# N627QS: 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: 680A0241 - Year built: 2020 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: March 5, 2020 - Certificate issued: September 18, 2025 - Expires: September 30, 2032 - Mode S code: A831AD - Owner type: Co-owned - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=627QS - Page: https://openairdocs.org/aircraft/N627QS 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 N627QS. ## FAA accident and incident reports None matched to N627QS. ## Reports on N627QS not matched to an aircraft (1) They name N627QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [Incident 20141016019189I](https://openairdocs.org/incident/20141016019189I), Oct 16, 2014: Cessna 560XL (N627QS), Minneapolis, MN, No damage. On initial climb out after departure from msp, at approximately 400 feet AGL, pilots reported that acm (air cycle machine) overheat warning light illuminated… ## Service difficulty reports (11) 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 DXTA2026032307375](https://openairdocs.org/sdr/DXTA2026032307375), Mar 21, 2026: LINK. CORRODED. LT MLG TRAILING LINK HAS SIGNS OF PITTING ON THE INNER WALL. / FOUND WHILE PERFORMING SL680A-32-11. CORRECTIVE ACTION: PERFORMED EDDY CURRENT INSPECTION. NO CRA - [SDR DXTA2026032307376](https://openairdocs.org/sdr/DXTA2026032307376), Mar 21, 2026: LINK. CORRODED. RH MLG TRAILING LINK HAS SIGNS OF PITTING ON THE INNER WALL. / FOUND WHILE PERFORMING SL680A-32-11. CORRECTIVE ACTION: PERFORMED EDDY CURRENT INSPECTION. NO CRA - [SDR 2025FA0000346](https://openairdocs.org/sdr/2025FA0000346), May 7, 2025: SKIN. DEBONDED. DISBONDS ON THE UPPER WINGS BETWEEN THE OUTBOARD END OF STRINGERS AND THE COMMON SKIN DOUBLERS. THE SKIN AND COMMON DOUBLERS MAY ALSO EXHIBIT A GRADUAL DEVIATIO - [SDR DXTA2025011401902](https://openairdocs.org/sdr/DXTA2025011401902), Jan 9, 2025: SKIN. DENTED. DENT DISCOVERED ON TOP OF LEFT WING.2). FLAP: RIGHT FLAP HAS A NOTICEABLE DENT ON THE TOP DISCOVERED DURING PREFLIGHT INSPECTION. PERFORMED PERMANENT REPAIR IAW - [SDR DXTA2024080500083](https://openairdocs.org/sdr/DXTA2024080500083), Aug 3, 2024: WIRE. PULLED. LAV FLOOR EMERGENCY LIGHT INOP. PERFORMED THE "EMERGENCY LIGHTS FAIL PREFLIGHT TEST" PROCEDURE FROM THE QRH. LIGHT REMAINED INOP. FOUND LAV FLOOR EMERGENCY LIGH - [SDR 2022FA0000192](https://openairdocs.org/sdr/2022FA0000192), Apr 6, 2022: NONE. CHIPPED. LH MLG AXLE PLATING DAMAGE (CHIPPED) - [SDR 2022F00179](https://openairdocs.org/sdr/2022F00179), Apr 6, 2022: STINGER. CORRODED. STINGER UPPER NUTPLATE DRAG ANGLES ARE CORRODED AT NUTPLATES. - [SDR DXTA2021120652980](https://openairdocs.org/sdr/DXTA2021120652980), Dec 3, 2021: NONE. NONE. MAIN EXIT SIGN/LIGHT: MAIN CABIN EXIT LIGHTS ALL REMAIN ON AFTER SHUTDOWN. // SIGNOFF // RESET COCKPIT INERTIA SWITCH IAW CE-680AMM 33-50-11 OPS CHECKS GOOD. - [SDR DXTA2021120352930](https://openairdocs.org/sdr/DXTA2021120352930), Dec 3, 2021: NONE. NONE. LAV EMERG LIGHT: ON INITIAL EMER LIGHT TEST, FOUND LAV EMER FLOOR LIGHT IMOP. // SIGNOFF// POWERED ON A/C AND CONFIRMED SQWAK REMOVED TOILET FRONT PIECE TO ACCE - [SDR 2021F00382](https://openairdocs.org/sdr/2021F00382), Nov 20, 2021: SKIN. CHAFED. THE FUSELAGE LOWER SKIN (PN: 7411392-12) WAS CHAFED IN TWO AREAS FROM CONTACT WITH THE ANTI-ICE CROSSFLOW VALVE. THE VALVE IS REPOSITIONED PER TEXTRON AVIATION - [SDR DXTA2021080246240](https://openairdocs.org/sdr/DXTA2021080246240), Aug 1, 2021: G SWITCH. FAILED. EMERGENCY EXIT SIGN/LIGHT: EMERGENCY LIGHTS WILL NOT TURN OFF WITH SWITCH IN OFF POSITION. LIGHTS ARE OVER THE MAIN CABIN DOOR (WHITE), 2 (RED) SIDE WALL LIGHTS ## Service difficulty reports on N627QS not matched to an aircraft (17) They name N627QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR EBVR20190304001](https://openairdocs.org/sdr/EBVR20190304001), Mar 4, 2019: PIVOT. CRACKED. FOUND DURING INSPECTION: HORIZONTAL STAB AFT PIVOT FITTING CRACKED. P/N 6631102-31. - [SDR CWQR20150129005](https://openairdocs.org/sdr/CWQR20150129005), Jan 29, 2015: FITTING. CRACKED. DURING A SCHEDULED INSPECTION, FOUND THE HORIZONTAL STABILIZER ATTACH FITTING CLIP CRACKED IN TWO PLACES. THE CRACKS WERE IN THE CUT OUT RADIUS ABOUT .12 INCH L - [SDR DXTA2014101705912](https://openairdocs.org/sdr/DXTA2014101705912), Oct 16, 2014: UNKNOWN. SMOKE. SMOKE WAS OBSERVED IN THE COCKPIT & CABIN. ODOR WAS ALSO OBSERVED. - [SDR 2012FA0000710](https://openairdocs.org/sdr/2012FA0000710), Oct 10, 2012: CONTROL CABLE. FRAYED. WHILE TROUBLESHOOTING, AN AUTO PILOT PORPOISE DISCREPANCY, THE TECH PULLED ON A PRIMARY RUDDER CABLE IN THE TAIL CONE AND IT SNAPPED. THE CABLE HAS BEEN BROKEN - [SDR DXTA2012052504979](https://openairdocs.org/sdr/DXTA2012052504979), May 24, 2012: UNKNOWN. ODOR. APPROX 1 HR INTO A FLIGHT, AT 41,000 AND IN NORMAL CRUISE MODE. CO-PILOT AND PILOT COULD DETECT AN ODOR OF FUEL. WENT TO BACK OF PLANE WHERE FOUR OTHER CREW MEM - [SDR DXTA2011042004551](https://openairdocs.org/sdr/DXTA2011042004551), Apr 19, 2011: WATER SEPARATOR. ODOR. DISTINCT EXHAUST ODOR IN COCKPIT AT TAKE OFF WITH APU ON AND APU BLEED AIR ON. WITH BLEED AIR OFF THE ODOR IS REDUCED. IN FLIGHT THERE IS AN EXHAUST ODOR (NOT A - [SDR DXTA2011022104471](https://openairdocs.org/sdr/DXTA2011022104471), Feb 20, 2011: GYRO. INOPERATIVE. AT FL 430, WITH PFD 2 SELECTED (RT SEAT FLYING) LT PFD COMMAND BAR TURNED BLUE ALONG WITH ALL TREND BARS AND COURSE INDICATORS. THE RED AIRSPEED TAPE DISSAPEARE - [SDR 2010F00010](https://openairdocs.org/sdr/2010F00010), Jan 22, 2010: INDICATOR. MALFUNCTIONED. AFTER TAKE OFF (L) FUEL GUAGE ANNUNCIATOR ILLUMINATED. FUEL LOAD INITIALLY SHOWED 1000 LBS HIGH, THEN STABILIZED SHOWING 1000 LBS LOW AND REMAINED THERE. - [SDR DXTA2010010803933](https://openairdocs.org/sdr/DXTA2010010803933), Jan 7, 2010: FLOW VALVE. INOPERATIVE. MOVING THE FUEL TRANSFER SWITCH FROM LT TO OFF CAUSES THE L/R LOW PRESS ANNUN. TO ILLUMINATE MOMENTARY & TURN THE L/R FUEL BOOST PUMP ANNUN. ON. TROUBLESHOT TO - [SDR DXTA2009090303770](https://openairdocs.org/sdr/DXTA2009090303770), Sep 2, 2009: ACTUATOR. INOPERATIVE. LEFT GREEN DOWN AND LOCKED ANNUNCIATOR ILLUMINATED INTERMITTENTLY IN FLIGHT. HYDRAULIC PRESS LIGHT DID NOT ILLUMINATE. ALL OTHER INDICATIONS NORMAL. INSTALLED R - [SDR DXTA2009033003571](https://openairdocs.org/sdr/DXTA2009033003571), Mar 29, 2009: INDICATOR. UNKNOWN. AT BEGINNING OF TAKEOFF ROLL THE RT FUEL QUANTITY INDICATOR DROPPED TO ZERO AND THE RT FUEL GAUGE ANNUNCIATOR AND MASTER CAUTION ILLUMINATED. STARTED APU AND WA - [SDR 2008FA0000676](https://openairdocs.org/sdr/2008FA0000676), Sep 8, 2008: CONTROL CABLE. BROKEN. DURING ROUTINE INSP, FOUND CABLE STRANDS BROKEN AND FRAMED. THE DAMAGED AREA OF THE CABLE IS WHERE IT GOES OVER A SERIES OF "S" PULLEYS MOUNTED IN THE HORIZ STA - [SDR DXTA200803081](https://openairdocs.org/sdr/DXTA200803081), May 27, 2008: WARNING SYSTEM. ACTIVATED. BOTH L/R FUEL GAUGE ANNUNCIATORS ILLUMINATED ON TAKEOFF. TAKEOFF WAS ABORTED. FUEL QTY GAUGES BOTH READ ZERO. GAINED ACCESS TO LT/RT WING ROOT ELECTRICAL CONNEC - [SDR DXTA20082874](https://openairdocs.org/sdr/DXTA20082874), Feb 13, 2008: PROBE. READS LOW. ON TAKEOFF ROLL, MASTER CAUTION CAME ON, REJECTED TAKEOFF, LT FUEL GAUGE ANNUNCIATOR LIGHT ON. CONNECTED TEST SET, FOUND PROBE NR 6 READING LOW. REMOVED NR6 PRO - [SDR DXTA200702737](https://openairdocs.org/sdr/DXTA200702737), Jan 1, 2008: ACTUATOR. LEAKING. ON TAKEOFF, GOT A STAB MISCOMPARE LIGHT AND THE HYDRAULIC PRESS LIGHT. REPLACED ACTUATOR DUE TO EXCESS LEAKAGE IN ACTUATOR IAW 560XL M/M 23-40-00. OPS AND LEAK - [SDR DXTA200702304](https://openairdocs.org/sdr/DXTA200702304), Jun 28, 2007: BRAKE. STUCK. LT BRAKE IS STICKING CAUSING CONTROL ISSUES WHILE TAXIING. INSTALLED AN OVERHAULED BRAKE IN LT POSITION IAW MM CH 32-42. INSTALLED AN OVERHAULED METERING VALVE - [SDR DXTA200300108](https://openairdocs.org/sdr/DXTA200300108), Sep 2, 2003: PUSHROD. CHAFED. DURING ROUTINE INSPECTION FOUND MAIN ENTRY DOOR PUSHROD (OPENING/CLOSING) RUBBING AGAINST THE CUTOUT IN THE DOOR STRUCTURE. ADJUSTED PUSHROD TO PREVENT CHAFING, ## 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.