# N695QS: 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: 680A0280 - Year built: 2021 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: August 30, 2021 - Certificate issued: June 12, 2025 - Expires: June 30, 2032 - Mode S code: A93EB8 - Owner type: Co-owned, fractional ownership - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=695QS - Page: https://openairdocs.org/aircraft/N695QS 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 N695QS. ## FAA accident and incident reports None matched to N695QS. ## Service difficulty reports (10) 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 DXTA2025031702727](https://openairdocs.org/sdr/DXTA2025031702727), Mar 16, 2025: WINDSHIELD. CRACKED. FLIGHT COMPARTMENT WINDOWS: SLIM CRACK ON RIGHT (COPILOT) WINDSHIELD. CORRECTIVE ACTION; CLEANED AND PERFORMED A WINDSHIELD DETAILED INSPECTION OF THE COPILOT W - [SDR DXTA2025012402065](https://openairdocs.org/sdr/DXTA2025012402065), Jan 21, 2025: UPLOCK SWITCH. FAILED. GEAR DISAGREE L AMBER CAS: DEPARTING ASE, DISAGREE L AMBER CAS ON, LEFT GREEN DN LIGHT REMAINED ON AND SOMEONE ON THE GROUND REPORTED THAT THE LEFT GEAR WAS DOW - [SDR DXTA2024103000964](https://openairdocs.org/sdr/DXTA2024103000964), Oct 26, 2024: WINDOW. CRACKED. FO SIDE WINDOW INNER PANE IS CRACKED CORRECTIVE ACTION; REPLACED RH COPILOT COCKPIT SIDE WINDSHIELD IAW CESSNA MODEL 680A MM56·10-05. OPS CHECK GOOD. LEAK CHEC - [SDR DXTA2023090594550](https://openairdocs.org/sdr/DXTA2023090594550), Sep 4, 2023: BOLT. GALLED. WHEN CLOSING DOOR, DOOR WILL INDICATE OPEN. YELLOW LIGHT ON DOOR & CASS MESSAGE INDICATE DOOR OPEN. BUMPING HANDLE, LIGHTS GO OFF & INDICATE CLOSED. RED BUTTON - [SDR DXTA2023070390110](https://openairdocs.org/sdr/DXTA2023070390110), Jul 3, 2023: UNKNOWN. UNKNOWN. WOW MISCOMPARE AMBER CAS: ON TAKEOFF GEAR HANDLE WOULD NOT MOVE. AFTER A MINUTE OR SO GOT WOW MISCOMPARE CAS. PLANE ALSO DEPRESSURIZED. RH MLG SQUAT SWITCH ROLL - [SDR DXTA2023063089950](https://openairdocs.org/sdr/DXTA2023063089950), Jun 30, 2023: UNKNOWN. UNKNOWN. ON TAXI OUT, AMBER MSG "CABIN DOOR OPEN" DISPLAYED. DID CABIN DOOR OPEN PROCEDURE WITH NO LUCK. POWERED DOWN AND TRIED AGAIN WITH NO LUCK. REMOVED THE UPPER STE - [SDR DXTA2022112174420](https://openairdocs.org/sdr/DXTA2022112174420), Nov 21, 2022: PCB. DEFECTIVE. RED BUTTON ON DOOR HANDLE INTERMITANTLY RESPONSIVE. DOES NOT ALLOW DOOR TO OPEN WHEN PUSHED. REMOVED AND REPLACED CABIN DOOR MONITOR PCB IAW MM 24-60-40. OPS CH - [SDR DXTA2022092671080](https://openairdocs.org/sdr/DXTA2022092671080), Sep 25, 2022: NONE. ABNORMAL. MAIN DOOR: SCREW CAME OFF OF MAIN DOOR CONTROL ARM. CONTROL ARM IS SEPARATED AND CANNOT LIFT DOOR.// SIGNOFF// REMOVED WORN FWD DOOR LIFT LINK ASSY PN: 7411323- - [SDR DXTA2022071465980](https://openairdocs.org/sdr/DXTA2022071465980), Jul 14, 2022: PIVOT PIN. LOOSE. MAIN DOOR: MAIN DOOR LIFT PIVOT PIN CAME LOOSE FROM MOTOR ARM. // SIGNOFF// INSPECTED HOLE, CHECKED THREADS, VERIFIED ALL PARTS IN SERVICABLE CONDTION. REINSTAL - [SDR DXTA2021122053900](https://openairdocs.org/sdr/DXTA2021122053900), Dec 20, 2021: NONE. NONE. MAIN DOOR: MAIN CABIN DOOR HANDLE EXTERIOR WOULD NOT OPEN REQUIRED BATTERIES TO BE DISCONNECTED AND RECONNECTED AND DISCONNECTED AGAIN FOR YELLOW DOOR OPEN LIGH ## Service difficulty reports on N695QS not matched to an aircraft (27) They name N695QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DXTA2019020191973](https://openairdocs.org/sdr/DXTA2019020191973), Feb 1, 2019: ACTUATOR. MALFUNCTIONED. NOSE GEAR DID NOT RETRACT AFTER TAKEOFF. GREEN NOSE GEAR LIGHT REMAINED ILLUMINATED AND ASSOCIATED AIRFLOW NOISE WAS EVIDENT. PERFORMED QRH PROCEDURE AND FLEW L - [SDR JGVR20171114001](https://openairdocs.org/sdr/JGVR20171114001), Nov 14, 2017: BRACKET. CORRODED. UPPER BRACKET OF THE CENTER RUDDER HINGE FOUND CORRODED OUT OF LIMITS. REPLACED THE BRACKET. - [SDR JGVR20171113001](https://openairdocs.org/sdr/JGVR20171113001), Nov 13, 2017: AXLE. DAMAGED. FOUNDS PLATING MISSING ON THE NOSE WHEEL AXLE TUBE DURING NOSE WHEEL R&R. REPLACED AXLE TUBE WITH NEW ONE P/N 7142022-21. - [SDR DXTR2015020401](https://openairdocs.org/sdr/DXTR2015020401), Jan 7, 2015: BRACKET. CRACKED. LOWER CLIP ON VERTICAL STABILIZER HAS 2 SMOKED HI-LOCKS ON OTBD EDGES ON FWD SIDE. FOUND A CRACK PROTRUDING FROM THE LT OTBD LOWER PIVOT FITTING FLANGE TRAVELIN - [SDR DXTA2014121505945](https://openairdocs.org/sdr/DXTA2014121505945), Dec 12, 2014: LINE. CHAFED. LOW HYD LEVEL LIGHT CAME ON SHORTLY AFTER TAKEOFF. RAISED THE GEAR & THEN THE FLAPS. THE LIGHT CAME ON IMMEDIATELY AFTER THE FLAPS WERE RAISED. THERE WERE NO OT - [SDR DXTA2014062305805](https://openairdocs.org/sdr/DXTA2014062305805), Jun 22, 2014: LANDING GEAR. MALFUNCTIONED. DURING APPROACH, SELECTED GEAR DOWN. MAIN GEAR EXTENDED NORMAL BUT THE NOSE GEAR DID NOT EXTEND. WHILE RUNNING THE LANDING GEAR WILL NOT EXTEND CHECKLIST, NOTIC - [SDR DXTA2014060505791](https://openairdocs.org/sdr/DXTA2014060505791), Jun 4, 2014: RELAY. FAILED. ON TAXI OUT RECEIVED FLASHING LOW BRAKE PRESSURE & ANTI SKID INOPERATIVE ANNUNCIATORS. ABOUT 20 SECONDS LATER, LOST NORMAL BRAKES, BRAKE PEDALS LOST PRESSURE & - [SDR DXTA2013121805599](https://openairdocs.org/sdr/DXTA2013121805599), Dec 17, 2013: RELAY. UNSERVICEABLE. UPON SHUTDOWN OF THE APU WE NOTICED A STRONG ODOR WHICH SMELLED LIKE ELEC WIRES BURNING AS WE WALKED TOWARDS THE LAVATORY, OPENED THE ACCESSORY DOOR TO THE APU - [SDR DXTA2013090505494](https://openairdocs.org/sdr/DXTA2013090505494), Sep 4, 2013: ACCESS PANEL. CORRODED. WHILE PERFORMING MX, FOUND SURFACE CORROSION ON FUEL PANEL 510DB DOUBLER. - [SDR DXTA2013082005483](https://openairdocs.org/sdr/DXTA2013082005483), Aug 19, 2013: BRAKE ASSY. MALFUNCTIONED. DURING TAXI WHILE APPLYING EVEN BRAKE PRESSURE TO SLOW ACFT, RT BRAKE SUDDENLY BROKE FREE(STOPPING PRESSURE ON THE BRAKES RELEASED) CAUSING THE ACFT TO SWERVE A - [SDR DXTA2013080505466](https://openairdocs.org/sdr/DXTA2013080505466), Aug 4, 2013: MASTER CYLINDER. FAILED. RIGHT BRAKE FAILED DURING TAXI. RIGHT COCKPIT BRAKE PEDAL FAILED TO MAINTAIN BRAKE PRESSURE TO RT MAIN WHEEL BRAKE. LT PILOT TOOK CONTROL OF THE ACFT AND BRAKIN - [SDR DXTA201304150555](https://openairdocs.org/sdr/DXTA201304150555), Apr 15, 2013: ACTUATOR. SEIZED. ON LANDING GEAR EXTENTION LT MLG DID NOT LOCK DOWN AND HAD UNLOCK LIGHT ON TESTED LIGHT AND LIGHT WORKED DID CHECK LIST AND STILL NO LT MLG ON LANDING AND AT TO - [SDR DXTA2013050805387](https://openairdocs.org/sdr/DXTA2013050805387), Mar 22, 2013: RING ASSEMBLY. UNSERVICEABLE. PERFORMED BORESCOPE INSPECTION OF COMBUSTION CHAMBER LINER COOLING RING SEGMENT SELF LOCKING NUTS. DISASSEMBLED CLEANED AND VISUALLY INSPECTED HT DISC ASSEMBLY. - [SDR DXTA2012061805003](https://openairdocs.org/sdr/DXTA2012061805003), Jun 17, 2012: UNKNOWN. ODOR. DURING DESCENT, ENCOUNTERED VERY STRONG INTERMITTENT ODOR ON THE FLIGHT DECK. DURING POSTFLIGHT CHECK WITH THE BATTERY MASTER ON, ODOR REAPPEARED. COULD NOT DUP - [SDR DXTA2012061805002](https://openairdocs.org/sdr/DXTA2012061805002), Jun 17, 2012: ACTUATOR. INOPERATIVE. DURING CLIMB WITH THE GEAR UP, THE GREEN NOSE GEAR DOWN LIGHT CAME ON WITH NO RED GEAR UNSAFE LIGHT. PUT THE GEAR HANDLE DOWN WITH THE ABNORMAL CHECKLIST, THE N - [SDR DXTA2011111004780](https://openairdocs.org/sdr/DXTA2011111004780), Nov 9, 2011: OIL SYSTEM. OVERSERVICED. WITH APU ON AND BLEED AIR ON, COCKPIT AND CABIN FILLED WITH THICK, PUNGENT AND ACRID SMOKE. TROUBLESHOT TO OIL LEVEL TO HIGH, ADJUSTED OIL LEVEL TO CORRECT LEVE - [SDR DXTA2011010304388](https://openairdocs.org/sdr/DXTA2011010304388), Jan 1, 2011: BRAKE ASSY. WEAK. AFTER TOUCHDOWN BRAKES FELT SPONGY AND THEN BECAME EXCESSIVELY GRABBY WHEN SLOWING. CONDUCTED BRAKE BLEED PROCEDURE AND TAXI CHECK. BRAKES FUNCTION NORMAL AT TH - [SDR DXTA2010012503955](https://openairdocs.org/sdr/DXTA2010012503955), Jan 24, 2010: HINGE. LACK OF LUBE. PASSING THROUGH 18,000' AND AN AIRSPEED OF APPOX 260KTS, FELT A SUDDEN JOLT FOLLOWED BY MEDIUM TO HIGH FREQUENCY VIBRATIONS IN THE FUSELAGE AND FLIGHT CONTROLS. - [SDR DXTA2009070103711](https://openairdocs.org/sdr/DXTA2009070103711), Jun 30, 2009: BULB. BURNED. SMOKE FROM CABIN LIGHTS IN BETWEEN SEATS 4 AND 6 AFTER ABOUT 40 MINUTES OF USE. SMOKE AND ELECTRICAL ODOR DISSIPATED WHEN CABIN LIGHT SWITCH TURNED OFF. R & R B - [SDR DXTA2009031603547](https://openairdocs.org/sdr/DXTA2009031603547), Mar 13, 2009: PCB. INOPERATIVE. ON TAKEOFF ROLL JUST PRIOR TO 70 KTS, NO TAKEOFF ANNUNCIATOR, WARNING HORN, AND MASTER CAUTION. EVERYTHING AS FAR AS FLAPS, SPEED BRAKES & TRIM WAS IN CORRECT P - [SDR DXTA200702698](https://openairdocs.org/sdr/DXTA200702698), Dec 20, 2007: WATER SEPARATOR. ODOR. NOXIOUS FUMES ENTER COCKPIT WHEN COCKPIT TEMPERATURE CONTROL IS RAISED TO HEAT COCKPIT. REMOVED & CLEANED WATER SEPARATOR. REINSTALLED WATER SEPARATOR IAW CESSN - [SDR DXTA200701832](https://openairdocs.org/sdr/DXTA200701832), Jan 2, 2007: CONNECTOR. DIRTY. DURING TAKEOFF THERE WAS A LARGE THROTTLE SPLIT AND TOOL, A LOT OF RT RUDDER TO MAINTAIN DIRECTIONAL CONTROL. RESET FAULT, DISCONNECTED, CLEANED AND INSPECTED, - [SDR DXTA200601408](https://openairdocs.org/sdr/DXTA200601408), May 26, 2006: CONTROL UNIT. FAILED. AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. WITH LDG GEAR HANDLE UP STILL HAD (3) GREEN INDICATION. CYCLED GEAR HANDLE DOWN AND BACK UP WITH SAME INDICATION. - [SDR DXTA200500958](https://openairdocs.org/sdr/DXTA200500958), Sep 8, 2005: A/C PACK. ODOR. 15 MIN PRIOR WITH APU RUNNING AT HPN (NJA FACILITY) OUR A/C WAS TAIL TO TAIL WITH A COMPANY ULTRA. THE ULTRA STARTED IT'S ENGINES AND RAN FOR 10 TO 15 MINS BLOW - [SDR DXTA200500809](https://openairdocs.org/sdr/DXTA200500809), Jun 28, 2005: CONTROL CABLE. SHEARED. LT RUDDER PEDAL WILL NOT MOVE RUDDER. RT RUDDER PEDAL WILL MOVE RUDDER. LT RUDDER PEDAL MOVES FREELY WITH NO RESISTANCE. ALSO NOTED RUDDER CABLE BOWS BEHIND PED - [SDR DXTA200400386](https://openairdocs.org/sdr/DXTA200400386), Sep 8, 2004: ARM. UNSECURE. DURING CLIMB OUT, THE GEAR UNLOCK LIGHT CAME ON, RECYCLED GEAR AND PROBLEM DID NOT GO AWAY. ACCOMPLISHED AIR TURN BACK TO MRY. FOUND THE EMERGENCY GEAR BOTTLE A - [SDR DXTA200300186](https://openairdocs.org/sdr/DXTA200300186), Nov 26, 2003: CONTROL CABLE. CHAFED. PERFORMED AILERON WING CABLE INSPECTION PER CESSNA ASL560XL-27-12, FOUND CABLES CHAFED/BROKEN BEYOND MANUFACTURER'S LIMITS. REMOVED AND REPLACED LEFT AND RIGHT ## 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 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.