# N967QS: 2025 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: 680A0421 - Year built: 2025 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: February 23, 2025 - Certificate issued: May 11, 2026 - Expires: May 31, 2033 - Mode S code: AD7796 - Owner type: Co-owned, fractional ownership - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=967QS - Page: https://openairdocs.org/aircraft/N967QS 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 N967QS. ## FAA accident and incident reports None matched to N967QS. ## 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 DXTA2026102110278](https://openairdocs.org/sdr/DXTA2026102110278), Oct 20, 2026: STOP FITTING. OUT OF ADJUST. MAIN CABIN DOOR HANDLE DIFFICULT TO MOVE TO BOTH THE OPEN AND CLOSED POSITION. (SELF INDUCED A CHECK DOORS CAS MESSAGE ON ONE OCCASION) PERFORMED THE ADJUSTMENT - [SDR DXTA2026101910229](https://openairdocs.org/sdr/DXTA2026101910229), Oct 17, 2026: MOTOR. FAULTED. DOOR WILL NOT CLOSE FULLY FROM INSIDE OR OUTSIDE AIRCRAFT. STOPS ABOUT 1/2-3/4" BEFORE FULLY CLOSED. REMOVED FAULTY CABIN DOOR LIFT MOTOR AND REPLACED WITH A CU - [SDR DXTA2026101210098](https://openairdocs.org/sdr/DXTA2026101210098), Oct 8, 2026: DOOR. NO DISCREPANCY. MAIN CABIN DOOR REQUIRES EXCESSIVE FORCE TO OPEN/CLOSE. FORCE REQUIRED WAS FOUND TO BE WITHIN LIMITS. OPS CHECK GOOD. IAW CE680A AMM 52-10-00 - [SDR DXTA2026082609416](https://openairdocs.org/sdr/DXTA2026082609416), Aug 23, 2026: HANDLE. STIFF. AOG: 52-12-01 MAIN-DOOR HANDLE - WHILE OPENING THE DOOR, THE HANDLE CATCHES ABOUT 3/4 OF THE WAY UP, HAVE TO PULL HARD TO OPEN. WHEN CLOSING THE DOOR, THE HANDL - [SDR DXTA2025102705446](https://openairdocs.org/sdr/DXTA2025102705446), Oct 25, 2025: HANDLE. STUCK. INTERIOR/EXTERIOR CABIN DOOR HANDLE JAMMED IN THE OPEN/UNLOCKED POSITION. CORRECTIVE ACTION: GAINED ACCESS TO MED LATCHING MECHANISM, FOUND DOOR LOCKING PINS DR - [SDR DXTA2025102005351](https://openairdocs.org/sdr/DXTA2025102005351), Oct 17, 2025: LATCH. OUT OF RIG. REPEAT WRITE UP FROM 10/01. MAIN DOOR LATCH TAKES A LOT OF PRESSURE TO PUSH DOWN INTO LOCKED POSITION CORRECTIVE ACTION: PERFORMED CABIN DOOR STOP RIGGING. OPS - [SDR DXTA2025100205169](https://openairdocs.org/sdr/DXTA2025100205169), Oct 1, 2025: DOOR. LACK OF LUBE. MAIN DOOR LATCH TAKES A LOT OF PRESSURE TO PUSH DOWN INTO LOCKED POSITION. LUBRICATED MAIN CABIN DOOR. OPS CHECK GOOD. IAW CE-680A MM 12·20-40 ## Service difficulty reports on N967QS not matched to an aircraft (14) They name N967QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DXTA2010010503931](https://openairdocs.org/sdr/DXTA2010010503931), Jan 4, 2010: PACKING. LEAKING. INITIALLY ON GEAR RETRACTION THE HANDLE WOULD NOT UNLOCK. TRIED AGAIN AND THE GEAR RETRACTION STARTED, ALL 3 GREEN LIGHTS EXTINGUISHED. GOT THE RED AND IT STAYE - [SDR DXTA2009091803792](https://openairdocs.org/sdr/DXTA2009091803792), Sep 17, 2009: COALESCER BAG. ODOR. ON THE RAMP WITH APU ON, WHITE SMOKE FILLED COCKPIT. APPEARED TO COME FROM COCKPIT PAC. NO SMOKE IN CABIN. ODOR WAS DETECTED FROM COCKPIT PAC IN FLIGHT WITH APU - [SDR DXTA2009052803665](https://openairdocs.org/sdr/DXTA2009052803665), May 27, 2009: UNKNOWN. ODOR. AFTER TURNING ON THE ANTI-ICE, A STRONG SULFUR ODOR WAS PRESENT FOR ABOUT 1 MINUTE, THEN DISSIPATED. RAN ACFT & TRIED TO DUPLICATE PROBLEM. NO ODOR NOTED IN COC - [SDR DXTA2009012403474](https://openairdocs.org/sdr/DXTA2009012403474), Jan 24, 2009: STRUT. DISCHARGED. AFTER T/O GEAR HANDLE WOULD NOT MOVE ON FIRST ATTEMPT. ON SECOND TRY, GEAR HANDLE MOVED, GEAR RETRACTED NORMALLY, BUT RED LIGHT REMAINED ON. LOWERED GEAR NORMAL - [SDR DXTA2009012603474](https://openairdocs.org/sdr/DXTA2009012603474), Jan 24, 2009: HANDLE. MALFUNCTIONED. AFTER T/O, GEAR HANDLE WOULD NOT MOVE ON FIRST ATTEMPT. ON SECOND TRY, GEAR HANDLE MOVED, GEAR RETRACTED NORMALLY BUT RED LIGHT REMAINED ON. - [SDR DXTA200702188](https://openairdocs.org/sdr/DXTA200702188), May 12, 2007: DOWNLOCK SWITCH. STICKING. WHEN ATTEMPTING TO RAISE LANDING GEAR, LEFT MAIN INDICATION REMAINED GREEN (DOWN). ROTARY TEST GOOD. TROUBLESHOT, FOUND DOWNLOCK SWITCH LT GEAR STICKING. REMOVE - [SDR DXTA200701921](https://openairdocs.org/sdr/DXTA200701921), Feb 8, 2007: VENT. SMOKE. SMOKE WAS DETECTED COMING FROM AIR VENT IN COCKPIT AND CABIN. REPLACED FORWARD ACM IAW CE-750 M/M CHAPTER 21-51-00. OPERATIONAL AND LEAK CHECK GOOD. - [SDR DXTA200701902](https://openairdocs.org/sdr/DXTA200701902), Feb 1, 2007: FLAP SYSTEM. MALFUNCTIONED. FLAPS FAIL CAS MSG. WOULD NOT RESET. FAILED WHEN FLAPS FULLY RETRACTED. REMOVED AND REPLACED RT RESOLVER WITH NEW. RIGGED SYSTEM PER CESSNA 750 M/M CHAP 27-50-0 - [SDR DXTA200500942](https://openairdocs.org/sdr/DXTA200500942), Aug 30, 2005: STRIKER. OUT OF ADJUST. DURING T/O ROLL AMBER EICAS MSG. BAGGAGE DOOR SEAL AND MASTER CAUTION ILLUMINATED BEFORE 80 KIAS. ABORTED T/O. ADJUSTED BAGGAGE DOOR SEAL SWITCH AND STRIKER PLA - [SDR DXTA200500878](https://openairdocs.org/sdr/DXTA200500878), Aug 2, 2005: PIN. SHEARED. DURING TAXI, TILLER KNOB DEVELOPED SLACK WHEN TURNING THEN FINALLY POPPED AND ROTATES FREELY. UNABLE TO STEER THE AIRCRAFT WITH THE TILLER. ROLL PIN IN TILLER K - [SDR DXTA200500691](https://openairdocs.org/sdr/DXTA200500691), Apr 21, 2005: LANDING GEAR. MALFUNCTIONED. LOUD BUMP WAS HEARD AND FELT IN THE NOSE COMPARTMENT DURING CRUISE. JACKED AIRCRAFT, INSPECTED NOSE STRUT, UPLOCK & SWITCH. INSPECTED MAIN GEAR UPLOCKS AND SWIT - [SDR DXTA200500683](https://openairdocs.org/sdr/DXTA200500683), Apr 17, 2005: ROLLER. STIFF. NOSE GEAR CYCLE - HEARD AND FELT A THUMP, NO LIGHTS. FOUND UPLOCK ROLLERS STIFF TO TURN AND LEFT MLG UPLOCK HOOK WAS STIFF AND WOULD NOT SEAT THE ROLLER EVERY T - [SDR DXTA200400463](https://openairdocs.org/sdr/DXTA200400463), Nov 30, 2004: WINDOW. FAILED. DURING CRUISE FLIGHT AT FL 410, WINDSHIELD HEAT INOP R CAS MESSAGE ILLUMINATED. TEN SECONDS LATER, LEFT WING SHIELD OUTER PANE SHATTERED, ELECTIRICAL ARCING WAS - [SDR DXTA200400410](https://openairdocs.org/sdr/DXTA200400410), Sep 29, 2004: ODOR. DETECTED. DURING DESCENT, STRONG SMOKE ODOR DETECTED AFTER REDUCING POWER, UNABLE TO DETERMINE CAUSE OR ISOLATE SOURCE. AFTER 3-4 MINUTES THE ODOR WENT AWAY. CHECKED NR 1 ## 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.