLG LANDING GEAR RETRACTION: GOT N GEAR DISAGREE ON RETRACTION. RAN QRH PUT GEAR BACK DOWN IT LOCKED. SUSPECT ICE ACCUMULATION. CORRECTIVE ACTION: REMOVED ICE B
- [SDR DXTA2024022811023](https://openairdocs.org/sdr/DXTA2024022811023), Feb 26, 2024: DOOR. OUT OF ADJUST. MAIN DOOR: MAIN CABIN DOOR HAS TO BE PULLED FROM OUTSIDE OR PUSHED FROM THE INSIDE TO OPEN IT AFTER THE HANDLE UNLATCHES THE PINS. THE DOOR FROM THE OUTSIDE APP
- [SDR DXTA2023032182960](https://openairdocs.org/sdr/DXTA2023032182960), Mar 20, 2023: RETAINING RING. DEFECTIVE. THE CLEANERS REPORT THE MED DOES NOT CLOSE AUTOMATICALLY. INSTALLED ONE RETAINING RING PN: MS16625-4031 SN: NA TO MAIN ENTRANCE DOOR LIFT ARM/LIFT LINK ASSEMBLY
- [SDR DXTA2022102872890](https://openairdocs.org/sdr/DXTA2022102872890), Oct 27, 2022: G SWITCH. TRIPPED. WHEN SHUTTING THE AIRPLANE DOWN, WITH ALL POWER OFF EXCEPT THE BATTERIES CONNECTED, THE EXIT LIGHTS BY THE MAIN CABIN DOOR AND THE FLOOR LIGHT UNDER SEAT 10 REM

## Service difficulty reports on N908QS not matched to an aircraft (24)

They name N908QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA2012032604431](https://openairdocs.org/sdr/DXTA2012032604431), Mar 25, 2012: A/C PACK. SMOKE. WHILE IN FLIGHT, A FAINT POP WAS HEARD, FOLLOWED BY A SLIGHT SMOKE ODOR. CABIN WAS INSPECTED AND NO SOURCE FOUND. UPON ARRIVAL AT RAMP AFTER ENGINE SHUTDOWN, CA
- [SDR DXTA2010040104056](https://openairdocs.org/sdr/DXTA2010040104056), Mar 31, 2010: STRUT. UNDERSERVICED. "BUMP IN THE NIGHT" NOSE GEAR BUMP OCCURRED SEVERAL TIMES IN FLIGHT. FOUND LOWER STRUT AT 38 PSI. SERVICED LOWER STRUT AS REQ'D. READS 50 PSI AT THIS TIME. OPS 
- [SDR 2010F00034](https://openairdocs.org/sdr/2010F00034), Feb 11, 2010: WARNING LIGHT. ILLUMINATED. FUEL FILTER BYPASS R ILLUMINATED IN FLIGHT.
- [SDR DXTA2009091103782](https://openairdocs.org/sdr/DXTA2009091103782), Sep 11, 2009: METERING VALVE. WEAK. BRAKES DO NOT WORK PROPERLY. HAVE TO PUSH DOWN BRAKE PEDALS VERY HARD AND STILL DOES NOT SLOW DOWN AIRPLANE PROPERLY. NEED MORE RUNWAY THEN USUAL TO STOP. REMOV
- [SDR DXTA2009041303594](https://openairdocs.org/sdr/DXTA2009041303594), Apr 11, 2009: WHEEL. VIBRATION. YAW DAMPER OFF LOWER AMBER CAS MESSAGE ILLUMINATED DURING INITIAL T/O ROLL. ASSOCIATED WITH MODERATE SHIMMY FELT IN NOSE WHEEL. INSPECTED NOSE GEAR TORQUE LINKS
- [SDR DXTA200702669](https://openairdocs.org/sdr/DXTA200702669), Dec 9, 2007: IRS. UNKNOWN. DURING CRUISE FLT AT FL410, NR2 IRS FAILED. WE WERE ABLE TO REVERT AND USE NR1 IRS INFO. CHECKED FAULTS AND FAULTS FOR PREVIOUS LEG CALL FOR RETURN TO SERVICE &
- [SDR DXTA200702476](https://openairdocs.org/sdr/DXTA200702476), Sep 14, 2007: UNKNOWN. MALFUNCTIONED. THE APU WAS RUNNING NORMAL WHEN IT SHUTDOWN BY ITSELF FOR NO REASON. TRIED TO RESTART THE APU BUT IT WOULD NOT GO PAST 23 PERCENT. DID A COMPLETE RESET OF THE A
- [SDR DXTA200702455](https://openairdocs.org/sdr/DXTA200702455), Sep 7, 2007: CABLE. STICKING. BRAKES REQUIRE EXCESSIVE FORCE FOR LANDING AND TAXIING. AFTER LANDING, BRAKES SEEMED AT TIMES AS IF THEY WERE DRAGGING AND HAD TO APPLY 50+ N2 TO TAXI. VERIFIED
- [SDR DXTA200702449](https://openairdocs.org/sdr/DXTA200702449), Sep 5, 2007: BRAKE. NOISY. AFTER LANDING THE RT BRAKE MADE A LOUD GRINDING NOISE. WE REQUIRED 50 PERCENT N1 TO TAXI THE AIRCRAFT.
- [SDR DXTA200702440](https://openairdocs.org/sdr/DXTA200702440), Sep 1, 2007: BRAKE ASSY. NONE. RT BRAKE REQUIRES EXCESSIVE FORCE FOR NORMAL BRAKING. SAME FOR LT AND RT SEAT PEDALS. PERFORMED HIGH SPEED TAXI CHECK AND APPLIED BRAKES NUMEROUS TIMES. NO EXCE
- [SDR DXTA200702415](https://openairdocs.org/sdr/DXTA200702415), Aug 21, 2007: BYPASS VALVE. INOPERATIVE. AN EXCESSIVE ODOR OF BURNING OIL IS PRESENT THROUGHOUT CABIN. FOUND APU OIL OVER SERVICED. REMOVED 0.5 CAPS OIL TO BRING APU OIL TO SERVICEABLE LEVEL. INSPECTED
- [SDR DXTA200702297](https://openairdocs.org/sdr/DXTA200702297), Jun 25, 2007: HYDRAULIC SYSTEM. FAILED. DURING CRUISE AT FL480, THE B SIDE HYDRAULIC SYSTEM FAILED. AMBER CAS MESSAGE B PUMP FAIL, THE B QTY LOW, B PRESSURE DROPPED TO 0 PSI, QTY DROPPED TO 2 PERCENT,
- [SDR DXTA200702189](https://openairdocs.org/sdr/DXTA200702189), May 13, 2007: ACM. FROZEN. AFTER LANDING, COCKPIT TEMP INDICATOR ROSE TO 250 DEGREES AND BLACK SMOKE FILLED THE COCKPIT. COCKPIT TEMP WAS UNCONTROLLABLE THE LAST 30 MINUTES OF THE FLT WIT
- [SDR DXTA200701898](https://openairdocs.org/sdr/DXTA200701898), Jan 31, 2007: UNKNOWN. ODOR. BURNING SMELL COMING FROM OUTSIDE THE LT AFT FUSELAGE. (NEAR TAILCONE AND NR 1 ENGINE). ACRID AND OILY CONSISTENCY. RAN APU & BOTH ENGINES FOR A PERIOD OF 30 MI
- [SDR DXTA200601604](https://openairdocs.org/sdr/DXTA200601604), Sep 14, 2006: RESERVOIR. UNKNOWN. BRAKES ARE SPONGY ON LANDING, DURING A STATIC TAKEOFF THE BRAKES WOULD NOT HOLD THE AIRCRAFT ABOVE 75% N1 FROM EITHER PILOT SEAT. BLED ALL BRAKES. TAXIED ACFT T
- [SDR DXTA200601351](https://openairdocs.org/sdr/DXTA200601351), Apr 18, 2006: NUT. LOOSE. AFTER TAKEOFF CLIMBING THROUGH FL 250 NOTICE A BUMP OR THUMP APPARENTLY COMING FROM NOSE GEAR AREA FOLLOWED BE GEAR UNLOCKED RED LIGHT. CYCLED GEAR ON APP & LIG
- [SDR DXTA200601177](https://openairdocs.org/sdr/DXTA200601177), Jan 1, 2006: SENSOR. MALFUNCTIONED. YAW DAMPER FAIL UPPER A - B FAIL ILLUMINATED IN FLIGHT UPPER RUDDER WOULD NOT MOVE. REMOVED AND REPLACED RT UPPER RUDDER POSITION SENSOR. COMPLIED WITH RIG & OP
- [SDR DXTA200500827](https://openairdocs.org/sdr/DXTA200500827), Jul 8, 2005: ACTUATOR. FAILED. AMBER "RUB LIMIT FAIL B" CAS MESSAGE WITH A AMBER "RUDDER LIMIT 18%" MESSAGE IN EICAS CNTRL POSITION PAGE. EVENT MARKER PUSHED. COULD NOT DUP FLT CREWS DISCREPA
- [SDR DXTA200500817](https://openairdocs.org/sdr/DXTA200500817), Jul 3, 2005: BRAKE. MALFUNCTIONED. DURING LANDING ROLLOUT BRAKES WERE SOFT AND FELT UNRESPONSIVE WHEN HARD BRAKING WAS APPLIED. ON TAXI IN BRAKES WERE CHECKED BY BOTH PILOTS AND BOTH PILOTS HAD T
- [SDR DXTA200500834](https://openairdocs.org/sdr/DXTA200500834), Jun 25, 2005: ACTUATOR. FAILED. RUD LIMIT FAIL B AMBER CAS MESSAGE IN CRUISE FLIGHT, FAILED AT 18%. INSTALLED OVERHAULED LWR RUDDER TRAVEL LIMITER ACTUATOR IAW 750 M/M 27-23-00, AND 27-20-00-7
- [SDR DXTA200500653](https://openairdocs.org/sdr/DXTA200500653), Mar 31, 2005: SENSOR. FAILED. ON TAKEOFF ROLL, FULL POWER, ABOUT 70-80 KTS THE RED STAB BLD LEAK L CAS MESSAGE ILLUMINATED. INSTALLED NEW STABILIZER TEMP SENSOR. OPS CHECKED GOOD IAW 750 MM 
- [SDR DXTA200500605](https://openairdocs.org/sdr/DXTA200500605), Feb 21, 2005: ACM. DISINTEGRATED. DESCENDING FROM FL 410, LOAD POP HEARD FROM REAR OF AIRPLANE AND SMOKE SMELL FILLED THE COCKPIT. PER CHECKLIST ISOLATED THE COCKPIT PAC AND THE SMOKE DISSIPATED
- [SDR DXTA200300117](https://openairdocs.org/sdr/DXTA200300117), Sep 15, 2003: FILTER. CLOGGED. FUEL FILTER BYPASS L CAS MESSAGE CAME ON ABOUT 5 SECONDS AFTER TAKEOFF POWER APPLIED. TAKEOFF ABORTED. INSTALLED NEW FUEL FILTER & RESET BYPASS INDICATOR IAW AE
- [SDR DXTA200300104](https://openairdocs.org/sdr/DXTA200300104), Aug 27, 2003: CIRCUIT BREAKER. TRIPPED. DURING CLIMB THRU 7000 FEET " REMOTE CB TRIPPED" CYAN CAS MESSAGE ILLUMINATED AND ELECTRICAL FIRE SMELL WAS NOTED IN COCKPIT, NO SMOKE SEEN IN AIRCRAFT. FOUND P

## 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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