# N690QS: 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: 680A0223
- Year built: 2019
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 4, 2019
- Certificate issued: January 16, 2025
- Expires: January 31, 2032
- Mode S code: A92C25
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=690QS
- Page: https://openairdocs.org/aircraft/N690QS

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 N690QS.

## FAA accident and incident reports

None matched to N690QS.

## 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 DXTA2026092809868](https://openairdocs.org/sdr/DXTA2026092809868), Sep 24, 2026: LANDING GEAR. FAULTED. ON APPROACH TO KCHS, SELECTED MLG DOWN & GOT 3 GREEN INDS, RECEIVED WOW MISCOMPARE CAS MESSAGE, ELECTED TO GO AROUND, ON GO AROUND, SELECTED MLG UP, HAD 3 GREEN
- [SDR DXTA2026031707275](https://openairdocs.org/sdr/DXTA2026031707275), Mar 13, 2026: LINK. CRACKED. MAIN LANDING GEAR TRAILING LINK ENHANCED INSPECTION LT MLG TRAILING LINK CRACKED INSIDE ON THE BOTTOM OF THE TRAILING LINK. REPLACED TRAILING LINK. OPS CHECK GO
- [SDR DXTA2025112605835](https://openairdocs.org/sdr/DXTA2025112605835), Nov 24, 2025: BATTERY. INOPERATIVE. AFT EMERGENCY LIGHTS WILL NOT EXTINGUISH. EVEN WITH MAIN SHIP BATTERIES PULLED, AND FIVE G RESET SWITCH PRESSED. REMOVED AND REPLACED # 4 EMERGENCY LIGHT BATTER
- [SDR DXTA2025100705214](https://openairdocs.org/sdr/DXTA2025100705214), Oct 6, 2025: G SWITCH. TRIPPED. REAR EMERGENCY LIGHTS WILL NOT SHUT OFF CORRECTIVE ACTION: VERIFIED DISCREPANCY. GAINED ACCESS TO #4 EMER BATTERY G-SWITCH. RESET G-SWITCH AND LIGHTS WENT OUT I
- [SDR DXTA2025060203726](https://openairdocs.org/sdr/DXTA2025060203726), Jun 1, 2025: BATTERY PACK. INOPERATIVE. THE EMERGENCY LIGHTS ASSOCIATED WITH THE #4 BATTERY PACK ARE NOT WORKING, EVEN AFTER TWO 30 MIN CHARGE CYCLES PER THE QRH. LIGHTS AFFECTED ARE AFT BULKHEAD EXIT
- [SDR DXTA2024091600545](https://openairdocs.org/sdr/DXTA2024091600545), Sep 14, 2024: PRESSURE SWITCH. FAILED. FUEL FLTR BYPASS L AMBER CAS: AT FL410 RECEIVED AMBER FUEL FILTER BYPASS L CAS MESSAGE. COMPLIED WITH QRH AND DIVERTED TO KLEX. NO ISSUES DURING THE DIVERSION N
- [SDR DXTA2023083094210](https://openairdocs.org/sdr/DXTA2023083094210), Aug 29, 2023: UNKNOWN. UNKNOWN. WORN BRAKES: WHEEL BRAKES MAKE A LOUD RUBBING NOISE AND VIBRATION AFTER LANDING WHEN HOT AND WHEN SLOWING TO A STOP PERFORMED INSPECTION OF ALL MLG BRAKE ASSEMB
- [SDR DXTA2023012779240](https://openairdocs.org/sdr/DXTA2023012779240), Jan 26, 2023: HINGE. BROKEN. ENTRANCE STAIR: TOP ENTRANCE STEP IS DETACHED FROM THE DOOR. REMOVED CABIN DOOR HINGE STEP X3 HINGES. INSTALLED CABIN DOOR STEP HINGE IAW MM 25-20-09
- [SDR DXTA2023010677960](https://openairdocs.org/sdr/DXTA2023010677960), Jan 5, 2023: OUTLET. SPARKS. 5 VDC 3 AMP USB OUTLET ADJACENT TO SEAT 6 SPARKED AND EMITTED ELECTRICAL BURNING ODOR WHEN USB CORD WAS PLUGGED IN. REINSTALLED PASSENGER SEAT #6 OUTLET ASSY PA
- [SDR DXTA2022120175220](https://openairdocs.org/sdr/DXTA2022120175220), Nov 30, 2022: LIGHT. MALFUNCTIONED. EXIT LIGHT OVER MAIN DOOR AND TOE KICK LIGHT UNDER 10 ILLUMINATED WITH SWITCH OFF AND BATTERIES DISCONNECTED.
- [SDR 2022FA0000240](https://openairdocs.org/sdr/2022FA0000240), Apr 29, 2022: NONE. DENTED. CUSTOMER REPORTS THE RH ELEVATOR END CAPS ARE DAMAGED/DENTED AND IS REQUESTING TO COLD WORK BACK TO ORIGINAL CONTOUR. NETJETS REQUEST FOR TECHNICAL SERVICES (RF
- [SDR 2022FA0000239](https://openairdocs.org/sdr/2022FA0000239), Apr 29, 2022: NONE. DENTED. CUSTOMER REPORTS THE RH ELEVATOR END CAPS ARE DAMAGED/DENTED AND IS REQUESTING TO COLD WORK BACK TO ORIGINAL CONTOUR. NETJETS REQUEST FOR TECHNICAL SERVICES (RF
- [SDR 2022FA0000038](https://openairdocs.org/sdr/2022FA0000038), Jan 20, 2022: NONE. GOUGED. RH FUSELAGE SKIN HAS 1 DRILL START AT APPROXIMATELY FS 440.81 BEHIND SPLICE STRAP. ACCOMPLISHED MINOR REPAIR TO RIGHT TAILCONE SKIN P/N: 7412023-12 IAW TEXTRON 
- [SDR 2022FA0000037](https://openairdocs.org/sdr/2022FA0000037), Jan 20, 2022: NONE. NONE. LEFT FUSELAGE BOND ASSEMBLY P/N: 7411391-1 CHAFED. ACCOMPLISHED MINOR REPAIR TO LEFT FUSELAGE BOND ASSEMBLY P/N: 7411391-1 IAW TEXTRON AVIATION ENGINEERING MEMO
- [SDR DXTA2021112452440](https://openairdocs.org/sdr/DXTA2021112452440), Nov 23, 2021: NONE. NONE. MAIN DOOR: AMBER CAS DISPLAYED . DOOR IS CLOSED . RESET CHECK DIDNT WORK. COMPLETE SHUT DOWN TO RESET DIDNT WORK EITHER . // SIGNOFF // MAIN DOOR: AMBER CAS DIS

## Service difficulty reports on N690QS not matched to an aircraft (17)

They name N690QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA200803160](https://openairdocs.org/sdr/DXTA200803160), Jul 4, 2008: UNKNOWN. ODOR. SHORTLY AFTER TAKEOFF CREW COULD DETECT AN ELECTRICAL ODOR. AFTER LANDING, COULD DETECT THE ODOR IN AFT CABIN AND LUGGAGE COMPARTMENT. COULD NOT DETECT IT IN HE
- [SDR DXTA200802825](https://openairdocs.org/sdr/DXTA200802825), Feb 3, 2008: OXYGEN MASK. LEAKING. CAPT'S 02 MASK HOSE DEVELOPED A LEAK WHERE IT ATTACHES TO MASK AND COULD NOT STOP LEAK. INSTALLED NEW O2 MASK. OPS CHECK GOOD IAW MM CH 35-10-01. (K)
- [SDR DXTA200702634](https://openairdocs.org/sdr/DXTA200702634), Nov 28, 2007: PUSHROD. LOOSE. RACHETING FEELING IN YOLK WHILE TURNING LT OR RT. MORE NOTICABLE DURING LT TURNS. MUCH MORE NOTICEABLE AT HIGH SPEEDS. OCCASIONALLY FEELS LIKE CONTROLS ARE STIC
- [SDR DXTA200702070](https://openairdocs.org/sdr/DXTA200702070), Apr 3, 2007: EEC. FAILED. LT EEC FAILED TO MANUAL ON TAKEOFF ROLL AT 40 KIAS. TWO TIMES. ABORTED TAKE OFF. REMOVED BLEED SERVO AND INSTALLED NEW SERVO SN TR2508 IAW PW MM CH 75-50-01. OP
- [SDR DXTA200701993](https://openairdocs.org/sdr/DXTA200701993), Mar 3, 2007: MOTOR. FAILED. NR 2 ENGINE EEC FAILED AFTER DEPARTURE PASSING THROUGH 10,000 FEET. AFTER CHECKLIST ITEMS WERE COMPLETE ENGINE COMPRESSOR STALLS CONTINUED. VERIFIED DISCREPANCY
- [SDR DXTA200601669](https://openairdocs.org/sdr/DXTA200601669), Oct 18, 2006: ACTUATOR. BINDING. RUDDER PEDAL HAVE BINDING/SHUTTERING FEEL DURING SLOW/LOW SPEED TAXI. ON TAKEOFF ROLL PEDALS FEEL STIFF AS IF YAW DAMPER WERE ENGAGED. REMOVED RUDDER BIAS ACTUA
- [SDR CWQR2006015](https://openairdocs.org/sdr/CWQR2006015), Jul 17, 2006: CABLE. FRAYED. DURING A SCHEDULED INSP ON THIS AIRCRAFT THE OPERATOR REQUESTED THAT WE INSPECT THE AFT CABLES ON THE ELEVATOR TRIM SYSTEM. PRIOR TO REMOVAL WE CHECKED THE CABL
- [SDR DXTA200400334](https://openairdocs.org/sdr/DXTA200400334), Jul 9, 2004: SELECTOR KNOB. OUT OF POSITION. DURING CRUISE AT 22,000 FT, MASTER WARNING CAME ON FOR LOSS OF CABIN PRESSURIZATION. DECLARED EMERGENCY AND DESCENDED DOWN TO 10,000 FT, PROBLEM WENT AWAY. DIVE
- [SDR DXTA200400296](https://openairdocs.org/sdr/DXTA200400296), Apr 18, 2004: LANDING GEAR. MALFUNCTIONED. SELECTED GEAR UP ON TAKEOFF, GEAR FAILED TO RETRACT, INDICATION SHOWED 3 GREEN 1 RED UNLOCK LIGHT . SELECTED GEAR DOWN, 3 GREENS RED EXTINGUISHED, ACCOMPLISHED 
- [SDR DXTA200400295](https://openairdocs.org/sdr/DXTA200400295), Apr 17, 2004: LIGHT. INOPERATIVE. DURING APPROACH SELECTED GEAR DOWN AND DID NOT GET A SAFE GEAR INDICATION FOR THE RIGHT MAIN GEAR. PERFORMED THE EMERGENCY CHECKLIST AND BLEW GEAR DOWN BY PNEUM
- [SDR DXTA200300184](https://openairdocs.org/sdr/DXTA200300184), Nov 22, 2003: CONTROL CABLE. CHAFED. PERFORMED AILERON WING CABLE INSPECTION PER CESSNA ASL560XL-27-12, FOUND CABLES CHAFED/BROKEN BEYOND MANUFACTURER'S LIMITS. REMOVED AND REPLACED LEFT AND RIGHT 
- [SDR DXTA200300161](https://openairdocs.org/sdr/DXTA200300161), Nov 9, 2003: STRUT. DAMAGED. AFTER TAKEOFF DURING GEAR RETRACTION GEAR UNLOCK LIGHT STAYED ON. TROUBLESHOT AND FOUND NOSE STRUT NOT FULLY EXTENDING WITH WEIGHT OFF WHEELS. REMOVED STRUT AND
- [SDR DXTA200300125](https://openairdocs.org/sdr/DXTA200300125), Sep 22, 2003: BELLCRANK. MISINSTALLED. DURING ENGINE RUN FOR POST INSTALLATION OF MFG SB 560XL7603R1 (THROTTLE CUT OFF IMPROVEMENT) FOUND ENGINES FAILED TO STAY IN FLIGHT IDLE, WHEN POWER IS REDUCED 
- [SDR DXTA200300041](https://openairdocs.org/sdr/DXTA200300041), Jun 3, 2003: GROUND WIRE. DAMAGED. LEFT ENGINE FIRE WARNING LIGHT ILLUMINATED DURING CLIMB THRU FL260 WITH ENGINE/WING ANTI-ICE ON. REDUCED POWER TO 72 PERCENT ON EFFECTED ENGINE AND LIGHT EXTING
- [SDR DXTA200300039](https://openairdocs.org/sdr/DXTA200300039), Jun 1, 2003: TUBE. LEAKING. LT ENGINE FIRE WARNING LIGHT ILLUMINATED ON CLIMBOUT AT 14,000 FT. TROUBLESHOT FIRE DETECTION SYSTEM. PERFORMED FIRE LOOP CONTINUITY RESISTANCE CHECK IAW CE-560
- [SDR DXTA200300036](https://openairdocs.org/sdr/DXTA200300036), May 24, 2003: FIRE LOOP. MISROUTED. DURING FLIGHT 120124-1 FROM MIA TO CHS DIVERTED TO MCO DUE TO LT ENGINE FIRE LIGHT CAME ON AT FL240. REDUCED POWER TO HALF THROTTLE AND LIGHT EXTINGUISHED, NO E
- [SDR 20010129CW016](https://openairdocs.org/sdr/20010129CW016), Jan 8, 2001: TORQUE TUBE. CORRODED. AFT AILERON SECTOR TORQUE TUBE CORRODED THE LENGTH OF THE TUBE BETWEEN THE UPPER AND LOWER BELLCRANKS.

## 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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