# N982QS: 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: 680A0444 - Year built: 2025 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 4, 2025 - Certificate issued: October 7, 2025 - Expires: October 31, 2032 - Mode S code: ADB401 - Owner type: Co-owned, fractional ownership - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=982QS - Page: https://openairdocs.org/aircraft/N982QS 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 N982QS. ## FAA accident and incident reports None matched to N982QS. ## Service difficulty reports (3) 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 DXTA2026091809755](https://openairdocs.org/sdr/DXTA2026091809755), Sep 16, 2026: ELEC CONNECTOR. DISCONNECTED. FORWARD EMERGENCY EXIT LIGHT AT MAIN CABIN DOOR IS INOPERATIVE. FWD EMER EXIT LIGHT WAS FOUND TO BE DISCONNECTED. RECONNECTED LIGHT, OPS CHECKS GOOD WITH NO OTH - [SDR DXTA2026030407092](https://openairdocs.org/sdr/DXTA2026030407092), Mar 2, 2026: POWER SUPPLY. DEFECTIVE. FLOOR EMERGENCY LIGHTS UNDER SEATS 5 AND 8, OVERHEAD EMERGENCY LIGHT SEAT 7 AND WING EMERGENCY STEP LIGHT FAILED PREFLIGHT TEST. COMPLIED WITH AFM CHARGING PROC - [SDR DXTA2025100305179](https://openairdocs.org/sdr/DXTA2025100305179), Oct 2, 2025: ELEC CONNECTOR. LOOSE. EMERGENCY LIGHTS IN SEAT NR 3 OVERHEAD LIGHT IS INOP, FLOOR LIGHTING ON NR 3 IS INOP AND RIGHT WING INSPECTION LIGHT IS INOP. ALL EMERGENCY LIGHTS ARE ON BATTER ## Service difficulty reports on N982QS not matched to an aircraft (35) They name N982QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR 2017F00197](https://openairdocs.org/sdr/2017F00197), Aug 18, 2017: SKIN. CORRODED. FUSELAGE SKIN CORRODED. - [SDR 2017F00196](https://openairdocs.org/sdr/2017F00196), Aug 18, 2017: SKIN. CORRODED. FUSELAGE AND TAILCONE SKIN CORRODED REPAIRED IAW ENGINEERING DQ8835M1, REV A. - [SDR 2017F00195](https://openairdocs.org/sdr/2017F00195), Aug 18, 2017: SKIN. CORRODED. REPAIR OF LT WING SKIN CORROSION IAW ENGINEERING DQ8751M1. - [SDR DXTA2016061406258](https://openairdocs.org/sdr/DXTA2016061406258), Jun 17, 2016: DOWNLOCK SWITCH. UNSERVICEABLE. WHEN LANDING GEAR WAS EXTENDED WE GOT 3 GREEN AND 1 RED UNLOCKED LIGHT. AURAL WARNINGS CAME ON WHEN FLAPS FULLY EXTENDED AND WHEN TLA WAS BROUGHT TO IDLE. REMOV - [SDR DXTA2015082706066](https://openairdocs.org/sdr/DXTA2015082706066), Aug 26, 2015: INDICATOR. OUT OF LIMITS. AFTER TAKEOFF & DURING CLIMB, CONTROL COLUMN, CAPTAIN'S SIDE, HAD A DEAD SPOT IN PITCH, ALLOWING PLUS OR MINUS 3 INCHES OF COLUMN MOVEMENT, WITH NO CONTROL FEEL - [SDR DXTA2014021205650](https://openairdocs.org/sdr/DXTA2014021205650), Feb 11, 2014: SKIN. CORRODED. CORROSION FOUND ON LOWER WING SKIN. REPAIRED CORROSION IAW S-750-ATA57 09RD, S-750-ATA 07RD REV A & S-750-0182 15RD. - [SDR DXTA2013103005551](https://openairdocs.org/sdr/DXTA2013103005551), Oct 29, 2013: ACM. ODOR. ODOR IN COCKPIT & CABIN NOTICED BY CREW AND PASSENGERS. UNABLE TO DETERMINE WHETHER ENVIRONMENTAL OR ELECTRICAL. ODOR SLOWLY DISSIPATED DURING DESCENT. VERIFIED - [SDR DXTA2013012405260](https://openairdocs.org/sdr/DXTA2013012405260), Jan 23, 2013: TURBOCHARGER. INOPERATIVE. ON INITIAL START UP OF APU A STRONG BURNING ODOR WAS OBSERVED FOLLOWED BY A VISABLE MIST IN THE COCKPIT ONLY. THIS OCCURED AS THE ISOLATION VALVE WAS OPENED. PE - [SDR DXTA2011082604711](https://openairdocs.org/sdr/DXTA2011082604711), Aug 25, 2011: RUDDER PEDAL. BINDING. WHEN AIRPLANE IS TURNED TO THE LEFT IN FLIGHT THE RUDDER SEEMS TO GET STUCK. PROBLEM HAPPENS WITH AUTOPILOT ENGAGED AND DISENGAGED. DIDN'T MATTER WHAT ALTITUDE/ - [SDR DXTA2011080904695](https://openairdocs.org/sdr/DXTA2011080904695), Aug 9, 2011: UNKNOWN. ODOR. ON THE GROUND WITH JUST THE APU RUNNING, TURNED ON THE BLEED AIR MAX COOL SWITCH AND ISOLATION VALVE TO OPEN AND SMELLED A BURNING RUBBER ODOR. NO SMOKE OBSERVE - [SDR DXTA2011032104517](https://openairdocs.org/sdr/DXTA2011032104517), Mar 20, 2011: FLOAT VALVE. FOD. AT FL390, RECEIVED RT FUEL IMBALANCE. USED CHECKLIST, ABLE TO BALANCE FUEL & RETURNED SWITCHES TO NORMAL. CRUISE, NOTICED FUEL CONTINUED TO UNBALANCE. APPEARED - [SDR DXTA2011021804470](https://openairdocs.org/sdr/DXTA2011021804470), Feb 16, 2011: OIL SYSTEM. FAILED. DURING DESCENT CREW SMELLED SULPHUR ODOR IN ACFT. UPON DEBARKATION OF PASSENGERS, CABIN FILLED WITH SMOKE, STARTING FROM THE REAR OF THE ACFT. ON INSPECTION OF - [SDR DXTA2010020503972](https://openairdocs.org/sdr/DXTA2010020503972), Feb 4, 2010: COALESCER BAG. ODOR. BAD ODOR FROM PAC'S. R & R BOTH RT & LT COALESCER SOCKS. - [SDR DXTA2009051103644](https://openairdocs.org/sdr/DXTA2009051103644), May 9, 2009: ACTUATOR. MALFUNCTIONED. RUDDER LIMIT FAIL B AMBER CAS MESSAGE ILLUMINATED ON CLIMBOUT. RUDDER LIMITED TO 32 PERCENT. TROUBLESHOT SYSTEM. REMOVED AND REPLACED RUDDER LIMIT ACTUATOR "B" - [SDR DXTA200803012](https://openairdocs.org/sdr/DXTA200803012), Apr 22, 2008: ACM. ODOR. WITH APU ON AN OILY MUSTY ODOR IS PRESENT WITH THE CABIN AND COCKPIT PAC'S COOLING THE AC. REMOVED AND REPLACED AFT ACM IAW MM CHAPTER 21-51-00. OPERATIONAL AND - [SDR DXTA200802990](https://openairdocs.org/sdr/DXTA200802990), Apr 12, 2008: SEAL. SMOKE. IMMEDIATELY AFTER TAKEOFF SMELLED AND SAW SMOKE IN THE COCKPIT MOVING FROM LT TO RT ACROSS THE PILOT'S SEAT. REMOVED AND REPLACED LT ENGINE IAW 750 MM 71-00-03 - [SDR DXTA200802988](https://openairdocs.org/sdr/DXTA200802988), Apr 10, 2008: O-RING. LEAKING. CKPT PAC NOTICEABLE FUMES DURING TAKEOFF POWER. M2B-LT ENGINE N1A AND N1B SPEED SENSORS LEAKING OIL PAST O-RINGS. INSTALLED NEW O-RINGS AND LEAK CHECK GOOD PER - [SDR DXTA20082903](https://openairdocs.org/sdr/DXTA20082903), Feb 28, 2008: APU. OVERSERVICED. ON TAKEOFF, COCKPIT AND CABIN BEGAN FILLING WITH SMOKE. AN IMMEDIATE RETURN FOR LANDING WAS ACCOMPLISHED. FOUND APU OVER SERVICED AND REMOVED EXCESS OIL. INSPEC - [SDR DXTA200802841](https://openairdocs.org/sdr/DXTA200802841), Feb 5, 2008: ACM. LEAKING. SMOKE IN COCKPIT, SMELLED AND SEEN AS A LIGHT MIST, IMMEDIATELY AFTER TAKE OFF. RETURNED (M-2B) T/S AND REMOVED AND REPLACED COCKPIT ACM WITH A NEW UNIT. PERFOR - [SDR DXTA200702689](https://openairdocs.org/sdr/DXTA200702689), Dec 18, 2007: BULB. BURNED OUT. GREEN NOSE GEAR DOWN AND LOCKED LIGHT IS INOP, LANDING GEAR BLOW DOWN BOTTLE AND NOSE GEAR UPLOCK MANUAL RELEASE (D-RING) WAS USED. INSTALLED NEW BULBS IN NOSE - [SDR DXTA200702383](https://openairdocs.org/sdr/DXTA200702383), Aug 5, 2007: BRAKE. WEAK. RIGHT BRAKE PEDAL IS VERY SPONGY ON BOTH PILOTS AND COPILOTS SIDE. PEDAL GOES ALMOST TO THE BOTTOM BEFORE SOLID BRAKING OCCURS. BLED BRAKES IAW 750 MM 32-42-00. - [SDR DXTA200702333](https://openairdocs.org/sdr/DXTA200702333), Jul 13, 2007: STRUT. UNDERSERVICED. COULD NOT RETRACT GEAR AFTER DEPARTURE. GEAR HANDLE WAS LOCKED IN THE DOWN POSITION AND COULD NOT BE MOVED. JACKED A/C, FOUND NLG STRUT DID NOT EXTEND. SERVICED - [SDR DXTA200702111](https://openairdocs.org/sdr/DXTA200702111), Apr 16, 2007: A/C PACK. ODOR. STRONG BURN SMELL FROM COCKPIT PACK. PAC TURNED OFF. NO DIVERSION. REMOVED & REPLACED COCKPIT ACM IAW CESSNA 750 MM CHPT 21-51-00. OPS & LEAK CHECKS GOOD. - [SDR DXTA200702102](https://openairdocs.org/sdr/DXTA200702102), Apr 12, 2007: BRAKE ASSY. DAMAGED. BRAKES ARE HARD TO PUSH AND MAKE EXCESSIVE NOISE. [SUP 4-19-07] PERFORMED TESTS AS IAW CE750 MM 32-42-00, NO FAULTS WERE FOUND IN EITHER POWER BRAKE FUNCTIONAL - [SDR DXTA200601770](https://openairdocs.org/sdr/DXTA200601770), Nov 30, 2006: WHEEL. VIBRATES. NOSE WHEEL SHIMMY DEVELOPED AT LOW SPEED ON TAKE-OFF ROLL. LESS THAN 50 KNOTS. FOUND LT NOSE WHEEL OB BEARING BURNED, IB BEARINGS DIRTY, LT AXLE UNDER TORQUED A - [SDR DXTA200601585](https://openairdocs.org/sdr/DXTA200601585), Aug 31, 2006: TIRE. FAILED. DURING TAKEOFF ROLL, AIRCRAFT BEGAN TO SHUTTER ACCELERATING THRU 60 KIAS. TAKEOFF WAS ABORTED AND RETURNED TO NORMAL AS AIRCRAFT SLOWED THRU 60 KIAS. REMOVED AN - [SDR DXTA200601358](https://openairdocs.org/sdr/DXTA200601358), Apr 23, 2006: PITOT SYSTEM. CONTAMINATED. YAW DAMP, MACH TRIM DISENGAGED TWICE ON TAKEOFF ROLL. PITOT HEAT WAS ON FOR 5 MINUTES PRIOR TO SECOND TAKEOFF ROLL. PERFORMED OPS CHECK OF YAW DAMPNER ON FGC A - [SDR DXTA200501047](https://openairdocs.org/sdr/DXTA200501047), Oct 19, 2005: STRUT. DIRTY. DURING FLIGHT GEAR RETRACTS HEARD AND FELT BUMP IN THE NIGHT FOUR (4) TIMES DURING FLIGHT. MEASURED EXTENSION OF NOSE STRUT, MEASURED 9.80 INCHES DISASSEMBLED A - [SDR DXTA200500971](https://openairdocs.org/sdr/DXTA200500971), Sep 16, 2005: ACM. FAILED. WHILE DESCENDING OUT OF 410, HEARD A LOUD BANG AND SMELLED SMOKE. THE SMOKE CLEARED, UNABLE TO CONTROL COCKPIT TEMP. SUSPECT COCKPIT ACM BROKEN. ITEM IS UNDER I - [SDR DXTA200500905](https://openairdocs.org/sdr/DXTA200500905), Aug 17, 2005: ACTUATOR. FAILED. RUDDER LIMIT FAIL A EICAS MESSAGE. CONTROL PAGE SHOWS 43 PERCENT RUD LIMIT. REMOVED UPPER RUDDER -A- LINEAR ACTUATOR DUE TO INTERNAL FAILURE. INSTALLED OVERHAUL - [SDR DXTA200500861](https://openairdocs.org/sdr/DXTA200500861), Jul 24, 2005: HANDLE. LOCKED. GEAR WOULD NOT RETRACT AFTER T/O HANDLE LOCKED IN DOWN POSITION T/O INDICATORS ON N1 STAYED ON AFTER POWER REDUCTION THEY WERE WHITE. ITEM IS UNDER INVESTIGATIO - [SDR DXTA200500767](https://openairdocs.org/sdr/DXTA200500767), Jun 11, 2005: LIGHT. SMOKE. AT 41,000 FT WHITE PUFF OF SMOKE APPEARED FROM F/O CHART HOLDER LIGHT. THE LIGHT WAS OFF. THE MAP CB WAS PULLED AND THE SMOKE STOPPED. ITEM DEFERRED PER NJA CAR - [SDR DXTA200500633](https://openairdocs.org/sdr/DXTA200500633), Mar 18, 2005: STRUT. UNDERSERVICED. AFTER DEPARTURE FROM MIDWAY, GEAR HANDLE WOULD NOT RELEASE FROM THE DOWN POSITION, COULD NOT BE RAISED, AIRCRAFT RETURNED FOR LANDING. JACKED ACFT AND FOUND THE - [SDR DXTA200300199](https://openairdocs.org/sdr/DXTA200300199), Dec 15, 2003: TIRE. FAILED. ON LANDING AT TXKF BOTH MAIN TIRES BLEW DAMAGING HARDWARE ON STRUT, GEAR DOOR AND FLAP TRACK FAIRINGS. ITEM IS UNDER INVESTIGATION. - [SDR DXTA200300019](https://openairdocs.org/sdr/DXTA200300019), Apr 28, 2003: CONTROLLER. MALFUNCTIONED. JUST AFTER STARTING A DESCENT FROM FL 410 CABIN RAPIDLY OVERPRESSURIZED . PRESSURE WENT TO BELOW ZERO AND CABIN DPSI WAS RIGHT AT REDLINE. DUE TO RATE AND PRESS ## 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.