# N694QS: 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: 680A0226
- Year built: 2019
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 13, 2019
- Certificate issued: October 8, 2024
- Expires: October 31, 2031
- Mode S code: A93B01
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=694QS
- Page: https://openairdocs.org/aircraft/N694QS

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 N694QS.

## FAA accident and incident reports

None matched to N694QS.

## Service difficulty reports (16)

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 2025FA0000834](https://openairdocs.org/sdr/2025FA0000834), Dec 19, 2025: HP TURBINE. CRACKED. RH ENGINE HAS EVIDENCE OF AXIAL CRACKING ON HPT STAGE 1 BLADES (4 TOTAL BLADES).
- [SDR DXTA2025060603788](https://openairdocs.org/sdr/DXTA2025060603788), Jun 5, 2025: DOOR. BINDING. MAIN CABIN DOOR DIFFICULT TO CLOSE FROM INSIDE. FEELS LIKE PIN ALLIGNMENT, TOP AFT PIN. FUNCTIONAL FROM EXTERIOR. DOOR IS ALSO INTERMITTENTLY SLOW TO OPEN. UPON
- [SDR DXTA2025031702678](https://openairdocs.org/sdr/DXTA2025031702678), Mar 14, 2025: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTING: EMERGENCY LIGHTS DO NOT ILLUMINATE IN THE ARM POSITION. CORRECTIVE ACTION; REPLACED THE EMERGENCY LIGHT BATTERY PACK ASSEMBLY BATTERY !AW SI
- [SDR 2025FA0000131](https://openairdocs.org/sdr/2025FA0000131), Feb 25, 2025: DECK PLATE. CORRODED. FOUND LAVATORY DECK CORRODED ON UNDER SIDE. COMPLIED WITH RFTS-113043 N694QS (680A-0226) TOILET SEAL PANEL CORROSION REV.0 DATED 21FEB25.
- [SDR 2025FA0000125](https://openairdocs.org/sdr/2025FA0000125), Feb 21, 2025: TAIL CONE. CORRODED. AFT FUSELAGE FAIRING SUPPORT CORROSION
- [SDR DXTA2025021002265](https://openairdocs.org/sdr/DXTA2025021002265), Feb 6, 2025: BATTERY. DISCHARGED. CABIN EMERG LIGHT: DURING THE POWER ON CHECKLIST, WITH THE BATTERIES OFF, WHEN THE EMER LTS SWITCH IS PLACED IN THE ARM POSITION NONE OF THE INTERIOR EMERGENCY 
- [SDR DXTA2025012902141](https://openairdocs.org/sdr/DXTA2025012902141), Jan 28, 2025: BATTERY PACK. NO TEST. DURING THE EMER LIGHT TEST WHILE SELECTING TO ARM THE EMERGENCY EXIT AND OVERHEAD LIGHTS DID NOT ILLUMINATE. WHEN SELECTING EMER LIGHT TO ON THE LIGHTS WOULD EL
- [SDR DXTA2024110701046](https://openairdocs.org/sdr/DXTA2024110701046), Nov 3, 2024: RUDDER. NO DISCREPANCY. RUDDER: DURING APPROACH WITH 15 KTS LEFT CROSSWIND THE RUDDER PEDAL SEEM TO BE BINDING AND HARD TO PUSH FOR CROSSWIND ALIGNMENT. THE YAW DAMPER WAS VERIFIED OFF
- [SDR DXTA2024021510901](https://openairdocs.org/sdr/DXTA2024021510901), Feb 14, 2024: GENERATOR. FAILED. HALF WAY DURING FLIGHT AT 40,000 THE RIGHT WINDSHEILD HEAT INOP CAS MESSAGE CAME ON. PROCEDURE ON CHECKLIST WAS COMPLETED. THIS IS A REPEAT WRITE UP. REMOVED FA
- [SDR DXTA2023111310032](https://openairdocs.org/sdr/DXTA2023111310032), Nov 12, 2023: UNKNOWN. UNKNOWN. LAV EMERG LIGHT: WITH THE EMER LIGHT TO ARM AND THE MAIN BATTERIES OFF, THE EXIT SIGN ON THE BULKHEAD BEHIND SEAT 7 IS INOP, THE SPOT LIGHT AT SEAT 7 IS INOP, T
- [SDR DXTA2023071991230](https://openairdocs.org/sdr/DXTA2023071991230), Jul 18, 2023: UNKNOWN. UNKNOWN. CABIN DOOR OPEN AMBER CAS: CHECK DOORS AMBER CAS AND AMBER DOOR OPEN LIGHT ON THE HANDLE ALL ILLUMINATED WITH THE DOOR CLOSED. QRH COMPLIED WITH. RESULTS WERE U
- [SDR 2023FA0000103](https://openairdocs.org/sdr/2023FA0000103), Mar 1, 2023: NONE. NONE. IMPACT DAMAGE - L/H WING, UPPER AND LOWER SKINS, TRAILING EDGE, CWS 320 - WS 369. REFERENCE FR-680A-0226-10757 AND FAA FORM 8100-9 DATED 06JUL2022. REFERENCE TE
- [SDR DXTA2021091548840](https://openairdocs.org/sdr/DXTA2021091548840), Sep 14, 2021: LANDING GEAR. DEFECTIVE. GSD FAIL 2 AMBER CAS: SHORTLY AFTER BEGINNING OUR DISSENT FROM FLIGHT LEVEL 410 THE GSD FAIL 2 AMBER ICAS MESSAGE ELIMINATED. THE AMBER MESSAGE CHECKLIST DROVE 
- [SDR 2021F00219](https://openairdocs.org/sdr/2021F00219), Aug 24, 2021: SKIN. CHAFED. CHAFE IN LOWER FUSELAGE SKIN CAUSED BY ANTI-ICE CROSSFLOW VALVE. ACCOMPLISHED TEXTRON STANDARD REPAIR SR-680A-ATA53-22175 DATED 7/19/2019, STEPS 1-5, STEPS 6-8 
- [SDR DXTA2021032239780](https://openairdocs.org/sdr/DXTA2021032239780), Mar 22, 2021: SUPPORT ROD. BENT. WHILE CLOSING THE MED THE DOOR SUPPORT ROD WAS BENT. THIS ALSO PUT ABOUT A 1/2" CRACK IN THE INNER LINER OF THE MED. "CORRECTIVE ACTION" INSTALLED NEW LIFT LINK
- [SDR DXTA2021020404673](https://openairdocs.org/sdr/DXTA2021020404673), Feb 3, 2021: INDICATOR. WARNING MESSAGE. GEAR POSITION & WARNING: LANDING GEAR EXCEEDED GEAR EXTENSION SPEED AT APPROX 230KTS CORRECTIVE ACTION JACKED AIRCRAFT, PERFORMED SLOW CYCLE OF LANDING GEAR. IN

## Service difficulty reports on N694QS not matched to an aircraft (24)

They name N694QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR EBVR20141107001](https://openairdocs.org/sdr/EBVR20141107001), Nov 7, 2014: FITTING. CRACKED. WE ARE FINDING MORE OF THESE PIVOT FITTING ASSEMBLY HAVING CRACKS PN 6631102-15 & T CLIP PN 6631202-7 HAVING LOOSE HARDWARE.
- [SDR DXTR2014102101](https://openairdocs.org/sdr/DXTR2014102101), Oct 21, 2014: FITTING. CRACKED. HORIZONTAL STABILIZER FITTING ASSY CRACKED ABOVE CLIP ATTACH POINT.
- [SDR DXTA2013031805318](https://openairdocs.org/sdr/DXTA2013031805318), Mar 17, 2013: RELAY. INOPERATIVE. BRAKE FAILURE AFTER LANDING WHILE TAXIING TO THE FBO. STOPPED ACFT USING EMERGENCY BRAKES. PERFORMED SATISFACTORY RINGOUT OF HIGH PRESSURE SWITCH FOR ANTI-SKID 
- [SDR DXTA2012122105211](https://openairdocs.org/sdr/DXTA2012122105211), Dec 20, 2012: POWERPACK. FAILED. ON ROLLOUT ANTI-SKIP INOPERATIVE LIGHT ILLUMINATED. DURING TAXI IN LOW BRAKE PRESSURE LIGHT ILLUMINATED. FOLLOWED BY LOSS OF BRAKES. USED EMERGENCY BRAKING TO S
- [SDR DXTA2011060704609](https://openairdocs.org/sdr/DXTA2011060704609), Jun 7, 2011: TRUNNION. CORRODED. CORROSION FOUND ON RT LANDING GEAR RETRACT ACTUATOR TRUNNION ATTACH POINT. INSTALLED RT MLG TRUNNION ASSY REF MM 32-10-00.
- [SDR DXTA2010112904331](https://openairdocs.org/sdr/DXTA2010112904331), Nov 28, 2010: DISPLAY. FAILED. COPILOTS PFD FAILED RED X THEN BLANK SCREEN-- IT RETURNED TO OPERATING STATUS AFTER A FEW MINUTES- ALSO A VERY STRONG ELECTRICAL BURNING ODOR WAS PRESENT IN THE
- [SDR DXTA2008122403437](https://openairdocs.org/sdr/DXTA2008122403437), Dec 24, 2008: SEAL. INOPERATIVE. DOOR SEAL LIGHT ANNUNCIATOR CAME ON IN FLIGHT. DOOR SEAL INOP. PURGED DOOR SEAL WITH NITROGEN. PERFORMED CABIN ENTRY DOOR PRIMARY SEAL TEST IAW MM 52-10-04. OPS
- [SDR DXTA2008103103329](https://openairdocs.org/sdr/DXTA2008103103329), Oct 29, 2008: APU. FAILED. APU FAILED WHILE RUNNING ON THE RAMP, APU FAIL LIGHT ON. APU INOP. COCKPIT FILLED WITH SMOKE, SHUTDOWN APU, STARTED ENGINES, SMOKE CLEARED. REMOVED FAILED APU A
- [SDR DXTA200803117](https://openairdocs.org/sdr/DXTA200803117), Jun 13, 2008: BUNGEE. MALFUNCTIONED. AFTER TAKEOFF UPON GEAR RETRACTION THE NOSE GEAR (GREEN) DOWN LOCK LIGHT REMAINED ILLUMINATED. REMOVED DAMAGED NLG CENTERING BUNGEE FROM NLG AND INSTALLED NEW G
- [SDR DXTA200803032](https://openairdocs.org/sdr/DXTA200803032), Apr 29, 2008: MOTOR-BRAKE UNIT. INOPERATIVE. (PWR BRAKES) CIRCUIT BREAKER POPPED RESULTING IN LOSS OF BRAKE PRESSURE. REPLACED HYD BRAKES POWER PACK AND HIGH PRESSURE SWITCH, BLED BRAKES OPPS CHECKED SATIS
- [SDR DXTA200802984](https://openairdocs.org/sdr/DXTA200802984), Apr 7, 2008: ACTUATOR. STUCK. FLAPS WILL NOT RETRACT BEYOND 7 DEG WITH THE FLAP HANDLE IN THE 0 POSITION. RECEIVED ACFT WITH FLAPS STUCK HARD AT 15 DEGREES. ATTACHED HYDS AT EXTEND AND RETRA
- [SDR DXTA20082984](https://openairdocs.org/sdr/DXTA20082984), Apr 7, 2008: FLAP SYSTEM. MALFUNCTIONED. FLAPS WILL NOT RETRACT BEYOND 7 DEG WITH THE FLAP HANDLE IN THE 0 POSITION.
- [SDR CWQR200705](https://openairdocs.org/sdr/CWQR200705), Jul 16, 2007: CLOSEOUT PANEL. CRACKED. DURING A PHASE 5 INSPECTION, FOUND LT WHEEL WELL AFT SPAR CLOSE OUT PANEL CRACKED. (3) CRACKS WERE FOUND BEGINING FROM THE LOWER SKIN ATTACH FLANGE AND GOES STR
- [SDR CWQR200704](https://openairdocs.org/sdr/CWQR200704), Jul 16, 2007: CLOSEOUT PANEL. CRACKED. DURING A PHASE 5 INSPECTION, FOUND LT WHEEL WELL AFT SPAR CLOSE OUT PANEL CRACKED. (3) CRACKS WERE FOUND BEGINNING FROM THE LOWER SKIN ATTACH FLANGE AND GOES ST
- [SDR DXTA200701971](https://openairdocs.org/sdr/DXTA200701971), Feb 27, 2007: CABLE. OUT OF ADJUST. GEAR 'UNLOCK' LIGHT ILLUMINATED AFTER GEAR RETRACTION. CYCLED GEAR TWICE WITH SAME RESULT. HYD SYSTEM REMAINED PRESSURIZED UNTIL GEAR SELECTED DOWN. ADJUSTED & 
- [SDR DXTA200701941](https://openairdocs.org/sdr/DXTA200701941), Feb 11, 2007: ANNUNCIATOR. FAULTY. WITH GEAR SELECTED DOWN AND LOCKED (3 GREEN, NO RED) SELECTED FLAP SWITCH TO 15 AND 'HYD' PRESSURE LIGHT CAME ON FLASING WITH MASTER CAUTION FLASHING INSTANTLY 
- [SDR DXTA200701895](https://openairdocs.org/sdr/DXTA200701895), Jan 30, 2007: LANDING GEAR. MALFUNCTIONED. GEAR UNLOCKED LIGHT REMAINS ON AFTER GEAR RETRACTION. CYCLED BREAKER NO CHANGE. RETURN TO FIELD. JACKED AIRCRAFT & SWUNG GEAR SEVERAL TIMES & COULD NOT DUPLICAT
- [SDR DXTA200701882](https://openairdocs.org/sdr/DXTA200701882), Jan 27, 2007: LANDING GEAR. MALFUNCTIONED. AFTER TAKEOFF WITH GEAR SELECTED UP AND FLAPS SELECTED UP MASTER CAUTION ILLUMINATED. (HYD PRESS) (STAB MISCOPARE) AND GEAR (UNLOCK) LIGHTS ILLUMINATED. PLACED 
- [SDR DXTA200601526](https://openairdocs.org/sdr/DXTA200601526), Jul 30, 2006: ODOR. DETECTED. ENVIRONMENTAL ODOR DETECTED AFTER APU SHUTDOWN IN FLIGHT. O2 USED FOR DURATION OF FLIGHT. NO VISIBLE SMOKE NOTED. ITEM IS UNDER INVESTIGATION.
- [SDR CWQR2006016](https://openairdocs.org/sdr/CWQR2006016), Jul 28, 2006: CONTROL CABLE. FRAYED. DURING PHASE 1-4 INSPECTION, IAW OPERATOR REQUEST WE INSPECTED THE AFT ELEVATOR TRIM CABLES. UPON INSPECTION WE FOUND A SINGLE BROKEN WIRE. REMOVED CABLE AND PR
- [SDR DXTA200500965](https://openairdocs.org/sdr/DXTA200500965), Sep 12, 2005: AILERON. LOOSE. WHILE IN FLIGHT AILERON HAS 3 TO 4 INCHES OF FREE PLAY WITH NO EFFECT ON MOVEMENT OF AILERONS.
- [SDR CWQ2004F00005](https://openairdocs.org/sdr/CWQ2004F00005), Jul 23, 2004: VAPOR BARRIER. CRACKED. DURING ROUTINE PHASE INSP. 1-4 HAD TO REMOVE RT IB LE FOR ANOTHER PROBLEM (REF SCR NR 156504) BEFORE REINSTALLATION OF REPAIRED LE INSPECTED AREA AND FOUND THE 
- [SDR CWQ2004F00006](https://openairdocs.org/sdr/CWQ2004F00006), Jul 22, 2004: DIFFUSER. CRACKED. FOUND LT AND RT IB LE SKIN WHERE IT JOINS CUFF SKIN RIVETS FOUND COCKED IN HOLES WITH HEAD COCKED ABOVE SURFACE. TO REPLACE RIVETS THE LE HAD TO BE REMOVED, UPO
- [SDR DXTA200300081](https://openairdocs.org/sdr/DXTA200300081), Aug 11, 2003: LINE. CHAFED. WHILE PERFORMING NJA'S ONE TIME INSPECTION OF THE HYDRAULIC/PNEUMATIC LINES IN THE WHEEL WELLS, FOUND THE RT EMERGENCY BRAKE LINE CHAFFED THROUGH, THE LT EMEGEN

## 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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