# N696QS: 2019 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: 680A0227
- Year built: 2019
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 15, 2019
- Certificate issued: November 24, 2025
- Expires: November 30, 2032
- Mode S code: A9426F
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=696QS
- Page: https://openairdocs.org/aircraft/N696QS

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 N696QS.

## FAA accident and incident reports

None matched to N696QS.

## Reports on N696QS not matched to an aircraft (1)

They name N696QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 20030217007779I](https://openairdocs.org/incident/20030217007779I), Feb 17, 2003: Cessna 560XL (N696QS), Washington, DC, Minor damage. (-23) Reported snow depth was 1 inch of packed. Previous aircraft reported extremely poor conditions, and had problems being pulled to the left. Maintenance…

## Service difficulty reports (22)

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 DXTA2026060508327](https://openairdocs.org/sdr/DXTA2026060508327), Jun 2, 2026: ACTUATOR. FAULTED. ON TAKEOFF JUST AFTER POWER WAS SET, NOSE PULLED HARD TO THE LT. LT RUDDER PEDAL ALSO WENT FULL. CORRECTED WITH RIGHT RUDDER & ABORTED TAKE OFF. RUDDER BIAS CHE
- [SDR DXTA2025102805459](https://openairdocs.org/sdr/DXTA2025102805459), Oct 26, 2025: HOSE. LEAKING. UPON REACHING END OF RUNWAY 34 WE HEARD A THUD WHEN SETTING PARKING BREAK AND GOT A PARK BRAKE LOW PRESS AMBER CAS MESSAGE. THERE WAS A PUDDLE UNDER RIGHT MAIN 
- [SDR DXTA2025022402441](https://openairdocs.org/sdr/DXTA2025022402441), Feb 20, 2025: BATTERY PACK. NO TEST. ALL INTERIOR AND EXTERIOR LIGHTS ASSOCIATED WITH BATTERY PACK #3 FAIL TO ILLUMINATE WITH PREFLIGHT TEST AND ASSOCIATED QRH CHARGING PROCEDURE WITH 60 MINUTES OF
- [SDR DXTA2024110501041](https://openairdocs.org/sdr/DXTA2024110501041), Nov 3, 2024: BATTERY PACK. FAULTY. DURING PRE-FLIGHT WITH THE AIRCRAFT BATTERIES OFF AND ALL GEN SOURCES OFF AND THE EMER LIGHT SWITCH IN ARM, ONLY SOME OF THE INTERIOR LIGHTS WERE ILLUMINATED. W
- [SDR DXTA2024100700767](https://openairdocs.org/sdr/DXTA2024100700767), Oct 5, 2024: BUSHING. OUT OF ADJUST. MAIN DOOR: EVALUATE MAIN ENTRY DOOR FOR PROPER ADJUSTMENT. IN THE OPEN POSITION, FORWARD HINGE AREA APPEARS TO RUB. MED HAS NORMAL FUNCTION IN ALL OTHER RESPECT
- [SDR DXTA2024091700567](https://openairdocs.org/sdr/DXTA2024091700567), Sep 16, 2024: SEAL. DIRTY. MAIN DOOR: MAIN DOOR BINDS WHEN CLOSING AND WILL NOT OPEN FREELY. I HAVE TO FORCE THE DOOR TO MAKE IT FREE FALL CORRECTIVE ACTION: CLEANED MAIN DOOR SEALS AND S
- [SDR DXTA2024091200508](https://openairdocs.org/sdr/DXTA2024091200508), Sep 10, 2024: BATTERY PACK. NO TEST. EMERGENCY LIGHT FAILED POST FLIGHT SEAT 3 AND OVERWING RIGHT SIDE. SEE PREVIOUS WRITE UP REPLACED #2 EMERGENCY BATTERY PACK REF. CE680A MM 33-50-00 & 33-50-06. 
- [SDR DXTA2024090900458](https://openairdocs.org/sdr/DXTA2024090900458), Sep 6, 2024: BATTERY PACK. DEFECTIVE. EMERGENCY LIGHTING: DURING EMER LIGHT CHECK IN ARM. NO EMER LIGHTS WORK. WITH EMER LIGHT SWITCH ON. EXIT LIGHT OVER MAIN DOOR NOT ON. OVERHEAD AT SEAT 3 AND 10 
- [SDR DXTA2024082600317](https://openairdocs.org/sdr/DXTA2024082600317), Aug 24, 2024: DOOR. OUT OF TOLERANCE. MAIN DOOR: MAIN ENTRY DOOR IS BINDING AND FAILS TO OPEN ON ITS OWN. IT ONLY OPENS ABOUT 1" AND THEN HAS TO BE PULLED/PUSHED BEYOND THAT POINT. CORRECTIVE ACTION
- [SDR DXTA2024070812288](https://openairdocs.org/sdr/DXTA2024070812288), Jul 7, 2024: BRAKE. FAULTED. LEFT MLG BRAKE GRABBING & MAKING A GRINDING NOISE AFTER LANDING & TAXI IN. SINGLE POINT JACKED LT MLG TO ROTATE NR 1 WHEEL ASSEMBLY & IT ONLY MADE IT ONE & A HA
- [SDR DXTA2023120410223](https://openairdocs.org/sdr/DXTA2023120410223), Dec 2, 2023: SWITCH. DAMAGED. ON TAXI OUT CABIN DOOR OPEN APPEARED. RAN THE QRH AND MESSAGE DID NOT CLEAR. FOUND INNER HANDLE PUSH BUTTON WIRING OPEN TO GROUND. REPAIRED BROKEN WIRE AT SPLIC
- [SDR DXTA2023080192050](https://openairdocs.org/sdr/DXTA2023080192050), Aug 1, 2023: UNKNOWN. UNKNOWN. CABIN EMERG LIGHT: NONE OF THE CABIN EMER LIGHTS WILL ILLUMINATE WITH THE EMER LTS SWITCH IN THE ON POSITION. CABIN EMER LIGHTS WILL ILLUMINATE AS EXPECTED WITH
- [SDR DXTA2023070790380](https://openairdocs.org/sdr/DXTA2023070790380), Jul 5, 2023: CHARGER. DEFECTIVE. LIGHTS TESTED NORMAL FIRST FLIGHT OF DAY YESTERDAY & TODAY. WHILE IN MDW, ANOTHER LATITUDE CAPTAIN ASKED TO CHECK EMER LIGHTS TO COMPARE BRIGHTNESS, TURNED OUR 
- [SDR DXTA2023070690380](https://openairdocs.org/sdr/DXTA2023070690380), Jul 5, 2023: UNKNOWN. UNKNOWN. CABIN EMERG LIGHT: TESTED NORMAL FIRST FLIGHT OF DAY YESTERDAY AND TODAY. WHILE IN MDW, ANOTHER LATITUDE CAPTAIN ASKED IF HE COULD CHECK EMER LIGHTS TO COMPARE 
- [SDR DXTA2023061288420](https://openairdocs.org/sdr/DXTA2023061288420), Jun 12, 2023: UNKNOWN. UNKNOWN. CO-PILOT SIDE, RIGHT WINDSCREEN IS CRACKED. PICTURES ATTACHED.
- [SDR DXTA2023021780660](https://openairdocs.org/sdr/DXTA2023021780660), Feb 16, 2023: BATTERY. INOPERATIVE. EMERGENCY LIGHTS BATTERY: EMERGENCY BATTERY PACK TWO ASSOCIATED LIGHTS ARE NOT ILLUMINATING DURING PREFLIGHT CHECK///SIGN OFF/// REMOVED #2 EMERGENCY BATT PACK,
- [SDR DXTA2022123077420](https://openairdocs.org/sdr/DXTA2022123077420), Dec 29, 2022: MODULE. DEFECTIVE. LANDING GEAR BLOWDOWN BOTTLE SERVICE: UPON LANDING, GEAR WOULD NOT EXTEND. YELLOW DN WAS DISPLAYED ON GEAR ICAS ALONG WITH GEAR DISAGREE CAS MESSAGE. RAN QRH, B
- [SDR DXTA2022112274490](https://openairdocs.org/sdr/DXTA2022112274490), Nov 22, 2022: UPLOCK SWITCH. DAMAGED. 25 MINUTES INTO FLIGHT LEVELING OFF AT 39000, HEARD & FELT A BUMP IN NOSE GEAR. FOLLOWED IMMEDIATELY BY NOSE GEAR INDICATOR GOING TO YELLOW CROSSHATCHINGS. FOLL
- [SDR DXTA2022092671100](https://openairdocs.org/sdr/DXTA2022092671100), Sep 25, 2022: MODULE. DEFECTIVE. FLAPS FAIL AMBER CAS: WHEN FLAP RETRACTION WAS ATTEMPTED AFTER TAKEOFF, AMBER FLAPS FAIL CAS MESSAGE ILLUMINATED. FLAP HANDLE WAS AT UP AND FLAPS WERE INDICATIN
- [SDR DXTA2022032258830](https://openairdocs.org/sdr/DXTA2022032258830), Mar 21, 2022: BATTERY. DEFECTIVE. EMERG EXIT SIGN/LIGHT: MAIN ENTRY DOOR EXIT SIDE WILL NOT EXTINGUISH. SEAT 10 EMER LIGHT IS ALSO ON. // SIGNOFF// REMOVED FAULTY #1 EMERGENCY BATTERY AND REPLAC
- [SDR 2022F00016](https://openairdocs.org/sdr/2022F00016), Dec 6, 2021: NONE. CHIPPED. CHIPPED PLATING ON RIGHT MAIN LANDING GEAR AXLE P/N 6741032-5. ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ32727M1 REV. B DATED DECEMBER 6, 2021; 680A-02
- [SDR DXTA2020031603585](https://openairdocs.org/sdr/DXTA2020031603585), Mar 14, 2020: BYPASS SWITCH. MALFUNCTIONED. FUEL FLTR BYPASS L AMBER CAS ILLUMINATED - IN CRUISE FLIGHT DURING LEFT TANK TO RIGHT ENGINE CROSSFEED: "FUEL FILTER BYPASS L" AMBER CAS MESSAGE ILLUMINATED. CR

## Service difficulty reports on N696QS not matched to an aircraft (18)

They name N696QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA2017042306399](https://openairdocs.org/sdr/DXTA2017042306399), Apr 23, 2017: ENGINE. POWER LOSS. WITH EEC IN MANUAL, TAKEOFF POWER OBTAINED. DURING CLIMB, NOTICED LARGE THROTTLE SPLIT AND NOTICED THAT THE LEFT ENGINE NOT DEVELOPING TAKEOFF THRUST. CONTINUED
- [SDR CWQR20160720022](https://openairdocs.org/sdr/CWQR20160720022), Jul 20, 2016: CABLE. BROKEN. THIS CABLE ASSEMBLY IS REPLACED AT THE AIRCRAFT OPERATOR REQUEST BECAUSE OF RELIABILITY ISSUES. INSPECTED CABLE AFTER REMOVAL, PREFORMED LOOP TEST AND FOUND TO 
- [SDR CWQR20160720021](https://openairdocs.org/sdr/CWQR20160720021), Jul 20, 2016: CABLE. FRAYED. THIS CABLE ASSEMBLY IS REPLACED AT THE AIRCRAFT OPERATOR REQUEST BECAUSE OF RELIABILITY ISSUES. INSPECTED CABLE AFTER REMOVAL, PREFORMED LOOP TEST AND FOUND TO 
- [SDR CWQR20160701020](https://openairdocs.org/sdr/CWQR20160701020), Jul 1, 2016: HOSE. BLOWN. DURING A SCHEDULED MAINTENANCE GEAR SWING THE RT GEAR UP-LOCK HOOK EXTEND HOSE ASSY, BLEW A HOLE IN IT ABOUT .5 INCH FROM THE SWEDGED FITTING HOSE END. THIS IS 
- [SDR DXTA2015051906020](https://openairdocs.org/sdr/DXTA2015051906020), May 18, 2015: COALESCER BAG. ODOR. MILDEW SMELL AT FLIGHT LEVEL 410. R & R WATER SEPARATOR CONDENSER SOCK IAW AMM 21-51-00. OPS & LEAK CHECKED GOOD.
- [SDR DXTA2014020505639](https://openairdocs.org/sdr/DXTA2014020505639), Feb 4, 2014: BRAKE SYS. CONTAMINATED. UPON LANDING BRAKES WERE EVENLY APPLIED BUT ASYMMETRICAL BRAKING WAS EXPERIENCED, ACFT PULLED TO THE LT, BRAKES WERE RELEASED & ACFT DIRECTION OF TRAVEL WAS COR
- [SDR DXTA2013100705530](https://openairdocs.org/sdr/DXTA2013100705530), Sep 13, 2013: SKIN. CORRODED. CORROSION DAMAGE WAS FOUND AT MULTIPLE LOCATIONS BETWEEN WS 117.9 AND 184.9 ON THE LT AND RT UPPER OTBD WING SKINS AND THE LT AND RT T/E SKINS. AFTER BLENDING T
- [SDR DXTA2013050805388](https://openairdocs.org/sdr/DXTA2013050805388), Apr 1, 2013: BLADES. DAMAGED. ACCOMPLISH BORESCOPE INSPECTION OF COMBUSTION CHAMBER LINER COOLING RING SEGMENT SELF LOCKING NUTS. ACCOMPLISHED PREINDUCTION GROUND PERFORMANCE RUN AND TRANSIE
- [SDR DXTR20120424002](https://openairdocs.org/sdr/DXTR20120424002), Apr 24, 2012: LINE. CHAFED. LEFT BRAKE LINE FWD OF COPILOTS RT RUDDER PEDAL IS CHAFED DUE TO RUDDER PEDAL CONTACT. R & R LT BRAKE LINE ASSY FWD OF COPILOTS RT RUDDER PEDAL IAW MM 20-10-06.
- [SDR DXTR20120424001](https://openairdocs.org/sdr/DXTR20120424001), Apr 24, 2012: BRACKET. CRACKED. RUDDER AUTOPILOT CABLE BRACKET AT AFT CANTED BULKHEAD IS CRACKED ON INBD RIVET LINE. R & R RUDDER AUTOPILOT CABLE BRACKET IAW SRM 51-40-03 AND MM 22-11-01.
- [SDR DXTA2011022104472](https://openairdocs.org/sdr/DXTA2011022104472), Feb 20, 2011: PITOT TUBE. OBSTRUCTED. BOTH PILOTS PFD'S DISPLAYED AN AMBER IAS MESSAGE AFTER PASSING THROUGH 160 KTS. AT MINIMUM LT PILOTS IAS INDICATING 160, RT PILOTS INDICATING 166 & STANDBY INDI
- [SDR DXTA2009013103481](https://openairdocs.org/sdr/DXTA2009013103481), Jan 31, 2009: WATER SEPARATOR. DIRTY. BOROSCOPE COMBUSTION SECTION FOUND IT TO BE GOOD. INSPECTED INTAKE COLD EXHAUST ALSO FOUND THEM TO BE GOOD. REMOVED OLD WATER SEPARATOR. INSTALLED NEW WATER SEP
- [SDR DXTA2009020203481](https://openairdocs.org/sdr/DXTA2009020203481), Jan 31, 2009: UNKNOWN. SMOKE. SMOKE IN THE COCKPIT CAME THROUGH THE GASPER FANS WITH THE APU RUNNING ON THE GROUND.
- [SDR DXTA2009020203480](https://openairdocs.org/sdr/DXTA2009020203480), Jan 31, 2009: UNKNOWN. SMOKE. SMOKE IN THE COCKPIT CAME THROUGH THE GASPER FANS WITH THE APU RUNNING ON THE GROUND.
- [SDR DXTA200702197](https://openairdocs.org/sdr/DXTA200702197), May 15, 2007: ACTUATOR. DEFECTIVE. ON DEPARTURE AFTER RAISING THE GEAR, THE GEAR UNLOCK LIGHT ON AND THE GREEN NOSE GEAR LIGHT ILLUMINATED. RECYCLED THE GEAR AND HAD THE SAME INDICATION. EXTENDED
- [SDR DXTA200702088](https://openairdocs.org/sdr/DXTA200702088), Apr 7, 2007: WINDSHIELD. FAILED. LT WINDSHIELD SHATTERED. RECEIVED LT FAULT, SELECTED OFF, LT O'HEAT WINDSHIELD, ARCED AND SHATTERED, DIVERTED. [SUP 4-19-07] REPLACED WINDOW IAW MM 56-11-00
- [SDR DXTA200702017](https://openairdocs.org/sdr/DXTA200702017), Mar 13, 2007: TRANSMITTER. MALFUNCTIONED. DURING POWER REDUCTION TO IDLE AT 10.000 FT, LT ENGINE OIL PRESSURE DROPPED TO BELOW 20 PSI AND JUMPED BACK AND FORTH TO 40 PSI. ON POWER INCREASE, PRESSURE STA
- [SDR DXTA200500857](https://openairdocs.org/sdr/DXTA200500857), Jul 24, 2005: TRANSDUCER. INOPERATIVE. ON TAKEOFF ROLL, APPROACHING 60K MASTER CAUTION LIGHT ILLUMINATED WITH ANTI-SKID ANNUNCIATOR LIGHT SWITCHES PROPER POSITION, TAKEOFF ABORTED. T/S TO BAD RT WHEE

## 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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