# N907QS: 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: 680A0321
- Year built: 2022
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 7, 2022
- Certificate issued: January 2, 2026
- Expires: January 31, 2033
- Mode S code: AC8A9C
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=907QS
- Page: https://openairdocs.org/aircraft/N907QS

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 N907QS.

## FAA accident and incident reports

None matched to N907QS.

## Service difficulty reports (9)

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 DXTA2026072708982](https://openairdocs.org/sdr/DXTA2026072708982), Jul 24, 2026: PITCH CONTROL. FAULTED. ON ROTATION & CLIMB OUT, PRIMARY PITCH TRIM FAILED. SWITCHED TO SECONDARY WHICH ALSO FAILED. RAN QRH. TECHS REVIEWED TEAM 680'S ARES ANALYSIS, WHICH DETERMINED 
- [SDR DXTA2026050407871](https://openairdocs.org/sdr/DXTA2026050407871), Apr 30, 2026: LIGHT. FAULTED. EXTERIOR EMERGENCY LIGHT ABOVE THE RIGHT WING IS NOT ILLUMINATING PROPERLY. BRIGHTNESS LEVEL IS NOT NORMAL (IT IS EXTREMELY ANEMIC) AND DOES NOT REALLY ILLUMINA
- [SDR DXTA2026050107871](https://openairdocs.org/sdr/DXTA2026050107871), Apr 30, 2026: LIGHT. DIM. EXTERIOR EMERGENCY LIGHT ABOVE THE RIGHT WING IS NOT ILLUMINATING PROPERLY. BRIGHTNESS LEVEL IS NOT NORMAL (IT IS EXTREMELY ANEMIC) AND DOES NOT REALLY ILLUMINA
- [SDR DXTA2026010906452](https://openairdocs.org/sdr/DXTA2026010906452), Jan 5, 2026: AHRS. FAULTED. DURING CRUISE FLIGHT AMBER HEADING MIS COMPARE DISPLAYED. WE NOTED A 8 DEGREE DIFFERENCE BETWEEN HDG1 AND HDG2. HDG2 MATCHED THE STBY SO WE REVERTED HDG1 OVER T
- [SDR DXTA2025090404784](https://openairdocs.org/sdr/DXTA2025090404784), Sep 1, 2025: HANDLE. MALFUNCTIONED. REPEAT RIGHT UP. THE LATCHING HANDLE ON THE MAIN CABIN DOOR WILL NOT ENGAGE. THE HANDLE WILL NOT MOVE INSIDE OR OUTSIDE WHEN THE DOORS IN THE CLOSED POSITION DO
- [SDR DXTA2025090304778](https://openairdocs.org/sdr/DXTA2025090304778), Aug 31, 2025: LATCH. FAULTED. THE LATCH WILL NOT ENGAGE ON THE MAIN CABIN DOOR FROM THE INSIDE OR THE OUTSIDE. THE DOOR IS CURRENTLY OPEN. ARRIVED AT AIRCRAFT AND CONFIRMED PILOT WRITE UP MA
- [SDR DXTA2025040802999](https://openairdocs.org/sdr/DXTA2025040802999), Apr 8, 2025: HANDLE. STUCK. MAIN DOOR HANDLE: MAIN CABIN DOOR HANDLE WILL NOT LATCH FROM INSIDE WITH DOOR CLOSED. DOOR IS STICKING, FEELS LIKE THE SEALS ARE MAKING TOO MUCH CONTACT CORRECT
- [SDR DXTA2023072491600](https://openairdocs.org/sdr/DXTA2023072491600), Jul 23, 2023: MODULE. FAULTED. MLG DID NOT COME DOWN WHEN SELECTED. CAS MESSAGE GEAR DISAGREE. AFTER RUNNING CHECKLIST ALL 3 GEAR CAME DOWN & GOT 3 GREEN. MANUALLY RESET & SAFETIED CONTROL AR
- [SDR DXTA2023050185110](https://openairdocs.org/sdr/DXTA2023050185110), May 1, 2023: UNKNOWN. UNKNOWN. MAIN DOOR: MAIN CABIN DOOR DIFFICULT OPEN OR CLOSE FROM OUTSIDE//CORRECTIVE ACTION//PERFORMED CABIN DOOR LUBE IAW TEXTRON 680A MM 12-20-40. OPENED AND CLOSED MA

## Service difficulty reports on N907QS not matched to an aircraft (27)

They name N907QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR 2020FA0000161](https://openairdocs.org/sdr/2020FA0000161), Feb 17, 2020: SKIN. CORRODED. CORROSION DAMAGE WAS FOUND AT 5 SITES ON THE RH WING UPPER SKIN FROM CWS 363.9 TO 378.71. REFERENCE FAA FORM 8100-9 FIELD REPAIR FR-750-0201-7656 REV -, DATED 2
- [SDR DXTA2019051302379](https://openairdocs.org/sdr/DXTA2019051302379), May 10, 2019: UNKNOWN. ODOR. DURING FLIGHT BURNING SMELL NOTICED NEAR GALLEY AREA. TURNED CABIN MASTER SWITCH OFF AND ODOR WENT AWAY IN LESS THAN 2 MINUTES. CABIN MASTER REMAINED OFF FOR DU
- [SDR DXTA2018110201621](https://openairdocs.org/sdr/DXTA2018110201621), Nov 2, 2018: UNKNOWN. SMOKE. AT 40,000 FEET, SMOKE AND PUNGENT ODOR IN THE COCKPIT. DIVERTED.
- [SDR DXTA2017070206419](https://openairdocs.org/sdr/DXTA2017070206419), Jul 2, 2017: HOSE. FAILED. A HYDRAULIC SYSTEM WENT TO ZERO PRESSURE AND ZERO QUANTITY SHORTLY AFTER TAKEOFF. DURING POST FLIGHT, FLUID WAS FOUND DRIPPING FROM TAILCONE COMPARTMENT. VISUAL
- [SDR 2017FA0000054](https://openairdocs.org/sdr/2017FA0000054), Feb 10, 2017: SKIN. CORRODED. LT WING LOWER SKIN CORRODED.
- [SDR DXTA2016112606332](https://openairdocs.org/sdr/DXTA2016112606332), Nov 25, 2016: APU. ODOR. PAX COMPLAINED OF ODOR IN THE CABIN. REMOVED AND REPLACED APU, AND REMOVED AND REPLACED COALESCER SOCK.
- [SDR DXTA2014050205754](https://openairdocs.org/sdr/DXTA2014050205754), Apr 23, 2014: SKIN. CORRODED. FUSELAGE SKIN UNDER DORSAL LE FAIRING CORRODED. REPAIRED IAW S-750-020113RD.
- [SDR DXTA2013010405233](https://openairdocs.org/sdr/DXTA2013010405233), Dec 22, 2012: ACM. DEFECTIVE. NOTICED A POPPING SOUND COMING FROM THE BACK OF ACFT. BURNED RUBBER ODOR WAS THEN NOTICED. COCKPIT SUPPLY TEMP WAS THEN OBSERVED RISING IN AUTO MODE. ON TROUBLE
- [SDR DXTA2012022704890](https://openairdocs.org/sdr/DXTA2012022704890), Feb 24, 2012: OIL SYSTEM. LEAKING. TOXIC SMOKE SMELL SEEMS LIKE IT IS COMING THROUGH THE WEMACS. SEEMS TO BE LESS INTENSE WITH COCKPIT PAC TURNED OFF. TROUBLESHOT TO APU INTERNAL OIL LEAK. REMOVE
- [SDR DXTA2011101004748](https://openairdocs.org/sdr/DXTA2011101004748), Oct 9, 2011: COALESCER BAG. ODOR. ON GROUND STRONG ODOR OF SMOKE IN THE COCKPIT AREA, THIS WAS FOLLOWED BY GRAY SMOKE. R & R CABIN ACM AND WATER SEPARATOR SOCKS. SYS OPS CHECKED GOOD IAW MM 21-5
- [SDR DXTA2011041804548](https://openairdocs.org/sdr/DXTA2011041804548), Apr 17, 2011: DRIVE UNIT. FAILED. FLAP FAIL AMBER CAS DURING APPROACH AND LANDING. FLAPS FAILED AT APROX 2 DEGREES WITH SLATS OUT. FOUND FLAP CONTROL BITE CODE 2. TESTED FLAP PDU IAW MM 27-50-00
- [SDR DXTA2011031704511](https://openairdocs.org/sdr/DXTA2011031704511), Mar 16, 2011: BRAKE ASSY. LEAKING. NOTICED AFTER LANDING THAT THE NR 3 MAIN WHEEL (RIGHT SIDE INNER MAIN WHEEL) WAS SMOKING. FOUND BRAKE FLUID LEAKING AND APPROX 3" PUDDLE OF FLUID ON GROUND AND 
- [SDR DXTA2010120204342](https://openairdocs.org/sdr/DXTA2010120204342), Dec 1, 2010: ACTUATOR. FAILED. AFTER TAKEOFF AMBER CAS "RUD LIMIT FAIL B" RUDDER LIMIT 90 PERCENT. RUDDER LOWER ACTUATOR FAILED CHECK. REMOVED LOWER ACTUATOR AND REPLACED WITH NEW. COMPLETED 
- [SDR DXTA2010012203952](https://openairdocs.org/sdr/DXTA2010012203952), Jan 21, 2010: SEAL. NICKED. RECEIVED AMBER CABIN ALT CAS MESSAGE & SHORTLY AFTER A RED CABIN ALT CAS MESSAGE. ALSO RECEIVED AN AMBER CARGO SEAL MESSAGE BUT NO PROBLEM WITH CABIN ALTITUDE. 
- [SDR DXTA2009031603551](https://openairdocs.org/sdr/DXTA2009031603551), Mar 14, 2009: CONTROL HANDLE. CONTAMINATED. FLAPS FAILED WHEN SELECTED TO 5 DEGREES AT 17000 FT. THE RESET SWITCH RESETS BUT FAILS IMMEDIATELY WHEN FLAPS ARE SET TO A DETENT FOR EXTENSION. SLATS OPERATE N
- [SDR DXTA2009022303521](https://openairdocs.org/sdr/DXTA2009022303521), Feb 21, 2009: SENSOR. MALFUNCTIONED. ON APPROCH THE FLAPS FAIL CAS MESSAGE CAME ON WITH THE SLATS EXTENDED AND THE FLAPS AT 3DEG. REPLACED LT AND RT RESOLVER. GAINED ACCESS TO AND REMOVED LT AND RT
- [SDR DXTA200808223236](https://openairdocs.org/sdr/DXTA200808223236), Aug 22, 2008: ACM. SEIZED. DURING APU RUN, AIRPLANE FILLED WITH SMOKE, THE SMOKE HAD A BURNING RUBBER SMELL. T/S TO CABIN ACM TURBINE BEING SEIZED. REMOVED FWD ACM IAW MM 21-51-00 8/22 RE
- [SDR DXTA200803236](https://openairdocs.org/sdr/DXTA200803236), Aug 22, 2008: UNKNOWN. ODOR. DURING APU RUN, ACFT FILLED WITH SMOKE. THE SMOKE HAD A BURNING RUBBER SMELL. KSAT.
- [SDR DXTA200803163](https://openairdocs.org/sdr/DXTA200803163), Jul 6, 2008: COALESCER BAG. ODOR. PASSENGER NOTICED OILY ODOR IN CABIN. REMOVED AND REPLACED BOTH COALESCER SOCKS AND CLEANED WATER SEPERATORS PER MM 21-51-00 OPS CHECK GOOD.
- [SDR DXTA20082959](https://openairdocs.org/sdr/DXTA20082959), Mar 22, 2008: FLAP SYSTEM. FAILED. (FLAPS FAIL) AT APPROX 3 DEGREES WITH SLATS EXTENDED. PERFORMED FLAP SYSTEM OPERATION TEST IAW MM 27-50-00 4 A, B, C, D & F. RAN FLAPS THROUGH 10 TIMES. OPS CHE
- [SDR DXTA200702107](https://openairdocs.org/sdr/DXTA200702107), Apr 15, 2007: CONTROLLER. MALFUNCTIONED. CABIN PAC HAS BURNED ODOR COMING INTO CABIN. NO DIVERTION. REMOVED AND REPLACED INOP TEMP CONTROLLER OPS CHECK GOOD IAW CE750 MM 21-61-00
- [SDR DXTA200601464](https://openairdocs.org/sdr/DXTA200601464), Jun 29, 2006: LINE. LEAKING. DURING FLIGHT FROM SAV TO HPN, NOTICED OILY ODOR WHEN PAC IS RUNNING, CONTINUED FLIGHT TO HPN WITHOUT INCIDENT. INSPECTED APU AND TAIL COMPT. FOUND APU COMPT TO
- [SDR DXTA200601233](https://openairdocs.org/sdr/DXTA200601233), Feb 5, 2006: STRUT. UNDERSERVICED. UNABLE TO MOVE GEAR HANDLE TO RETRACT (UP) POSITION AFTER TAKEOFF. TROUBLESHOT FOUND NOSE GEAR STRUT WAS NOT FULLY EXTENDING AND NOT MAKING NOSE GEAR SQUAT SWIT
- [SDR DXTA200601213](https://openairdocs.org/sdr/DXTA200601213), Jan 25, 2006: POSITION SWITCH. OUT OF ADJUST. AFTER TAKEOFF GEAR HANDLE WOULD NOT CYCLE TO UP POSITION, GEAR REMAINED DOWN AND LOCKED. ADJUSTED NOSE GEAR SQUAT SWITCH IAW CE 750 MM 32-60-00. OPS CHECK GOOD.
- [SDR DXTA200400411](https://openairdocs.org/sdr/DXTA200400411), Oct 2, 2004: VENT. MALFUNCTIONED. AT FL280 APPROXIMATELY 25 MINUTES INTO FLIGHT LEFT WING BEGAN VENTING FUEL STARTING AT 2900 LBS IN WING (NO FUEL IN CENTER TANK), VENTING CONTINUED THROUGH DESC
- [SDR DXTA200400398](https://openairdocs.org/sdr/DXTA200400398), Sep 17, 2004: FRICTION BRAKE. DAMAGED. RT BRAKE VERY SPONGY AND DOES NOT GRAB UNTIL EXCESSIVE PRESSURE IS APPLIED THEN GRABS VERY ABRUPTLY. INSPECTED THE LT AND RT BRAKES, FOUND NO LEAKS AND .2 LEFT 
- [SDR DXTA200400237](https://openairdocs.org/sdr/DXTA200400237), Feb 4, 2004: WARNING LIGHT. ILLUMINATED. ON TAKEOFF ROLL MASTER WARNING LIGHT AND AUDIO INDICATIONS APPEARED WITH NO OTHER CAS INDICATIONS. WARNINGS WENT OFF AFTER 1 CYCLE THEN REAPPEARED WITH NR 2 ENG

## 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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