# N650QS: 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: 680A0196
- Year built: 2019
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 13, 2019
- Certificate issued: August 31, 2026
- Expires: August 31, 2033
- Mode S code: A88E29
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=650QS
- Page: https://openairdocs.org/aircraft/N650QS

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 N650QS.

## FAA accident and incident reports

None matched to N650QS.

## 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 2025FA0000535](https://openairdocs.org/sdr/2025FA0000535), Aug 5, 2025: NUT PLATE. CORRODED. UPON REMOVAL OF 316CBC AND 316DBC FOR L5 INSTALLATION, FOUND CORROSION UNDER MULTIPLE NUTPLATES. REMOVED NUTPLATES AND BLENDED CORROSION FROM AFFECTED AREA ON A
- [SDR DXTA2024081200185](https://openairdocs.org/sdr/DXTA2024081200185), Aug 11, 2024: NONE. NONE. OVERWEIGHT LANDING: EMERGENCY LANDING. LANDED 200 LBS OVERWEIGHT AFTER DECLARING AN EMERGENCY FOR PRIMARY AND SECONDARY STAB TRIM FAILURES ON TAKEOFF. PERFORMED
- [SDR DXTA2024060711983](https://openairdocs.org/sdr/DXTA2024060711983), Jun 6, 2024: WIRE HARNESS. FAULTED. ON APPROACH, RECEIVED A RT MLG UNSAFE RED X W/ AURAL MLG & GEAR DISAGREE R CAS. RAN QRH & BLOWED DOWN MLG, GEAR INDICATED GREEN & LOCKED. LATER, RECEIVED RT MLG
- [SDR 2023F00130](https://openairdocs.org/sdr/2023F00130), May 6, 2023: PIN. CORRODED. RH MLG TRAILING LINK PIN HAS MISSING PLATING. REPORT NO. DQ39339M1 DATED MAY 5, 2023.
- [SDR 2023F00133](https://openairdocs.org/sdr/2023F00133), May 6, 2023: NUT PLATE. BROKEN. RH AFT FAIRING PANEL # 316AR HAS A BROKEN NUTPLATE IN CAPTURED FRAME P/N 6910269-48. REPORT NO. DQ39269M1 DATED MAY 3, 2023.
- [SDR 2023F00129](https://openairdocs.org/sdr/2023F00129), May 6, 2023: STABILIZER. CORRODED. REPAIR OF CORROSION ON LH HORIZONTAL STAB LOWER SKIN AT OUTBOARD TRAILING EDGE. REPORT NO. DQ39265 DATED APRIL 29, 2023
- [SDR 2023F00128](https://openairdocs.org/sdr/2023F00128), May 6, 2023: STABILIZER. CORRODED. REPAIR OF CORROSION ON RH HORIZONTAL STAB LOWER SKIN AT OUTBOARD TRAILING EDGE. REPORT NO. DQ39265 DATED APRIL 29, 2023
- [SDR 2023F00127](https://openairdocs.org/sdr/2023F00127), May 6, 2023: STABILIZER. CORRODED. REPAIR OF CORROSION ON HORIZONTAL STAB LOWER SKIN AT OUTBOARD TRAILING EDGE. REPORT NO. DQ39265 DATED APRIL 29, 2023
- [SDR 2023F00126](https://openairdocs.org/sdr/2023F00126), May 5, 2023: STABILIZER. CORRODED. REPAIR OF CORROSION ON HORIZONTAL STAB LOWER SKIN AT OUTBOARD TRAILING EDGE. REPORT NO. DQ39265 DATED APRIL 29, 2023
- [SDR 2023F00131](https://openairdocs.org/sdr/2023F00131), May 5, 2023: STABILIZER. CORRODED. REPAIR OF CORROSION ON HORIZONTAL STAB LOWER SKIN AT OUTBOARD TRAILING EDGE. REPORT NO. DQ39265 DATED APRIL 29, 2023
- [SDR 2023F00123](https://openairdocs.org/sdr/2023F00123), May 3, 2023: UNKNOWN. CHIPPED. RH HORIZONTAL WIPER DAMAGE. ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ39198M1 REV A DATED MAY 03, 2023; 680A-0196 RH HORIZONTAL WIPER DAMAGE MINOR REPA
- [SDR 2023F00122](https://openairdocs.org/sdr/2023F00122), May 3, 2023: UNKNOWN. CHIPPED. RH HORIZONTAL WIPER DAMAGE. ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ39198M1 DATED APRIL 26, 2023; 680A-0196 RH HORIZONTAL WIPER DAMAGE MINOR REPAIR.
- [SDR DXTA2022121976630](https://openairdocs.org/sdr/DXTA2022121976630), Dec 19, 2022: UNKNOWN. ODOR. DURING CLIMB OUT, A BURNING PLASTIC SMELL WAS ENCOUNTERED AND DID NOT GO AWAY UNTIL AFTER ENGINES WERE SHUT DOWN. NO SMOKE OR HAZE PRESENT AT ANY TIME. RAN AIRC
- [SDR DXTA0312202139260](https://openairdocs.org/sdr/DXTA0312202139260), Mar 11, 2021: LIGHT. FAILED. MAIN EXIT SIGN/LIGHT: WITH THE EMERGENCY LIGHTS ARMED AND THE PAX SAFETY OFF ,EXIT LIGHT REMAINS ON AT THE MAIN ENTRANCE *** CORRECTIVE ACTION *** RESET EMERGEN
- [SDR DXTA2019123093268](https://openairdocs.org/sdr/DXTA2019123093268), Dec 29, 2019: CONTROL HANDLE. DEFECTIVE. ALL LANDING GEAR EXTENSION DID NOT EXTEND, ALL LANDING GEAR DID NOT EXTEND NORMALLY. RAN THE LANDING GEAR WILL NOT EXTEND QRH AND AFTER BLOW DOWN WE HAD 3 GREEN

## Service difficulty reports on N650QS not matched to an aircraft (16)

They name N650QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA200803053](https://openairdocs.org/sdr/DXTA200803053), May 11, 2008: CONNECTOR. CONTAMINATED. NO TAKEOFF WARNING AND HORN , CAME ON AFTER JUST PASSING 70 KNTS. C/W FUNCTIONAL CHECK OF THE NO TAKEOFF SYSTEM. NO FAULTS FOUND. INSPECTED SPEEDBRAKE STOW SWIT
- [SDR DXTA20082908](https://openairdocs.org/sdr/DXTA20082908), Mar 2, 2008: TRIM TAB. MISRIGGED. TRIM INDICATOR GOES .5 IN BEYOND FWD WHITE BAND AND ONLY BACK AS FAR AS THE O IN (TO) EXCESSIVE FWD CONTROL PRESSURES REQUIRED DURING TAKEOFF WITH INDICATOR IN 
- [SDR DXTA200802859](https://openairdocs.org/sdr/DXTA200802859), Feb 10, 2008: UPLOCK SWITCH. INOPERATIVE. AFTER TAKEOFF, THE GEAR UNLOCK LIGHT, STAB MISCOMPARE AND HYD PRESS ANNUNCIATORS ILLUMINATED CONTINUOUSLY AFTER THE GEAR HANDLE WAS RAISED TO THE (UP) POSITION.
- [SDR DXTA200802849](https://openairdocs.org/sdr/DXTA200802849), Feb 7, 2008: UPLOCK SWITCH. OUT OF ADJUST. AFTER TAKEOFF , THE GEAR UNLOCK LIGHT ANNUNCIATOR ILLUIMINATED CONTINUOSLY AFTER THE GEAR HANDLE WAS RAISED TO THE UP POSITION. ADJUSTED L/R MAIN UPLOCK SWITCHE
- [SDR DXTA200702576](https://openairdocs.org/sdr/DXTA200702576), Oct 27, 2007: UPLOCK. INOPERATIVE. AFTER NORMAL T/O AND GEAR RETRACTION, THE HYD PRESSURE AND GEAR UNLOCK ANNUNCIATOR REMAINED ILLUMINATED. REMOVED THE NOSE GEAR UPLOCK ACTUATOR AND REPLACED WITH
- [SDR DXTA200702564](https://openairdocs.org/sdr/DXTA200702564), Oct 23, 2007: BYPASS VALVE. INOPERATIVE. AFTER NORMAL T/O FOLLOWING SOP'S GOT A FLASHING MASTER CAUTION HDG, STAB MISCOMPARE. REMOVED AND REPLACED BYPASS AND LANDING VALVE IAW MM 29-11-04 GROUND AND LE
- [SDR DXTA200702548](https://openairdocs.org/sdr/DXTA200702548), Oct 16, 2007: UPLOCK SWITCH. MALFUNCTIONED. AFTER GEAR RETRACTION,GEAR UNLOCK LIGHT AND HYD PRESS ANNUNCIATOR REMAINED ILLUMINATED. REMOVED AND REPLACED NJG UPLOCK SWITCH. IAW CE 560XL M/M CHPT. 32-30-05.
- [SDR DXTA200702172](https://openairdocs.org/sdr/DXTA200702172), May 2, 2007: CONTROL UNIT. INOPERATIVE. ON TAKE OFF ROLL, THE RT WINDSHIELD FAULT ANNUNCIATOR ILLUMINATED. REMOVED AND REPLACED POWER CONTROL UNIT ON RT ENG, OPS CHECK GOOD IAW CE 560XL M/M CH 24-20-0
- [SDR CWQR2006006](https://openairdocs.org/sdr/CWQR2006006), Mar 8, 2006: DRAIN VALVE. LOOSE. FOUND THE STATIC SYSTEM DRAIN VALVE POPPET RETAING RING COMING LOOSE FROM VALVE BASE.
- [SDR DXTA200501122](https://openairdocs.org/sdr/DXTA200501122), Nov 14, 2005: BRAKE ASSY. MALFUNCTIONED. TAXIING OUT FOR DEPARTURE FROM TEB, WHILE MAKING RIGHT TURN AIRCRAFT WOULD NOT RESPOND & SUDDENLY MOVED TO THE LEFT. PRESSING ON THE RIGHT BRAKE WAS A RESISTANC
- [SDR DXTA200500992](https://openairdocs.org/sdr/DXTA200500992), Sep 29, 2005: CONVERTER. MALFUNCTIONED. SHORTLY AFTER TAKEOFF, AN ODOR PERMEATED THE AIRPLANE. SMELLED ELECTRICAL, BUT NO SMOKE OR VISIBLE INDICATIONS. SIC'S EYES WERE BURNING, PIC HAD SLIGHT HEADACHE
- [SDR DXTA200500561](https://openairdocs.org/sdr/DXTA200500561), Jan 26, 2005: CIRCUIT BOARD. FAILED. NO GEAR INDICATION LIGHTS WHEN LANDING GEAR EXTENDED. GEAR CIRCUIT BREAKER POPPED. DURING CHECKLIST, WHEN C/B WAS RESET, MOMENTARILY GOT 3 GREEN LIGHTS, THEN C/
- [SDR DXTA200500552](https://openairdocs.org/sdr/DXTA200500552), Jan 23, 2005: HANDLE. STUCK. COULD NOT RAISE GEAR HANDLE TO RETRACT GEAR AFTER T/O. INSPECTED GEAR HANDLE AND FOUND IT TO BE BINDING. REMOVED GEAR HANDLE WHEEL AND CLEANED SLIDING SAFETY SH
- [SDR DXTA200500551](https://openairdocs.org/sdr/DXTA200500551), Jan 22, 2005: WIRE HARNESS. CHAFED. DURING APPROACH, SELECTED GEAR DOWN, HEARD THE GEAR DEPLOY BUT GOT NO SAFE LIGHT INDICATION. GEAR WARN C/B POPPED & RESET IT TO FIND 3 GREEN, LANDED NORMAL. TRO
- [SDR DXTA200500557](https://openairdocs.org/sdr/DXTA200500557), Jan 18, 2005: DOWNLOCK SWITCH. MALFUNCTIONED. DID NOT GET ANY GEAR INDICATION LIGHTS WHEN LANDING GEAR WAS EXTENDED GEAR CIRCUIT BREAKER WAS POPPED. RESET C/B & IT POPPED AGAIN. RESET C/B A 2ND TIME AND IT 
- [SDR DXTA200400257](https://openairdocs.org/sdr/DXTA200400257), Mar 6, 2004: CAP. LOOSE. AFTER TAKEOFF RED GEAR UNLOCK LIGHT WILL NOT GO OUT WHEN GEAR HANDLE IS SELECTED UP. CYCLED GEAR 2 TIMES WITH NO CHANGE, ACCOMPLISHED AIR TURNBACK AND LANDED WI

## 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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