# N919QS: 2023 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: 680A0341
- Year built: 2023
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 17, 2023
- Certificate issued: May 1, 2026
- Expires: May 31, 2033
- Mode S code: ACB989
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=919QS
- Page: https://openairdocs.org/aircraft/N919QS

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 N919QS.

## FAA accident and incident reports

None matched to N919QS.

## Service difficulty reports (4)

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 DXTA2026081309243](https://openairdocs.org/sdr/DXTA2026081309243), Aug 11, 2026: TRANSFER SYS. MALFUNCTIONED. ON RAMP, FUEL 300LBS, LT TANK HEAVY. CROSSFEED TO LT TANK UTILIZED ON TAXI OUT. FUEL IN NORMAL POSITION ON TAKEOFF. 220 LBS HEAVY ON THE LT TANK. CLIMBING OUT, 
- [SDR 2024F00103](https://openairdocs.org/sdr/2024F00103), Mar 31, 2024: STRUCTURE. DAMAGED. WHILE PERFORMING SB680A-52-11 FOUND 2 OVERSIZE HOLES IN BAGGAGE DOOR STRUCTURE COMMON TO THE SNUBBER BACKET PN 7412078-5. ACCOMPLISHED TEXTRON AVIATION REPAIR L
- [SDR 2024F00102](https://openairdocs.org/sdr/2024F00102), Mar 31, 2024: STRUCTURE. DAMAGED. OVERSIZE HOLES IN BAGGAGE DOOR STRUCTURE COMMON TO THE SNUBBER BACKET PN 7412078-5.
- [SDR 2024F00105](https://openairdocs.org/sdr/2024F00105), Mar 30, 2024: SKIN. DELAMINATED. THE 7422086-3 LH WING UPPER SKIN BOND ASSEMBLY INSTALLED ON 680A-0341 ESCAPED TO THE FIELD WITH A POSSIBLE NONCONFORMING FINISH ON THE 6922462-1 STRINGER 5. TES

## Service difficulty reports on N919QS not matched to an aircraft (28)

They name N919QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTAT2PL6D005ETFY](https://openairdocs.org/sdr/DXTAT2PL6D005ETFY), Oct 5, 2017: HYDRAULIC LINE. LEAKING. HYDRAULIC VOLUME LOW A CAS MESSAGE IN FLIGHT. EMERGENCY GEAR EXTENTION USED AS WELL AS EMERGENCY BRAKE SYSTEM. HYDRAULIC FLUID LEAKING REAR OF AIRCRAFT AS WELL 
- [SDR 2017F00078](https://openairdocs.org/sdr/2017F00078), May 5, 2017: SKIN. DENTED. HORIZONTAL STAB SKIN DENTED. REPAIR.
- [SDR DXTA2014051405771](https://openairdocs.org/sdr/DXTA2014051405771), May 7, 2014: SKIN. CORRODED. REPAIR OF LOWER WING SKIN CORROSION. REPAIRED IAW CESSNA S750-0224 11RD.
- [SDR DXTA2014011305618](https://openairdocs.org/sdr/DXTA2014011305618), Jan 13, 2014: BRAKE SYS. CONTAMINATED. DURING LANDING ROLLOUT & BRAKE APPLICATION, ACFT PULLED SEVERELY TO THE LEFT THEN RIGHT. ACFT DIRECTIONAL CONTROL WAS VERY DIFFICULT. BRAKES GRABBED UNCOMFORTAB
- [SDR DXTA201305060571](https://openairdocs.org/sdr/DXTA201305060571), May 3, 2013: O-RING. TORN. LOST A SYS HYD SYS. QUANITY DROPPED BELOW 14 PERCENT FOLLOWED BY ASSOCIATED CAS MSG. "A" PRESSURE WENT TO ZERO. FOLLOWED CHECKLIST, BLEW GEAR DOWN. HYD FLUID LE
- [SDR DXTA2012080805080](https://openairdocs.org/sdr/DXTA2012080805080), Mar 15, 2012: SKIN. CORRODED. WINGS HAVE MULTIPLE CORROSION SITES ON THE FUEL PANEL WING LANDS. ACCOMPLISHED ALL REPAIRS ON LEFT AND RIGHT WING FUEL PANEL WING LANDS IAW MM 57-20-01 AND REPA
- [SDR DXTA2011030304487](https://openairdocs.org/sdr/DXTA2011030304487), Mar 2, 2011: STRUT. LOW PRESSURE. LANDING GEAR FAILED TO RETRACT ON TAKEOFF. CHECKED STRUT PRESSURES AND FOUND NLG STRUT LOW. SERVICED NLG STRUT IAW AMM 12-10-38. PERFORMED GEAR SWINGS IAW AMM 3
- [SDR DXTA2010120604347](https://openairdocs.org/sdr/DXTA2010120604347), Dec 3, 2010: STRUT. DISCHARGED. GEAR HANDLE WOULD NOT COME UP AFTER TAKEOFF. FOUND NOSE STRUT LOW, SERVICED NOSE STRUT IAW MM 12-10-38. CYCLED LANDING GEAR. NLG OPS CHECKED AND LEAK CHECKED GO
- [SDR DXTA2010072604179](https://openairdocs.org/sdr/DXTA2010072604179), Jul 22, 2010: A/C PACK. SMOKE. WITH APU RUNNING ON GROUND, COCKPIT PAC SELECTED OFF, CABIN PAC ON HIGH AND APU BLEED SELECTED TO HIGH FLOW, SMOKE ENTERED COCKPIT THROUGH WEMACS. COCKPIT TEMP 
- [SDR DXTA2010011803948](https://openairdocs.org/sdr/DXTA2010011803948), Jan 14, 2010: LINKAGE. DISCONNECTED. ON VISUAL APPROACH, THE FLYING CO-PILOT COMPLAINED THE ACFT WAS OUT OF RIG; WANTED TO ROLL RIGHT WITH FLAPS AT 35 DEG. ON POST FLIGHT WE DISCOVERED THE RIGHT FL
- [SDR DXTA2009122103902](https://openairdocs.org/sdr/DXTA2009122103902), Dec 20, 2009: COMPRESSOR. SEIZED. WHILE DESCENDING THROUGH FL320, A LOUD DULL THUD WAS HEARD, FOLLOWED CLOSELY BY AN ACRID ODOR AND A GREYISH HAZE . THE HAZE AND ODOR RETURNED ON THE GROUND WITH
- [SDR DXTA2009082803767](https://openairdocs.org/sdr/DXTA2009082803767), Aug 27, 2009: WARNING MESSAGE. ILLUMINATED. CLIMBING THROUGH 10,000 FT THE AMBER "PITCH FEEL FAIL" CAS MESSAGE CAME ON AND REMAINED ON FRO APPROX 15 MINUTES. PITCH CONTROL FELT NORMAL WHILE HAND FLYING. C
- [SDR DXTA2009070803723](https://openairdocs.org/sdr/DXTA2009070803723), Jul 7, 2009: COALESCER BAG. ODOR. COALESCER CLOTHS SMELL FOUL, MORE NOTICEABLE FROM COCKPIT PAC, AND SLIGHT BURNED ODOR AS WELL. REMOVED AND CLEANED COALESCER CLOTHS IAW THE MM TASK 12-10-01-160
- [SDR DXTA2009051403651](https://openairdocs.org/sdr/DXTA2009051403651), May 13, 2009: BRAKE. FAULTY. ON LANDING ROLL OUT, LT BRAKE IS HYPER SENSITIVE TO INPUTS AND IS ALMOST UNUSABLE BECAUSE IT GRABS VIOLENTLY. INSPECTED THE LTH MLG BRAKES, NO DEFECTS NOTED. ME
- [SDR DXTA2008122103424](https://openairdocs.org/sdr/DXTA2008122103424), Dec 21, 2008: FLAP SYSTEM. MALFUNCTIONED. DURING APPROACH TO LAND, RECEIVED "FLAPS FAIL" MESSAGE WHEN SELECTING 15 DEGREE. COMPLETED CHECKLIST AND UNABLE TO FIX PROBLEM. DIVERTED AND MADE A FLAPS 5 DEGR
- [SDR DXTA2008122303424](https://openairdocs.org/sdr/DXTA2008122303424), Dec 21, 2008: WARNING LIGHT. ILLUMINATED. DURING APPROACH TO LAND, RECEIVED "FLAPS FAIL" MESSAGE WHEN SELECTING 15*.
- [SDR DXTA200802847](https://openairdocs.org/sdr/DXTA200802847), Feb 7, 2008: ACTUATOR. MALFUNCTIONED. FOLLOWING GEAR RETRACTION AFTER TAKEOFF, THE GREEN NOSE GEAR DOWN LIGHT REMAINED ILLUMINATED. REPLACED NLG ACTUATOR IAW MM CH 32-30-03 OPS AND LEAK CHECK GOOD.
- [SDR DXTA200802818](https://openairdocs.org/sdr/DXTA200802818), Jan 31, 2008: RESOLVER. OUT OF ADJUST. FLAPS FAILED AT 15 DEGREES, PUSHED RESET BUTTON AND FLAPS REMAINED FAILED. FOUND BITES 1, 2 AND 9 ILLUMINATED. RESET CONTROLLER, FLAPS WORKED NORMALLY. TROUBLES
- [SDR DXTA200802751](https://openairdocs.org/sdr/DXTA200802751), Jan 8, 2008: LIMITER. MALFUNCTIONED. RUD LIMIT FAIL A AMBER CAS ILLUMINATED AFTER TAKEOFF AT APPROX 15000 FT. LIMIT WAS 22 PERCENT. R & R RUDDER TRAVEL LIMITERS IAW MM CH 27-23-00. OPS CK GOOD IAW 
- [SDR DXTA200702686](https://openairdocs.org/sdr/DXTA200702686), Dec 17, 2007: CONTROLLER. FAILED. AFTER TAKE-OFF, RETRACTED THE FLAP, THE FLAPS FAILED. TROUBLESHOT TO AN INTERNALLY FAILED FLAP CONTROLLER. REPLACED CONTROLLER WITH AN INSPECTED UNIT. FUNCTIONA
- [SDR DXTA200702552](https://openairdocs.org/sdr/DXTA200702552), Oct 18, 2007: SQUAT SWITCH. OUT OF ADJUST. GEAR WOULD NOT RETRACT AFTER TAKEOFF. GEAR LEVER WAS STUCK DOWN AND WOULD NOT MOVE. SERVICED NOSE STRUT & ADJUSTED NOSE GEAR SQUAT SWITCH. OP'S CHECK GOOD IAW M
- [SDR DXTA200702494](https://openairdocs.org/sdr/DXTA200702494), Sep 22, 2007: DRIVE UNIT. FAILED. FLAPS FAILED AT 5 DEGREES. REMOVED & REPLACED POWER DRIVE UNIT, OPERATIONALY CHECKS GOOD. IAW: CE750 M/M 27-50-00
- [SDR DXTA200702461](https://openairdocs.org/sdr/DXTA200702461), Sep 10, 2007: ENGINE. SMOKE. RT ENGINE IS SMOKING AFTER SHUTDOWN AND SMELLS LIKE OIL. NO LEAKS OBSERVED. OIL LEVEL 3.5 TO 4 QTS LOW AND ENGINE TEMP OK.
- [SDR DXTA200601636](https://openairdocs.org/sdr/DXTA200601636), Oct 5, 2006: CONTROL MODULE. MULTIPLE FAIL. APPARENT TOTAL ELECTRICAL FAILURE ON RT SIDE WITH ASSOCIATED INSTRUMENT FAILURES AND MANY AMBER AND CYAN CAS MESSAGES, NOSE WHEEL STEERING FAILURE AND RT T/R FA
- [SDR DXTA200500972](https://openairdocs.org/sdr/DXTA200500972), Sep 16, 2005: ACM. UNSERVICEABLE. UNABLE TO CONTROL TEMP RISE FOR CABIN PACK. SMOKE ENTERED CABIN ON LEFT SIDE OF CABIN AND TAIL CONE AREA SMELLED LIKE SOMETHING HAD BEEN BURNING. ACM WOULD NOT 
- [SDR DXTA200500578](https://openairdocs.org/sdr/DXTA200500578), Feb 4, 2005: BRAKE. SMOKE. DURING TAXI AND LANDING NOTICED BRAKES WERE VERY STICKY. ALSO AFTER PARKING NOTICED THE RIGHT SIDE MAINS, INBOARD AND OUTBOARD WERE SMOKING FOR UP TO 40 MINUTES
- [SDR DXTA200400299](https://openairdocs.org/sdr/DXTA200400299), Apr 22, 2004: PITOT LINE. CONTAMINATED. ON TAKEOFF ROLL AT APPROX 75 KNTS, THE MACH TRIM KICKED OFF AND ON, THEN THE YAW DAMPER KICKED OFF, MASTER CAUTION CAME ON, ABORT TAKEOFF. FOUND PITOT MASTS FUL
- [SDR DXTA200400278](https://openairdocs.org/sdr/DXTA200400278), Mar 27, 2004: PITOT TUBE. DAMAGED. ON TAKEOFF ROLL WITH UPPER AND LOWER YAW DAMPERS AND MACH TRIM IN A-CONFIGURATION, THE LOWER YAW DAMPER FAILED BETWEEN 50 AND 70 KTS, AMBER "YD OFF LOWER" EICAS

## 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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