# N675QS: 2019 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: 680A0212
- Year built: 2019
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 25, 2019
- Certificate issued: March 3, 2026
- Expires: March 31, 2033
- Mode S code: A8EFBA
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=675QS
- Page: https://openairdocs.org/aircraft/N675QS

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 N675QS.

## FAA accident and incident reports

None matched to N675QS.

## Reports on N675QS not matched to an aircraft (2)

They name N675QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 20130811014119I](https://openairdocs.org/incident/20130811014119I), Aug 11, 2013: Cessna 560XL (N675QS), Mesa, AZ, No damage. While climbing though FL 290, heard a pop and left PFD, MFD, and FMS screen went blank. Ahrs aux pwr 1 annunciator was illuminated and cabin pressurization…
- [Incident 20080413836859I](https://openairdocs.org/incident/20080413836859I), Apr 13, 2008: Cessna 560XL (N675QS), Torrance, CA, Minor damage. (-23) On April 13, 2008, N675QS was taxiing on taxiway "a" and made a right turn to the transit parking area. The right wing tip impacted the nose cowling of…

## Service difficulty reports (15)

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 DXTA2026071508824](https://openairdocs.org/sdr/DXTA2026071508824), Jul 14, 2026: DOOR. LACK OF LUBE. THE MAIN CABIN DOOR HANDLE REQUIRES EXCESSIVE FORCE TO LATCH. DURING SEVERAL CLOSURES, THE RESISTANCE VARIED, BUT WHEN IT DID HANG UP, THE INSIDE HANDLE WAS ABO
- [SDR DXTA2026052108172](https://openairdocs.org/sdr/DXTA2026052108172), May 20, 2026: PIN. LACK OF LUBE. MAIN CABIN DOOR HANDLE DIFFICULT TO FULLY ENGAGE IN LOCKED POSITION WHEN CLOSING DOOR FROM EITHER INSIDE OR OUTSIDE. HANDLE TRAVELS FREELY WHEN DOOR IS OPEN. OP
- [SDR MISR2026020306754](https://openairdocs.org/sdr/MISR2026020306754), Jan 31, 2026: MODULE. DEFECTIVE. ON CLIMB OUT FULL NOSE DOWN TRIM REQUIRED. AUTOPILOT KICKED OFF. DECISION MADE TO SLOW THE AIRCRAFT BELOW 200 KTS TO MAINTAIN CONTROL AND LESSEN CONTROL INPUTS.
- [SDR DXTA2026020306755](https://openairdocs.org/sdr/DXTA2026020306755), Jan 31, 2026: MODULE. DEFECTIVE. FLAP FAIL AND CAS MESSAGE APPEARED FOR EVERY FLAP SETTING SELECTED. RESET REQUIRED AND QRH RUN FOR EACH FAILURE (FLAPS 1, FLAPS 2, FLAPS FULL SELECTIONS). CORRE
- [SDR DXTA2025120906022](https://openairdocs.org/sdr/DXTA2025120906022), Dec 6, 2025: UNKNOWN. ODOR. WITH THE APU ON & BLEED AIR SELECTED ON, SMELL AN ELECTRICAL BURNING. TRACKED ODOR BACK TO LT SIDE OVERHEAD HEAT DUCT. WHEN TOUCHED, METAL TRACK WHERE THE HEATE
- [SDR 2025F00267](https://openairdocs.org/sdr/2025F00267), Nov 11, 2025: FITTING. CORRODED. AFTER REMOVAL OF NLG ACTUATOR FOUND CORROSION ON THE AFT FITTING ASSEMBLY. REMOVED CORRODED NLG ACTUATOR FITTING AND REPLACED WITH NEW CUSTOMER SUPPLIED NLG FIT
- [SDR 2025F00268](https://openairdocs.org/sdr/2025F00268), Nov 10, 2025: SKIN. CORRODED. FOUND 43 AREAS OF CORROSION UNDER AFT BELLY PANEL 316CBC. MECHANICALLY REMOVED CORROSION WHERE 36 NUTPLATES WERE REMOVED AND 4 ADDITIONAL AREAS IN BAY 316CBC IA
- [SDR 2025F00261](https://openairdocs.org/sdr/2025F00261), Nov 7, 2025: TUNNEL WALL. CORRODED. REPAIRED LEVEL 2 CORROSION ON LH AND RH NLG TUNNEL SKINS PER AQRD ERO-986034 REV.IR, TITLED "N675QS NLG TUNNEL CORROSION" DATED 28OCT25. SUPPORTED BY FAA FORM 8
- [SDR DXTA2025043003245](https://openairdocs.org/sdr/DXTA2025043003245), Apr 27, 2025: BUSHING. DAMAGED. MAIN DOOR: TO OPEN MAIN CABIN DOOR A PUSH IS REQUIRED FROM THE INSIDE TO GET THE DOOR TO OPEN. CORRECTIVE ACTION: ACCOMPLISHED FF-1 INFORMATION RECEIVED FROM NE
- [SDR DXTA2024101400811](https://openairdocs.org/sdr/DXTA2024101400811), Oct 10, 2024: LATCH. OUT OF RIG. MAIN DOOR: MAIN CABIN DOOR IS VERY HARD TO OPEN FROM THE OUTSIDE OF THE AIRCRAFT. REPEAT WRITE UP. CORRECTIVE ACTION: RIGGED CED LATCH/LOCK SYSTEM IN REF TO CE6
- [SDR DXTA2024100700746](https://openairdocs.org/sdr/DXTA2024100700746), Oct 3, 2024: NUT. LOOSE. MAIN DOOR: WE COULD NOT OPEN THE MAIN ENTRY DOOR FROM OUTSIDE THE AIRCRAFT, THE HANDLE WAS JAMMED, AND WOULD NOT MOVE IN EITHER DIRECTION. WE GAINED ACCESS TO T
- [SDR DXTA2022022157100](https://openairdocs.org/sdr/DXTA2022022157100), Feb 20, 2022: NOT REPORTED. NOT REPORTED. EXIT SIGN LIGHT IN BACK OF CABIN AND EMER LIGHTS ABOVE AND BELOW THE TOILET ARE INOPERATIVE. // SIGNOFF // DUE TOTHE SATISFACTORTY TASK CARD OPS CHECK FROM SQK 
- [SDR DXTA2022011054850](https://openairdocs.org/sdr/DXTA2022011054850), Jan 7, 2022: CONTACTOR. ABNORMAL. DC GEN AMPS R AMBER CAS: DURING CRUISE AT FL400, AMBER DC GEN AMP R CAME ON STEADY AND QRH P1 WAS DIRECTED AND FOLLOWED. DIVERSION TO MSY WAS NECESSARY. // SIGN
- [SDR 2021F00385](https://openairdocs.org/sdr/2021F00385), Dec 22, 2021: WEB. CRACKED. NOSE WHEEL WELL WEB (PN: 7413133-10) IS CRACKED ON LH AND RH SIDES AT FS 75. REPAIRED IAW TEXTRON AVIATION STANDARD REPAIR SR-680A-ATA53-25890 DATED 06/01/2020,
- [SDR 2021F00125](https://openairdocs.org/sdr/2021F00125), May 24, 2021: COVER. CORRODED. #2 ENGINE ACCESSORY GEARBOX REAR COVER HAS MULTIPLE AREAS OF CORROSION. ACCOMPLISH TEMPORARY REPAIR AND PROTECTION OF THE AGB COVER FLANGES FROM MINOR CORROSION

## Service difficulty reports on N675QS not matched to an aircraft (19)

They name N675QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA2015082606064](https://openairdocs.org/sdr/DXTA2015082606064), Aug 25, 2015: BRAKE. WORN. RIGHT BRAKE IS WORN MORE THAN THE LEFT BRAKE. RT BRAKE IS GRABBING & CAUSING ACFT TO DART TO THE RIGHT ON TAXI & LANDING ROLL OUT. JACKED ACFT & REMOVED RT BRAK
- [SDR DXTA2015082606063](https://openairdocs.org/sdr/DXTA2015082606063), Aug 25, 2015: VALVE. FAILED. AFTER TAKEOFF, EXCESSIVE AMOUNT OF BLEED AIR ALONG WITH A BURNING ODOR. THE ACM OVERHEAT LIGHT ILLUMINATED FOLLOWED BY THE BLEED AIR OVERHEAT LIGHT. MASTER WARN
- [SDR DXTR2015022401](https://openairdocs.org/sdr/DXTR2015022401), Feb 20, 2015: SUPPORT ANGLE. CRACKED. CRACK AT FWD DOOR SPRING ON FWD FRAME, PERFORMED EDDY CURRENT INSPECTION OF THE MAIN CABIN DOOR STRUCTURE IAW NDI MANUAL PN 6 20-00-02. VERIFIED EXISTENCE OF CR
- [SDR DXTR2015022402](https://openairdocs.org/sdr/DXTR2015022402), Feb 18, 2015: PULLEY BRACKET. CRACKED. RUDDER AUTOPILOT SERVO PULLEY BRACKET CRACKED. R & R BRACKET REF SRM 51-40-03. INSTALLED, PN 6661154-2.
- [SDR DXTA2014080605847](https://openairdocs.org/sdr/DXTA2014080605847), Jul 16, 2014: UNKNOWN. MALFUNCTIONED. RETRACTED GEAR ON DEPARTURE & WE GOT A GEAR UNSAFE RED LIGHT & NOSE WHEEL DOWN & LOCKED GREEN LIGHT. MAIN GEAR RETRACTED NORMALLY. NO OTHER ABNORMAL INDICATIONS
- [SDR DXTA2013050605376](https://openairdocs.org/sdr/DXTA2013050605376), May 7, 2013: BEARING. FAILED. NOSE WHEEL SHIMMY STARTING AT WALKING SPEED UP TO 60 KNOTS. MOST PRONOUNCED AT 40 KNOTS. REPLACED NOSE GEAR TORQUE LEAK BUSHING WITH NEW BUSHING IAW THE MM CHAP
- [SDR DXTA2013012905264](https://openairdocs.org/sdr/DXTA2013012905264), Jan 28, 2013: APU. SMOKE. DURING "BEFORE START" CHECKLIST AND WHILE STARTING THE APU, SMOKE WAS NOTICED IN THE CABIN. THE APU HAD COMPLETED IT'S START SEQUENCE AND THE APU GENERATOR WAS 
- [SDR CWQR20120330022](https://openairdocs.org/sdr/CWQR20120330022), Mar 30, 2012: CONTROL CABLE. FRAYED. DURING A SCHEDULED INSPECTION, THE ELEVATOR TRIM CABLE WAS FOUND TO BE FRAYED BEYOND LIMITS. THIS CABLE ASSY IS LOCATED WHERE THE CABLE TRANSITIONS FROM A VERTI
- [SDR DXTA2011051904584](https://openairdocs.org/sdr/DXTA2011051904584), May 18, 2011: ACTUATOR. MALFUNCTIONED. AFTER TAKEOFF, GEAR SELECTED UP, NLG WHEEL INDICATOR LIGHT STAYED GREEN WITH SOUND INDICATION, GEAR DOORS WERE STILL OPEN. MLG SWITCH WAS SELECTED DOWN WITH 3 G
- [SDR DXTA2011020704455](https://openairdocs.org/sdr/DXTA2011020704455), Feb 6, 2011: HOOK. STIFF. AFTER GEAR RETRACTION, 3 GREEN LIGHTS EXTINGUISHED BUT LANDING GEAR UNLOCK LIGHT ILLUMINATED. GEAR WAS EXTENDED AND REMAINED THAT WAY FOR THE REMAINDER OF THE F
- [SDR DXTA2010101204259](https://openairdocs.org/sdr/DXTA2010101204259), Oct 11, 2010: TRANSMITTER. OUT OF ADJUST. DURING TAKEOFF CLIMB, THE WIND SHEAR WARNING CAME ON IN CALM WINDS. AT 170 KNOTS INDICATED AND FLAPS UP THE ANGLE OF ATTACK TAPE ON THE AIR SPEED INDICATOR SHOW
- [SDR DXTA2010101204258](https://openairdocs.org/sdr/DXTA2010101204258), Oct 11, 2010: AUTOPILOT SYS. UNKNOWN. CLIMBING THROUGH FLIGHT LEVEL 380 WITH THE AUTO PILOT ON AND FLIGHT LEVEL CHANGE SET TO .65, THE ACFT PITCHED UP TO APPROX 10 DEGREES. THE VERTICAL SPEED INDICA
- [SDR DXTA20082876](https://openairdocs.org/sdr/DXTA20082876), Feb 14, 2008: ACTUATOR. FAILED. AFTER TAKEOFF, DURING GEAR RETRACTION, NOSE GEAR STAYED DOWN AND LOCKED (GREEN ) MAIN GEARS OPERATED NORMALLY. REMOVED NOSE GEAR ACTUATOR DUE TO INTERNAL FAILUR
- [SDR DXTA200501162](https://openairdocs.org/sdr/DXTA200501162), Dec 27, 2005: WHEEL. OUT OF ADJUST. DURING TAKEOFF AS A/C ACCELERATED TO 60 KIAS, A/C WANTED TO OVER-ROTATE. TAKEOFF ABORTED. PITCH TRIM DID NOT MOVE DURING ROLL ON TAKEOFF. TRIM WHEEL FOUND TO BE
- [SDR DXTA200501169](https://openairdocs.org/sdr/DXTA200501169), Dec 21, 2005: ROD. BROKEN. UPON GEAR RETRACTION HEARD A LOUD BANG. NO OTHER INDICATIONS. SHORTLY AFTERWARDS HEARD WHAT SOUNDED LIKE A NOSE GEAR DOOR OPEN. AFTER LANDING LT NOSE GEAR DOOR 
- [SDR DXTA200500985](https://openairdocs.org/sdr/DXTA200500985), Sep 26, 2005: THERMAL SWITCH. INOPERATIVE. RIGHT AT V1, EMER PRESS CAME ON FOLLOWED BY ACM OVERHEAT, AIR DUCT OVERHEAT ALSO AND SMOKE STARTED TO FILL THE CABIN. - GAINED ACCESS TO THE ACM, VISUALLY INSPE
- [SDR DXTA200500856](https://openairdocs.org/sdr/DXTA200500856), Jul 23, 2005: WHEEL. JAMMED. ELEVATOR TRIM JAMMED DURING FINAL APPROACH. HAD TO USE EXCESSIVE FORCE ON TRIM WHEEL TO TRIM AIRCRAFT. TRIM WHEEL REMAINS TIGHT WITH ALL POWER OFF AIRCRAFT. - I
- [SDR DXTA200400377](https://openairdocs.org/sdr/DXTA200400377), Aug 31, 2004: ENGINE. BIRD INGESTION. ON TAKEOFF ROLL INGESTED A BIRD IN LEFT ENGINE, ABORTED TAKEOFF AND RETURNED TO BLOCK. PRELIMINARY INSPECTION FOUND EVIDENCE OF INGESTION NOTED ON ENGINE INLET 
- [SDR DXTA200400213](https://openairdocs.org/sdr/DXTA200400213), Jan 5, 2004: THRUST REVERSER. LACK OF LUBE. DURING FLIGHT, THE LT THRUST REVERSER LIGHT CAME ON AND A SLIGHT VIBRATION FELT FROM THE LT SIDE OF AIRPLANE. COMPLIED WITH NORMAL CHECKLIST AND EMERGENCY STOW 

## 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

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