# N922QS: 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: 680A0331
- Year built: 2022
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 21, 2022
- Certificate issued: November 1, 2024
- Expires: November 30, 2031
- Mode S code: ACC707
- Owner type: Co-owned
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=922QS
- Page: https://openairdocs.org/aircraft/N922QS

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 N922QS.

## FAA accident and incident reports

None matched to N922QS.

## Service difficulty reports (7)

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 DXTA2025070704147](https://openairdocs.org/sdr/DXTA2025070704147), Jul 6, 2025: BATTERY. NO TEST. NONE OF THE EMER LTS ILLUMINATE WITH SWITCH IN ARM POSITION. RAN QRH RECHARGE PROCEDURE, STILL FAILED AFTER ALLOTTED CHARGING TIME. CORRECTIVE ACTION: REMOVED A
- [SDR DXTA2025050303341](https://openairdocs.org/sdr/DXTA2025050303341), May 3, 2025: PIN. LACK OF LUBE. MAIN DOOR: THE MAIN ENTRY DOOR IS BINDING/DIFFICULT TO CLOSE. CORRECTIVE ACTION: POWERED UP AIRCRAFT AND OPERATED CABIN DOOR. DOOR OPERATES FINE - SEVERAL TIMES
- [SDR DXTA2025042803220](https://openairdocs.org/sdr/DXTA2025042803220), Apr 25, 2025: LIFT STRUT. INOPERATIVE. MAIN DOOR HARDWARE: HARWARE FELL OUT OF DOOR STRUT CORRECTIVE ACTION: TECHS FOUND HARDWARE TEMP INSTALLED ON MED DOOR STRUT. REMOVED HARDWARE AND CHECKED FOR AN
- [SDR DXTA2025042503180](https://openairdocs.org/sdr/DXTA2025042503180), Apr 22, 2025: PROBE. INOPERATIVE. WHILE IN CRUISE, RECEIVED BOTH ON ADC 2 AMBER CAS. FOLLOWED THE CORRESPONDING QRH. THE QRC DIRECTED THE LEFT SEAT PILOT TO SWITCH THE ADC TO THE NORMAL SIDE, TH
- [SDR DXTA2024122301641](https://openairdocs.org/sdr/DXTA2024122301641), Dec 18, 2024: SWITCH. TRIPPED. DURING PREFLIGHT DISCOVERED EMER LIGHTS IN LAV AREA INOPERATIVE. AFTER POWERING UP AIRPLANE THE LIGHTS TURNED ON. WHEN POWERING DOWN THE EMER LIGHTS IN THE LAV 
- [SDR DXTA2023060587910](https://openairdocs.org/sdr/DXTA2023060587910), Jun 5, 2023: UNKNOWN. UNKNOWN. MAIN DOOR: MAIN CABIN DOOR DIFFICULT TO OPEN. FOUND DOOR SEAL TO BE GETTING STUCK ON UPPER FWD CORNER. ADJUSTED MCD SEAL PER CE 680A AMM 52-10-35. OPS CHECK AND
- [SDR DXTA2023041784440](https://openairdocs.org/sdr/DXTA2023041784440), Apr 17, 2023: UNKNOWN. UNKNOWN. MAIN DOOR: MAIN CABIN DOOR BINDING WHILE OPENING AND CLOSING. DIFFICULT TO OPEN AND CLOSE FROM INSIDE AND OUTSIDE OF AIRCRAFT. FOUND DOOR SEAL DIRTY AND CAUSING

## Service difficulty reports on N922QS not matched to an aircraft (25)

They name N922QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR EE4Y2020102111780](https://openairdocs.org/sdr/EE4Y2020102111780), Oct 21, 2020: FRAME. CORRODED. DURING THE MAINTENANCE PROCESS IT WAS FOUND AT THE TAIL CONE 170-50005-423 S/N: 0478001, AREA RT, SILENCER FWD EDGE SKIN WITH BULGED. THE AREA WAS ACCESSED, AND
- [SDR DXTA2017121806434](https://openairdocs.org/sdr/DXTA2017121806434), Dec 18, 2017: DISPLAY. UNSERVICEABLE. DU CAS MESSAGE AND PFD 2 CIRCUIT BREAKER POPPED. STRONG ELECTRICAL ODOR ALSO. CORRECTIVE ACTION: CONFIRMED PFD 2 BREAKER TRIP IMMEDIATELY WITH AVIONICS SWITCH O
- [SDR 2017F00185](https://openairdocs.org/sdr/2017F00185), Nov 2, 2017: SKIN. CORRODED. CORROSION ON UPPER WING SKINS (LEFT AND RIGHT SIDE) ENGINEERING LETTER DQ9925M1.
- [SDR 2017F00186](https://openairdocs.org/sdr/2017F00186), Nov 2, 2017: SKIN. GOUGED. RIGHT WING GOUGE ON UPPER SKIN ENGINEERING LETTER DQ10036M1.
- [SDR 2017FA0000542](https://openairdocs.org/sdr/2017FA0000542), Nov 2, 2017: DOOR FRAME. DEBONDED. REPAIR OF DIS-BOND AREA AROUND NOSE DOOR OPENING ENGINEERING LETTER DQ9996M1.
- [SDR DXTA2017042406400](https://openairdocs.org/sdr/DXTA2017042406400), Apr 24, 2017: UNKNOWN. ODOR. CABIN TEMPERATURE UNABLE TO CONTROL IN AUTO OR MANUAL MODES. CABIN FILLED WITH VISIBLE FUMES. THE FUMES DID NOT SMELL LIKE EITHER PAPER OR ELECTRICAL FIRE.
- [SDR 2016F00222](https://openairdocs.org/sdr/2016F00222), Nov 12, 2016: STIFFENER. CRACKED. REPAIR OF CRACKED RT WING RIB STIFFENER AT CWS 161.40 DATED NOV 8, 2016 AND FAA FORM 8100-9 DATED 11/9/2016.
- [SDR DXTA2015123006147](https://openairdocs.org/sdr/DXTA2015123006147), Dec 29, 2015: UNKNOWN. SMOKE. ON THE GND WITH APU RUNNING FOR ABOUT 5 MINUTES, TAIL CONE BLD LEAK AMBER CAS MSG CAME ON. WITHIN 30 SECONDS COCKPIT & CABIN FILLED WITH SMOKE. INSPECTED TAIL C
- [SDR DXTA2015102906115](https://openairdocs.org/sdr/DXTA2015102906115), Oct 28, 2015: APU. MALFUNCTIONED. AFTER ENGINE START AND WELL AFTER APU SHUTDOWN CABIN FILLED WITH A LIGHT FOG OF SMOKE. REMOVED APU. INSPECTED FIREWALL, MOUNTS, AND SUPPORT STRUCTURE. NO DEFECT
- [SDR DXTA2015090306074](https://openairdocs.org/sdr/DXTA2015090306074), Sep 2, 2015: UNKNOWN. ODOR. UPON RESTART OF APU, THE FADEC MSGS CAME BACK, ALONG WITH A NEW MESSAGE, TAIL CONE BLEED LEAK. WHEN SELECTED THE APU AIR, THERE WAS A STRONG BURNING ODOR IN THE
- [SDR DXTA2014060605796](https://openairdocs.org/sdr/DXTA2014060605796), Jun 5, 2014: UNKNOWN. ODOR. CLIMBING THRU FL 340, DETECTED AN ACRID BURNING ODOR, ONE MINUTE LATER THE FADEC FAULT L A B & R A B CAS MESSAGES CAME ON IN QUICK SUCCESSION. IAW THE CHECKLIST
- [SDR DXTA2013112705583](https://openairdocs.org/sdr/DXTA2013112705583), Nov 27, 2013: COMPUTER. CONTAMINATED. ABORTED TAKEOFF BELOW 60 KTS DUE TO YD KICKING OFF & NO TAKEOFF MESSAGE. WHEN EXITING RUNWAY WE GOT AMBER CAS FADEC FAULT R B THAT WE COULDN'T CLEAR USING AFM P
- [SDR DXTA2013062405423](https://openairdocs.org/sdr/DXTA2013062405423), Jun 22, 2013: APU. LEAKING. SMOKE OUT OF WEMACS WITH BLEED AIR ON HIGH. FOUND OIL PRESENT AT APU INLET. REMOVED LEAKING APU AND INSTALLED A REPAIRED APU. ALL WORK PERFORMED IAW AMM 49-00-0
- [SDR DXTA2012112605195](https://openairdocs.org/sdr/DXTA2012112605195), Nov 26, 2012: O-RING. LEAKING. DURING DECENT, CREW RECEIVED AN AMBER CAS MESSAGE: HYD LEVEL LOW A, HYD SHOWED 16 PERCENT. FOLLOWED EMERGENCY CHECKLIST AND MADE A SAFE LANDING, STOPPING THE AC
- [SDR DXTA2012082105099](https://openairdocs.org/sdr/DXTA2012082105099), Aug 20, 2012: APU. ODOR. FUMES IN CABIN AND COCKPIT, ISOLATED PACS FOR 10 MINUTES BUT COULD NOT TELL ANY DIFFERENCE. FOUND APU LEAKING OIL FROM INLET. INSTALLED REPAIRED APU IAW MM 49-1
- [SDR DXTA2012073005065](https://openairdocs.org/sdr/DXTA2012073005065), Jul 28, 2012: LANDING GEAR. FAILED. AFTER TAKEOFF THE NLG FAILED TO RETRACT. RED UNLOCK LIGHT FOR THE NOSE GEAR STAY ON. LOWER THE MAIN GEAR WE GET 3 GREEN DOWN AND LOCK. BUT THE GEAR STAYS STUCK 
- [SDR DXTA2012072705060](https://openairdocs.org/sdr/DXTA2012072705060), Jul 26, 2012: BEARING. FAILED. AFTER TAKEOFF THE LANDING GEAR FAILED TO RETRACT. THE RED UNLOCK LIGHT REMAINED ON. THE GEAR CONTINUED TO MAKE AIR NOISE. THE GEAR WAS CYCLED ONCE WITH THE SAME
- [SDR DXTA2011071004647](https://openairdocs.org/sdr/DXTA2011071004647), Jul 10, 2011: O-RING. LEAKING. IN CRUISE FLIGHT AT FL400, DURING CRUISE CHECKLIST, NOTED HYD VOL WAS 20 PERCENT AND DECREASING. ONCE HYD VOL A CAS ILLUMINATED FOLLOWED APPROPRIATE CHECKLIST A
- [SDR DXTA2011031104503](https://openairdocs.org/sdr/DXTA2011031104503), Mar 10, 2011: RESOLVER. INOPERATIVE. CLIMBING THROUGH FL200 FLAPS FAIL INDICATOR CAME ON WITH FLAPS INDICATING 0. RAN CHECKLIST AND PUSHED FLAP RESET AT WHICH TIME INDICATOR WENT TO AMBER FLAPS 7 W
- [SDR DXTA2011011804414](https://openairdocs.org/sdr/DXTA2011011804414), Jan 16, 2011: ACTUATOR. MALFUNCTIONED. IN FLIGHT, DURING CLIMBOUT FOR ABOUT 1000' FROM 15,000 TO 16,000 AT AN AIRSPEED OF 300KTS THE UPPER RUDDER BEGAN TO FLUTTER/PULSATE RAPIDLY LT AND RT. AFTER THE
- [SDR DXTA2010112904326](https://openairdocs.org/sdr/DXTA2010112904326), Nov 26, 2010: APU. LEAKING. WHEN PULLING POWER BACK FOR DESCENT, AS SOON AS HP VALVES OPENED, GOT VERY STRONG "LIGHTING A MATCH" ODOR IN THE COCKPIT. R & R APU IAW CMM 49-10-10. OPS & LEAK
- [SDR DXTA2010112904325](https://openairdocs.org/sdr/DXTA2010112904325), Nov 26, 2010: LINE. LEAKING. LEFT BRAKE GRABS HARD WHEN LIGHTLY APPLIED. FOUND LEAKING HYD LINE AT BRAKE FUSE. TIGHTENED & VERIFIED BRAKE HYD PRESSURES AT BRAKE METERING VALVE, RUDDER PEDAL
- [SDR DXTA2010112904324](https://openairdocs.org/sdr/DXTA2010112904324), Nov 26, 2010: APU. ODOR. VERY STRONG FUEL ODOR IN CABIN WITH APU RUNNING. BURNS EYES. SEEMS TO DISSIPATE AFTER APU SHUTDOWN AND ONLY ENGINES RUNNING. REMOVED CABIN & COCKPIT COALESCER S
- [SDR DXTA2010042704077](https://openairdocs.org/sdr/DXTA2010042704077), Apr 26, 2010: STRUT. FAILED. LANDING GEAR WOULD NOT RETRACT DURING INITIAL CLIMB OUT. GEAR HANDLE WILL NOT MOVE FROM THE DOWN POSITION. JACKED ACFT. FOUND NOSE STRUT NOT FULLY EXTENDED. HAN
- [SDR DXTA2009021703509](https://openairdocs.org/sdr/DXTA2009021703509), Feb 16, 2009: ENGINE. MAKING METAL. DURING TAKE OFF ROLL GOT "CHIP DETECT -R" AMBER CAS MESSAGE. ABORTED TAKEOFF. EXAMINED ALL RT ENG MAGNETIC PLUGS FOR PARTICLES. FOUND CHIP, REPLACED OIL FILTER 

## 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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