# N625QS: 2020 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: 680A0240 - Year built: 2020 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: February 27, 2020 - Certificate issued: January 30, 2026 - Expires: January 31, 2033 - Mode S code: A82A3F - Owner type: Co-owned, fractional ownership - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=625QS - Page: https://openairdocs.org/aircraft/N625QS 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 N625QS. ## FAA accident and incident reports None matched to N625QS. ## Service difficulty reports (14) 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 DXTA2026092809861](https://openairdocs.org/sdr/DXTA2026092809861), Sep 24, 2026: STEERING SYS. FAULTED. CLIMBING THROUGH 38,000 FEET A THUMP WAS HEARD FOLLOWED BY THE GEAR DISAGREE N CAS AND A HASHED BOX ON NOSE GEAR INDICATOR. APPROXIMATELY 30 MINUTES LATER WE HE - [SDR DXTA2026042807808](https://openairdocs.org/sdr/DXTA2026042807808), Apr 26, 2026: PRESSURE SWITCH. FAILED. FUEL BOOST PUMP ON RIGHT INDICATION WHEN SELECTING LEFT CROSSFEED. WE RAN THE QRH AND MESSAGE CLEARED. WHEN WE SELECTED CROSSFEED AGAIN NOTHING ABNORMAL HAPPENE - [SDR DXTA2026032307287](https://openairdocs.org/sdr/DXTA2026032307287), Mar 19, 2026: BATTERY. FAULTED. AFT EMER LIGHTS STAY ON WHEN PLANE TURNED OFF. RESET 5G SWITCH BUT THEY STAYED ON. REPLACED BATTERY. OPS CHECK GOOD. IAW AMM 33-50-06 - [SDR DXTA2025120205933](https://openairdocs.org/sdr/DXTA2025120205933), Dec 1, 2025: BATTERY PACK. INOPERATIVE. SEAT 7 LIGHT INOP. EXIT ON BULKHEAD DIM. OUTSIDE RT OVERWING INOP. REMOVED & REPLACED BATTERY PACKS. OPS AND FUNCTIONAL CHECKS GOOD.IAW AMM 33-50-06 - [SDR DXTA2025103105501](https://openairdocs.org/sdr/DXTA2025103105501), Oct 30, 2025: TRIM SYSTEM. OUT OF RIG. ON DEPARTURE I NOTICED THE AIRCRAFT PITCHED OFF THE RUNWAY MORE AGGREESIVELY THAN NORMAL PITCH INPUT. CLIMBING AT 250 KNOTS FELT NORMAL. OVER 10,000' CLIMHING A - [SDR DXTA2025031102621](https://openairdocs.org/sdr/DXTA2025031102621), Mar 8, 2025: BATTERY. DEFECTIVE. EMERGENCY LIGHTING: EMER LIGHT ON FLOOR, UNDERNEATH SEAT 3, DOES NOT ILLUMINATE DURING TEST. COMPLETED CHARGING PROCEDURE. AFTER 2, 30 MINUTE CHARGES, THE LIGHT - [SDR DXTA2025012702118](https://openairdocs.org/sdr/DXTA2025012702118), Jan 26, 2025: BATTERY. NO TEST. FLOOR EMERG EXIT LIGHT: SEAT 3 EMERGENCY LIGHT INOP AFTER 2 CHARGES. CORRECTIVE ACTION: REPLACED BATTERY. OPS CHECK GOOD. IAW . - [SDR DXTA2024062812202](https://openairdocs.org/sdr/DXTA2024062812202), Jun 27, 2024: BRAKE ASSY. UNKNOWN. WHEN HEAVY BRAKING APPLIED, BRAKES MAKE A VERY LOUD SOUND & RESONATES THROUGH ACFT. ACFT PULLED SLIGHTLY LT ON TOUCHDOWN BRAKING. SPUN WHEELS BY HAND, DID NOT N - [SDR 3J7R2024031400001](https://openairdocs.org/sdr/3J7R2024031400001), Mar 14, 2024: BATTERY. DISCHARGED. DURING MXC NOTED ALL EMERGENCY LIGHTS POWERED BY BATTERY PACK #3 DO NOT ILLUMINATE WITH BATTERY PACK POWER - [SDR DXTA2022080467330](https://openairdocs.org/sdr/DXTA2022080467330), Aug 3, 2022: ENGINE. DEFECTIVE. ENGINE FLAMEOUT: CLIMBING THROUGH FLIGHT LEVEL 280 THE NUMBER 2 ENGINE FLAMED OUT. LOUD BANG AND THEN INSTANT ROLL BACK QRH PROCEDURES ACCOMPLISHED. DECLARED AN - [SDR DXTA2022050461230](https://openairdocs.org/sdr/DXTA2022050461230), May 4, 2022: SEAL. LEAKING. MAIN CABIN DOOR HARD TO OPEN. FOUND PROBLEM TO BE CABIN DOOR SEAL. REMOVED MED SEAL P/N 9914814-1 NSN AND INSTALLED CUSTOMER SUPPLIED NEW SEAL P/N 9914814-1 PER - [SDR DXTA2022020956450](https://openairdocs.org/sdr/DXTA2022020956450), Feb 8, 2022: NOT REPORTED. NOT REPORTED. MAIN DOOR: WHEN YOU LIFT EITHER THE OUTSIDE HANDLE OR INSIDE HANDLE ON THE DOOR, NORMALLY THE DOOR JUST SMOOTHLY OPENS NOW IT TAKES A TUG ON THE HANDLE FROM THE - [SDR 2022F00039](https://openairdocs.org/sdr/2022F00039), Jan 27, 2022: SKIN. DENTED. RFTS-105731 (DENT FROM BIRD STRIKE MUST BE PERMANENTLY REPAIRED. - [SDR DXTA2020103004294](https://openairdocs.org/sdr/DXTA2020103004294), Oct 30, 2020: BATTERY PACK. DISCHARGED. AFTER LANDING AND SHUTDOWN NOTICED THE FORWARD ZONE OF THE EMERGENCY LIGHT SYSTEM STUCK ON. SIGN OFF. WE GAINED ACCESS TO THE "G SWITCH" UP ON THE AFT PORTION O ## Service difficulty reports on N625QS not matched to an aircraft (15) They name N625QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DXTA2013122005603](https://openairdocs.org/sdr/DXTA2013122005603), Dec 20, 2013: VALVE. DEFECTIVE. ON DEPARTURE, AFTER RAISING LG, WE GOT A RED UNLOCK LIGHT. FOLLOWED THE CHECKLIST, PULLED HYD PRESS CB, & HEARD A CLUNK IN THE NOSE OF THE PLANE, WE BELIEVED TH - [SDR DXTA2013092505519](https://openairdocs.org/sdr/DXTA2013092505519), Sep 24, 2013: COALESCER BAG. DIRTY. CABIN HAS AN ACRID ODOR WITH NOTHING RUNNING. STARTED APU AND ODOR INCREASED WITH BLEED AIR ON. STARTED ENGINES AND SHUTDOWN APU. ODOR WAS SLIGHTLY PRESENT. CLE - [SDR DXTA2012030504904](https://openairdocs.org/sdr/DXTA2012030504904), Mar 4, 2012: ACTUATOR. MALFUNCTIONED. LEFT MLG INDICATOR DID NOT SHOW SAFE DOWN WHEN EXTENDED AND RED UNSAFE LIGHT ILLUMINATED. YAWED ACFT TO ACHIEVE GOOD DOWN & LOCKED INDICATION. LANDED NORMALLY. - [SDR DXTA2011020804456](https://openairdocs.org/sdr/DXTA2011020804456), Feb 7, 2011: APU. SMOKE. APPEARANCE OF SMOKE/MIST IN CABIN AND COCKPIT WHEN APU BLEED AIR SWITCH TURNED ON. BOTH MAIN ENGINES WERE NOT RUNNING. HAD USED APU BLEED AIR TWICE EARLIER, NO - [SDR DXTA2009123103920](https://openairdocs.org/sdr/DXTA2009123103920), Dec 30, 2009: DISPLAY. INOPERATIVE. THE RT SIDE AMLCD SCREEN WENT BLANK (BLACK SCREEN). NO CIRCUIT BREAKERS WERE POPPED. AFTER SCREEN ATTEMPTED TO COME ON 2 MORE TIMES, IT WENT BLANK AGAIN AND AN - [SDR DXTA2009072303736](https://openairdocs.org/sdr/DXTA2009072303736), Jul 22, 2009: INDICATOR. OUT OF POSITION. EXTREME NOSE DOWN YOKE PRESSURE REQUIRED AFTER TAKEOFF. ELECTRIC TRIM CAN NOT KEEP UP WITH NOSE DOWN PRESSURE REQUIRED. COMPLIED WITH SYSTEM OPS CHECKS FOUND IN - [SDR DXTA200702473](https://openairdocs.org/sdr/DXTA200702473), Sep 13, 2007: ENGINE. NONE. JUST PRIOR TO V1 CALLOUT; SEAGULL STRIKE TO OB EDGE OF LT ENGINE NACELLE LIP. ABORTED TAKEOFF. OBVIOUS SIGNS OF (DEBRIS) INSIDE AND OUTSIDE INTAKE TO ENGINE. IN - [SDR DXTA200702171](https://openairdocs.org/sdr/DXTA200702171), May 2, 2007: UNKNOWN. UNKNOWN. AT FL190 AND 190KIAS, A SUDDEN LOUD, LOW 'THUD' WAS HEARD AND FELT. 3 SECONDS LATER IT WAS HEARD AGAIN. PASSENGER THOUGHT IT CAME FROM BENEATH HIM AT CABIN SEAT - [SDR DXTA200601258](https://openairdocs.org/sdr/DXTA200601258), Feb 22, 2006: CONTROL VALVE. FAILED. SHORTLY AFTER SELECTING BLEED AIR ON THE FLOW OF BLEED AIR TO THE COCKPIT WAS ABNORMALLY HIGH FOLLOWED BY ILLUMINATION OF THE AIR DUCT O'HEAT, CKPT ANNUNCIATOR - [SDR DXTA200500967](https://openairdocs.org/sdr/DXTA200500967), Sep 14, 2005: FIRE LOOP. DIRTY. LEFT FIRE DET SYSTEM INOP, LIGHT ON IN FLIGHT. VERIFIED SQWAWK, T/S SYSTEM BY SWAPPING LT & RT FIRE DETECT CONTROLS, NO HELP. REMOVED UPPER AND LOWER LT ENGINE - [SDR DXTA200500962](https://openairdocs.org/sdr/DXTA200500962), Sep 10, 2005: FUEL FILTER. CLOGGED. RIGHT SIDE FUEL FILTER BYPASS ANNUNCIATOR AND MASTER CAUTION LIGHT ILLUMINATED DURING TAKEOFF ROLL. LIGHT ILLUMINATED AS THROTTLES WERE PUT IN TO DETENT. THROTT - [SDR DXTA200500871](https://openairdocs.org/sdr/DXTA200500871), Jul 27, 2005: LINE. LEAKING. PILOT AND COPILOT BRAKES SPONGY. INSPECTED LT AND RT MAIN BRAKES WEAR INDICATORS ARE WITHIN LIMITS. CHECKED BRAKE ACCUMULATOR AND BRAKE RESERVOIR ARE GOOD. BLEE - [SDR DXTA200500867](https://openairdocs.org/sdr/DXTA200500867), Jul 27, 2005: BRAKE. MALFUNCTIONED. PILOT AND COPILOT BRAKES SPONGY. ITEM IS UNDER INVESTIGATION - [SDR DXTA200400287](https://openairdocs.org/sdr/DXTA200400287), Apr 1, 2004: AILERON. VIBRATION. AFTER TAKE OFF WITH GEAR UP ABOVE 180 KNOTS IAS, YOKE DEVELOPED AN AILERON SHIMMY/ VIBRATION OF APPROX. 1 TO 2 VIBRATIONS PER SECOND. INTENSITY INCREASED UP TO - [SDR DXTA200300159](https://openairdocs.org/sdr/DXTA200300159), Nov 10, 2003: STARTER GEN. FAILED. LEFT ENGINE FAILED TO START ON FIRST ATTEMPT N2 DID NOT INCREASE PAST 10 PERCENT. SECOND ATTEMPTED START NR N2 INDICATION AT ALL DISCONNECTED START SEQUENCE BLE ## 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.