# N662QS: 2021 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: 680A0274
- Year built: 2021
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 2, 2021
- Certificate issued: October 8, 2026
- Expires: October 31, 2033
- Mode S code: A8BD16
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=662QS
- Page: https://openairdocs.org/aircraft/N662QS

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 N662QS.

## NTSB investigations on N662QS not matched to an aircraft (2)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB ERA13IA114](https://openairdocs.org/ntsb/ERA13IA114), Jan 13, 2013: Cessna 560XL (N662QS), Debary, FL, incident, no damage. Probable cause: An accumulation of debris in the airplane’s bilge drain holes that prevented accumulated moisture from properly draining; the accumulated moisture subsequently froze around the elevator control…
- [NTSB ERA10IA285](https://openairdocs.org/ntsb/ERA10IA285), May 28, 2010: Cessna 560XL (N662QS), White Plains, NY, incident, minor damage. Probable cause: The flight crew's failure to ensure that the cabin door was secured/locked prior to takeoff.

## FAA accident and incident reports

None matched to N662QS.

## Reports on N662QS not matched to an aircraft (3)

They name N662QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 20130113001929I](https://openairdocs.org/incident/20130113001929I), Jan 13, 2013: Cessna 560XL (N662QS), Peachtree City, GA, No damage. Climbing out of FL350 in known icing (-23C, 1000 feet per minute, autopilot engaged, wing/engine anti-ice on), the aircraft suddenly pitched nose down. Upon…
- [Incident 20100528054029I](https://openairdocs.org/incident/20100528054029I), May 28, 2010: Cessna 560XL (N662QS), White Plains, NY, Minor damage. The SIC recalls closing the door after the two passengers had boarded. The crew indicated that the taxi was short and there was a wait of about ten minutes…
- [Incident 20070628827329I](https://openairdocs.org/incident/20070628827329I), Jun 28, 2007: Cessna 560XL (N662QS), Toledo, OH, Minor damage. (-23) While climbing through 5000 feet, shortly after take-off, a large portion of the upper cowling of the l/h engine broke apart from the aircraft. Only two…

## 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 DXTA2026092109770](https://openairdocs.org/sdr/DXTA2026092109770), Sep 17, 2026: LATCH. OUT OF RIG. CABIN DOOR HANDLE VERY HARD TO MOVE. GETS STUCK ABOUT HALF WAY POINT AND REQUIRES LOTS OF FORCE TO FULLY LOCK. RERIGGED CABIN DOOR LATCH STRIKER. OPS CHECK GOOD
- [SDR DXTA2026091609711](https://openairdocs.org/sdr/DXTA2026091609711), Sep 14, 2026: STRIKER. LOOSE. WHILE TRYING TO CLOSE THE MAIN CABIN DOOR THE LEVER SEEMS TO BE BINDING UP. MORE THAN NORMAL FORCE IS REQUIRED TO PULL THE LEVER DOWN TO LOCK THE MAIN DOOR. COR
- [SDR DXTA2026060908388](https://openairdocs.org/sdr/DXTA2026060908388), Jun 9, 2026: DOOR. NO DISCREPANCY. CLOSING THE MAIN CABIN DOOR, THE HANDLE IS VERY STIFF. IT DOES CLOSE FLUSHED WITH THE FUSELAGE, AND ALL LOCKING PIN ARE BEING ENGAGED. JUST SEEMS TO BE A LOT OF
- [SDR DXTA2025032102767](https://openairdocs.org/sdr/DXTA2025032102767), Mar 20, 2025: RUB BLOCK. OUT OF ADJUST. MAIN DOOR: MAIN ENTRY DOOR BINDS WHEN OPENING. DOOR NEEDS TO BE ASSISTED TO OPEN. CORRECTIVE ACTION; ADJUSTED SHIMS OF FWD MED DOOR RUB BLOCK TO PROPER LIMITS. 
- [SDR DXTA2024091000472](https://openairdocs.org/sdr/DXTA2024091000472), Sep 8, 2024: CIRCUIT BOARD. FAULTED. CABIN ODOR: VERY STRONG BURNING SMELL INSIDE AIRCRAFT AT 5K FT... THE PASSENGER SMELLED IT AS WELL. AFTER ENGINE SHUT DOWN, AE OPENED THE REAR EQUIPMENT BAY AND
- [SDR DXTA2024052311843](https://openairdocs.org/sdr/DXTA2024052311843), May 22, 2024: CONTROLLER. FAILED. DURING PRESSURIZATION FAILURE, PASSENGER OXYGEN MASKS DEPLOYED. THERE WERE NO PASSENGERS ON BOARD. REMOVED CABIN PRESSURIZATION CONTROLLER AND REPLACED WITH CUS
- [SDR 2023FA0000338](https://openairdocs.org/sdr/2023FA0000338), Jun 23, 2023: RETAINER. CHAFED. ESCAPE HATCH SEAL RETAINER SCREWS ARE MAKING CONTACT WITH BOTH FWD AND AFT LOWER FUSELAGE EMERGENCY ESCAPE HATCH DOOR FRAME CAUSING DAMAGE TO THE FWD SIDE OF TH
- [SDR 2023FA0000337](https://openairdocs.org/sdr/2023FA0000337), Jun 23, 2023: SHIELD. CHAFED. INNER STINGER SKIN DAMAGE TO L/H SKIN P/N 6912640-20 AND R/H SKIN 6912640-24, REF ENGINEERING MEMO DQ40101M1.
- [SDR DXTA2023061488720](https://openairdocs.org/sdr/DXTA2023061488720), Jun 14, 2023: UNKNOWN. UNKNOWN. MAIN DOOR: PIN FELL OUT ON MAIN CABIN DOOR LINKAGE. UNABLE TO CLOSE DOOR USING POWER ASSIST. FOUND PIN. TRIED TO REINSTALL, BUT APPEARS THREADS APPEAR TO BE STR

## Service difficulty reports on N662QS not matched to an aircraft (21)

They name N662QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA2018090401375](https://openairdocs.org/sdr/DXTA2018090401375), Aug 31, 2018: SHUTOFF VALVE. FAULTY. DURING TAKE OFF 10KTS BEEFIER V1 AIRCRAFT PULLED HARD RIGHT, CORRECTED WITH FULL LEFT RUDDER MAINTAINED CONTROL, ROTATED MADE NORMAL CLIMB, CRUISE, DESCENT, LAN
- [SDR JGVR201806132003](https://openairdocs.org/sdr/JGVR201806132003), Jun 12, 2018: FITTING. CORRODED. MECHANICALLY BLENDED FOUR AREAS OF CORROSION ON THE LT WING OTBD FLAP PUSHROD ATTACH FITTINGS, PERFORMED AN EDDY CURRENT INSPECTION AND AN ULTRASONIC THICKNESS 
- [SDR JGVR20180613002](https://openairdocs.org/sdr/JGVR20180613002), Jun 12, 2018: AXLE. CORRODED. FOUND THE LEFT MAIN LANDING GEAR AXLE CORRODED OUT OF LIMITS, REPLACED THE AXLE.
- [SDR JGVR20180612001](https://openairdocs.org/sdr/JGVR20180612001), Jun 12, 2018: ACCESS PANEL. CORRODED. CORROSION FOUND UNDERNEATH THE ACCESS PANEL 340CR, LOWER AFT ON THE RT SIDE OF THE VERTICAL STAB. BLENDED THE CORROSION, CLEANED, CHEMICALLY TREATED, AND PRIMED
- [SDR DXTA2015042006010](https://openairdocs.org/sdr/DXTA2015042006010), Apr 18, 2015: APU. SMOKE. SMOKE IN THE COCKPIT. APU WAS STARTED ABOUT FIVE MINUTES PRIOR TO LANDING & WAS OPERATING NORMALLY. UPON LANDING & TAXI IN APU QUIT DURING ENG SHUTDOWN. WE THOU
- [SDR DXTA2013072205452](https://openairdocs.org/sdr/DXTA2013072205452), Jul 19, 2013: BOLT. WORN. WITH SPEED SLOWLY ACCELERATING PAST 265 KIAS AND IN CLIMB THROUGH FL235, A DEFINITE RUMBLING VIBRATION WAS FELT IN THE ACFT. NO SIGNIFICANT VIBRATION IN YOKE, B
- [SDR DXTA2013011805249](https://openairdocs.org/sdr/DXTA2013011805249), Jan 13, 2013: PULLEY. DAMAGED. DURING CLIMB OUT, ACFT SUDDENLY PITCHED NOSE DOWN. ON DETECTING THE PITCH CHANGE, AUTOPILOT WAS DISENGAGED. CONTROLS WERE DIFFICULT TO MOVE ALONG VERTICAL AXIS 
- [SDR CWQR20110901018](https://openairdocs.org/sdr/CWQR20110901018), Sep 1, 2011: CONTROL CABLE. FRAYED. FRAYED ELEVATOR TRIM CABLE WAS FOUND DURING A SCHEDULED INSP CABLE WAS FRAYED A HALF OF THE CABLE'S DIAMETER. AND CABLE TENSION WAS WITHIN MM LIMITS.
- [SDR DXTA2011042504557](https://openairdocs.org/sdr/DXTA2011042504557), Apr 24, 2011: BRAKE ASSY. MALFUNCTIONED. WHILE TAXIING THE BRAKES WERE APPLIED ON THE RT (CO-PILOTS) SIDE, THEY GRABBED ABRUPTLY & PULLED TO ONE SIDE & WOULDN'T RELEASE RIGHT A SECOND TRY PRODUCED SIMI
- [SDR DXTA2011010504395](https://openairdocs.org/sdr/DXTA2011010504395), Jan 4, 2011: WHEEL. SEPARATED. NOSE WHEEL RIM ASSY SEPARATED WHILE BEING SERVICED. TECH USED HIGH PRESSURE TO SERVICE TIRE WITH NO REGULATOR. WHEEL & ATTACHING HARDWARE ARE UNSERVICEABLE. INS
- [SDR DXTA2010102804277](https://openairdocs.org/sdr/DXTA2010102804277), Oct 27, 2010: DISPLAY. MALFUNCTIONED. ON CLIMB OUT, CO-PILOT'S PFD NR 2 WENT BLANK FOR 5 - 6 SECONDS, WITH CHECK PFD NR 2 ANNUNCIATOR ILLUMINATED & MASTER CAUTION. SCREEN CAME BACK ON WITH RED X FOR
- [SDR DXTA201006014106](https://openairdocs.org/sdr/DXTA201006014106), May 28, 2010: DOOR. FAILED. MAIN ENTRY DOOR HISS ON CLIMB OUT, DOOR OPENED IN FLIGHT UPON RETURN TO AIRPORT. NO DEFECTS WERE NOTED WITH THE DOOR LATCHING/WARNING SYS. NTSB INVESTIGATION IN
- [SDR DXTA2010031504030](https://openairdocs.org/sdr/DXTA2010031504030), Mar 13, 2010: OIL SYSTEM. READS HIGH. AT CLIMB TO FL370. RT ENGINE OIL PRESSURE EXCEEDED RED LINE TO 190/200PSI. REDUCED THROTTLE & BEGAN TO DESCEND. AT FLT IDLE, OIL PSI STAYED ABOVE RED LINE UNTIL
- [SDR DXTA200808043215](https://openairdocs.org/sdr/DXTA200808043215), Aug 4, 2008: INDICATOR. FALSE INDICATION. AFTER BRAKE RELEASE, LT ITT GAUGE WENT OFF SCALE HIGH. TAKEOFF WAS ABORTED AT LESS THAN 20 KNOTS. PRIOR TO BRAKE RELEASE, ALL ENGINE GAUGES RAD NORMAL AT FULL P
- [SDR DXTA200807193188](https://openairdocs.org/sdr/DXTA200807193188), Jul 19, 2008: COALESCER BAG. CONTAMINATED. JUST PRIOR TO LEVEL OFF AT 15,000 FT, WE STARTED SMELLING A STRONG "BURNING" ODOR. AT LEVEL OFF, WITH POWER REDUCED, THE ODOR DISSIPATED. IT RECURRED ON APPROAC
- [SDR DXTA20083188](https://openairdocs.org/sdr/DXTA20083188), Jul 19, 2008: UNKNOWN. ODOR. JUST PRIOR TO LEVEL OFF AT 15,000 FT, STARTED SMELLING A STRONG "BURNING" ODOR. AT LEVEL OFF, WITH POWER REDUCED, THE ODOR DISSIPATED. ODOR RECURRED ON APPROACH
- [SDR DXTA200701865](https://openairdocs.org/sdr/DXTA200701865), Jan 19, 2007: CIRCUIT BREAKER. OPEN. DURING TAKEOFF PRIOR TO V1, LT SIDE MASTER WARNING LIGHT CAME ON STEADY. RT SIDE MASTER WARNING DID NOT COME ON AT ALL. (WILL NOT RESET) ALL OTHER INDICATIONS N
- [SDR DXTA200601598](https://openairdocs.org/sdr/DXTA200601598), Sep 11, 2006: UPLOCK SWITCH. OUT OF RIG. THE RED 'GEAR UNLOCKED' LIGHT WOULD NOT EXTINGUISH AFTER GEAR RETRACTION. RIGGED NOSE GEAR UPLOCK SWITCH FOR POSITIVE ACTUATION. COMPLETED SATISFACTORY FUNCTION
- [SDR DXTA200501155](https://openairdocs.org/sdr/DXTA200501155), Dec 22, 2005: FUEL FILTER. BYPASSING. RIGHT FUEL FILTER BYPASS LIGHT CAME ON WITH APPLICATION OF T/O POWER DURING TAKEOFF ROLL. REMOVED AND REPLACED RIGHT FUEL FILTER IAW P&W 545 M/M CH 73-10-05, OP
- [SDR DXTA200501042](https://openairdocs.org/sdr/DXTA200501042), Oct 28, 2005: FORK. MALADJUSTMENT. A -GEAR UNLOCK- LIGHT REMAINED ON AFTER TAKEOFF WITH THE GEAR IN THE -UP POSITION-, THE -HYD PRESS- LIGHT REMAINED ON AS WELL. REMOVED NLG STRUT PISTON ASSY. FO
- [SDR DXTA200500624](https://openairdocs.org/sdr/DXTA200500624), Mar 11, 2005: SUPPORT BRACKET. DAMAGED. NO TAKEOFF LIGHT AND HORN CAME ON AT TAKEOFF POWER AND TAKEOFF ROLL INITIATION. FLAPS 15, SPEED BRAKE RETRACTED, TRIMS SET FOR T/O). FOUND RT SPEED BRAKE SWITCH

## 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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