# N913QS: 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: 680A0334
- Year built: 2022
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 29, 2022
- Certificate issued: May 29, 2026
- Expires: May 31, 2033
- Mode S code: ACA33F
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=913QS
- Page: https://openairdocs.org/aircraft/N913QS

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 N913QS.

## FAA accident and incident reports

None matched to N913QS.

## Reports on N913QS not matched to an aircraft (2)

They name N913QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 20080614834179I](https://openairdocs.org/incident/20080614834179I), Jun 14, 2008: Cessna 750 (N913QS), Omaha, NE, No damage. (-23) N913QS, was enroute form aspen, co to des moines, IA, at flight level 390. The crew reported to air traffic control that they smelled smoke in cockpit.…
- [Incident 20061209026319I](https://openairdocs.org/incident/20061209026319I), Dec 9, 2006: Cessna 750 (N913QS), Wichita, KS. (-23) On December 9, 2006, the flight crew for netjets aviation inc. operating as flight 254-5226-1, departing Wichita Kansas (ict) for sacramento, California,…

## Service difficulty reports (5)

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 DXTA2025041503094](https://openairdocs.org/sdr/DXTA2025041503094), Apr 14, 2025: FILTER. ODOR. COCKPIT ODOR: COCKPIT AIR HAS REALLY BAD ODOR LIKE A DIRTY SOCK CORRECTIVE ACTION: REPLACED CABIN HEPA FILTER. OPS CHECK GOOD. IAW CE680A AMM 21-70-10.
- [SDR DXTA2025011301907](https://openairdocs.org/sdr/DXTA2025011301907), Jan 9, 2025: NONE. NONE. FUSELAGE STRUCTURE: ENCOUNTERED SEVERE TURBULANCE OVER KLIT AT FL390, CLEAN CONFUGURATION, M.75. AIRCRAFT DROPPED MAYBE 20' IN 1/2 SECOND, NO ROLLING MOTION. AL
- [SDR DXTA20240110743](https://openairdocs.org/sdr/DXTA20240110743), Dec 28, 2024: UPLOCK SWITCH. DEFECTIVE. NLG: WHEN RETRACTING THE GEAR, WE GOT THE "GEAR DISAGREE N" CAUTION MESSAGE. RAN THE QRH. GEAR CAME DOWN WITH 3 GREEN. WE DID NIT HAVE TO BLOW THE LANDING GEAR.
- [SDR DXTA2023112010087](https://openairdocs.org/sdr/DXTA2023112010087), Nov 19, 2023: UNKNOWN. UNKNOWN. MAIN CABIN DOOR BINDS AND STICKS WHEN OPENING. PERFORMED OPERATIONAL CHECKS CHECKS AND EVALUATED DOOR AND WAS ABLE TO DUPLICATE FAULT. DOOR ELECTRONICALLY WORKE
- [SDR DXTA2023042784960](https://openairdocs.org/sdr/DXTA2023042784960), Apr 26, 2023: UNKNOWN. UNKNOWN. MAIN DOOR: MAIN CABIN DOOR REMAINS IN THE CLOSED POSITION WHEN THE HANDLE IS OPENED. TO OPEN, IT HAS TO BE PUSHED OPEN. WHEN CLOSING FROM THE OUTSIDE AFTER MOTO

## Service difficulty reports on N913QS not matched to an aircraft (27)

They name N913QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA201503316000](https://openairdocs.org/sdr/DXTA201503316000), Mar 30, 2015: ACM. SEIZED. ON START UP WHEN WE POWERED UP, WE GOT SMOKE IN THE COCKPIT & CABIN. VERIFIED THAT THE CABIN ACM IS STARTING TO SEIZE AT THE PROPELLER SHAFT, COCKPIT ACM FOUND 
- [SDR DXTA2014092205891](https://openairdocs.org/sdr/DXTA2014092205891), Sep 2, 2014: SKIN. CORRODED. LEFT & RIGHT MUTABLE WING FUEL BAY PANELS LAND HAVE CORROSION ON LAND & ON UPPER SURFACE OF LOWER SKIN. REPAIRED IAW S-750-0113 23RD.
- [SDR DXTA2014090205870](https://openairdocs.org/sdr/DXTA2014090205870), Sep 1, 2014: APU. MALFUNCTIONED. SMOKY & OILY SMELL COMING FROM ENVIRONMENTAL SYS. SMELL OCCURS WITH BOTH COCKPIT & OR CABIN PACS. NO VISIBLE SMOKE IS OBSERVED. REMOVED & REPLACED APU WITH CUST
- [SDR DXTA2014082405867](https://openairdocs.org/sdr/DXTA2014082405867), Aug 25, 2014: SKIN. CORRODED. CORROSION WAS FOUND AT SEVERAL LOCATIONS ON THE LT & RT WING LOWER SKINS LOCATED AT 522AB, 621HB & 622EB. VERIFIED CORROSION REMOVAL IAW 750 NONDESTRUCTIVE TEST
- [SDR DXTA2013070505431](https://openairdocs.org/sdr/DXTA2013070505431), Jul 3, 2013: BRAKE SYS. MALFUNCTIONED. ON LANDING, TAKING EXCESSIVE BRAKE PRESSURE TO STOP. NO PULLING LT OR RT, FLUID QUANTITY GOOD, BRAKE WEAR PINS GOOD. HAD DIFFICULTY SETTING PARKING BRAKE. HAD T
- [SDR DXTA2012052904981](https://openairdocs.org/sdr/DXTA2012052904981), May 25, 2012: UNKNOWN. ODOR. ON DESCENT DETECTED A BURNING ODOR. F/O WENT BACK AND DETECTED THE BURNING ODOR MORE INTENSELY. NO SMOKE OBSERVED. LANDED UNEVENTFULLY. CLEANED BOTH SOCKS & WAT
- [SDR DXTA2011012404426](https://openairdocs.org/sdr/DXTA2011012404426), Jan 21, 2011: UPLOCK SWITCH. MALFUNCTIONED. GEAR UNSAFE LIGHT REMAINED ON AFTER HANDLE WAS RAISED. R & R LT MAIN GEAR UPLOCK SWITCH IAW MM 32-30-05.
- [SDR DXTA2010061404122](https://openairdocs.org/sdr/DXTA2010061404122), Jun 11, 2010: GCU. FAILED. WHILE IN CLIMB, WE HAD THE LT GENERATOR AMBER CAS MESSAGE. RAN CHECKLIST. A FEW MINUTES LATER WE HAD MULTIPLE AMBER CAS MESSAGE, NR 1, 2 AND 3 TUBES WENT BLACK 
- [SDR DXTA2009061503687](https://openairdocs.org/sdr/DXTA2009061503687), Jun 14, 2009: ACM. SEIZED. SWEET SMOKE ODOR IN COCKPIT IN CRUISE AT FL430. NO VISIBLE SMOKE. NO PAX SMOKING. EMERGENCY DESCENT TO LANDING PERFORMED. PAX DIDN'T DETECT ANYTHING. FOUND COCK
- [SDR DXTA200803226](https://openairdocs.org/sdr/DXTA200803226), Aug 17, 2008: WHEEL. VIBRATION. STRONG NOSE WHEEL SHIMMY ON TAKEOFF. ABORTED TAKEOFF. (S)
- [SDR DXTA200808153226](https://openairdocs.org/sdr/DXTA200808153226), Aug 15, 2008: WHEEL. OUT OF BALANCE. STRONG NOSE WHEEL SHIMMY ON TAKEOFF. PREVIOUS HISTORY SHOWED NOSE WHEEL UNDER TORQUED AND REPLACED, UPPER AND LOWER WERE REPLACED. BOTH NOSE TIRES HAD NO FLATS 
- [SDR DXTA200803165](https://openairdocs.org/sdr/DXTA200803165), Jul 9, 2008: SCISSOR LINK. DAMAGED. DURING TAKE OFF AT 40 KTS A SEVERE SHIMMY VIBRATION AT THE NOSE WHEEL THRU 55 KTS. IT WAS SO SEVERE THAT IT KICKED THE YD LOWER. TAKEOFF GROSS WEIGHT 30,773. FU
- [SDR DXTA200803121](https://openairdocs.org/sdr/DXTA200803121), Jun 14, 2008: A/C PACK. ODOR. AT FL390 DETECTED SMOKE AND PERFORMED AND EMERGENCY DECENT AND DIVERTED TO OMA. NO VISIBLE SMOKE UNTIL PACKS OFF. A HAZE DEVELOPED. REPLACED AFT ACM TURBINE REM
- [SDR DXTA200803109](https://openairdocs.org/sdr/DXTA200803109), Jun 9, 2008: SWITCH. OUT OF ADJUST. NOSE DOOR OPEN L MESSAGE DISPLAYED AFTER TAKEOFF AT GEAR RETRACTION. ADJUSTED DOOR WARNING SWITCHES IAW MM 52-70-00 OPS CHECK GOOD.
- [SDR DXTA200803092](https://openairdocs.org/sdr/DXTA200803092), Jun 3, 2008: WHEEL. VIBRATION. TAKE OFF ABORTED DUE TO SEVERE NOSE WHEEL SHIMMY AND VIBRATION. R&R BOTH NOSE TIRE & WHEEL ASSY'S IAW MM 32-41-00 TAXI CHECK GOOD.
- [SDR DXTA200802819](https://openairdocs.org/sdr/DXTA200802819), Jan 31, 2008: COMPUTER. INOPERATIVE. AT FL410 GOT AMBER PRI STAB TRIM FAIL. TROUBLESHOT TO NR1 (LT) IAC, REMOVED REPLACED AND OPS CHECK GOOD, NR1(LT) IAC IAW MM 34-25-01 NO OTHER DEFECTS NOTED.
- [SDR DXTA200702500](https://openairdocs.org/sdr/DXTA200702500), Sep 26, 2007: LAMP. BURNED OUT. LT PANEL LIGHTING C/B POPPED WITH BURNING INSULATION ODOR UPON ACTIVATION OF DAY/ NIGHT DIM SWITCH PRIOR TO ENGINE START. KPHL CHECKED AND LT PANEL LTS AND CB O
- [SDR DXTA200702312](https://openairdocs.org/sdr/DXTA200702312), Jul 1, 2007: ACM. LEAKING. EXTREME SULPHUR FUMES IN COCKPIT AND CABIN AT FL390, BOTH PACS IN NORM, BOTH TEMP SELECT IN AUTO, ENROUTE TIME 60 MINUTES. FUMES DISIPATED DURING DESCENT. DECLA
- [SDR DXTA200702254](https://openairdocs.org/sdr/DXTA200702254), Jun 10, 2007: PTU. INOPERATIVE. HYD A PRESSURE DROPPED TO 2000 PSI, FOLLOWED BY AMBER CAS (HYD LOW QTY B) AND (HYD O TEMP B) MESSAGES ILLUMINATED. REMOVED & REPLACED PTU, LH ENGINE DRIVEN HYD.
- [SDR 2006FA0001233](https://openairdocs.org/sdr/2006FA0001233), Dec 9, 2006: CONNECTOR. SHORTED. BATTERY OVERTEMP INDICATED R-RED CAS MESSAGE IN FLIGHT. FOUND SPLICE AT THE BATTERY TEMP SENSOR CONNECTOR PY044 BROKEN. ALSO CONNECTOR WAS FOUND BADLY CORRODED 
- [SDR DXTA200601801](https://openairdocs.org/sdr/DXTA200601801), Dec 9, 2006: CONNECTOR. CORRODED. BATT O'TEMP RIGHT RED CAS MESSAGE ILLUMINATED IN FLIGHT. REMOVED AND REPLACED CONNECTOR PY044 & REPLACED WIRES IAW CE750 W/M CH 20-10-06. OPS CHECKED GOOD.
- [SDR DXTA200601531](https://openairdocs.org/sdr/DXTA200601531), Jul 31, 2006: ACM. SEIZED. CABIN PAC OVERHEAT WHILE USING AIR CONDITIONING FROM THE APU ON THE GROUND. SMOKE FILLED THE CABIN, APU AND PAC WAS SHUT DOWN DURING FLIGHT FROM IAD TO ADS. INS
- [SDR DXTA200501144](https://openairdocs.org/sdr/DXTA200501144), Dec 15, 2005: ANTI-ICE SYSTEM. FAILED. ANTI-ICE ON BEFORE TAKEOFF RECEIVED NO COLD MESSAGES POWER TO TAKEOFF DETENT GOT 'SLAT COLD' MSG AND 'HOT STAB' MSG. ABORTED, SHUT DOWN ANTI-ICING AND ALLOWED T
- [SDR DXTA200501020](https://openairdocs.org/sdr/DXTA200501020), Oct 12, 2005: WARNING LIGHT. ILLUMINATED. AFTER TAKEOFF, GREEN NOSE WHEEL DOWN INDICATOR LIGHT REMAINING ON. NO RED UNLOCK INDICATOR, AND NO AUDIBLE GEAR OR GEAR DOOR NOISE. GEAR EXTENDED NORMALLY, NORM
- [SDR DXTA200500913](https://openairdocs.org/sdr/DXTA200500913), Aug 18, 2005: AUTOPILOT SYS. MALFUNCTIONED. ARRIVING 180 KNOTS, AUTO-PILOT REPEATEDLY CAME OFF-LINE. ELEV FELT HEAVY ON CONTROLS. AT 140 KNOTS, PRIMARY TRIM WOULD NOT WORK. NO CAS MESSAGES RECEIVED EXCEPT
- [SDR DXTA200500728](https://openairdocs.org/sdr/DXTA200500728), May 18, 2005: CONTROL CABLE. OUT OF ADJUST. AIRCRAFT ROLLS RIGHT DURING CRUISE. AILERON TRIM IS ROLLED OVER HALFWAY TO HOLD LEVEL FLIGHT. RUDDER TRIM IS ALSO TO LEFT OF CENTER. CONTROL RIGGING NEEDS TO BE
- [SDR DXTA200400332](https://openairdocs.org/sdr/DXTA200400332), Jul 6, 2004: ODOR. DETECTED. ALL WEMAC EMITTED A STRONG SULFUR SMELL INTERMITTENTLY IN DIFFERENT VALVE AND PAC POSITIONS, AS A RESULT CANNOT DETERMINE SOURCE. RAN ENGINES AND APU, USED BLEE

## 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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