# N624QS: 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: 680A0232
- Year built: 2019
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 17, 2019
- Certificate issued: April 29, 2026
- Expires: April 30, 2033
- Mode S code: A82688
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=624QS
- Page: https://openairdocs.org/aircraft/N624QS

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 N624QS.

## FAA accident and incident reports

None matched to N624QS.

## Reports on N624QS not matched to an aircraft (1)

They name N624QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 20141003017989I](https://openairdocs.org/incident/20141003017989I), Oct 3, 2014: Cessna 560XL (N624QS), St. Paul, MN, No damage. According to the pilots, on a flight from cle to stp, at approximately 20 to 25 miles out from stp the low oil pressure light for the right engine illuminated.…

## Service difficulty reports (14)

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 DXTA2026060208281](https://openairdocs.org/sdr/DXTA2026060208281), May 30, 2026: ELEC CONNECTOR. DISCONNECTED. EMERGENCY LIGHT OUT AT SEAT 8. FOUND SEAT 8 EMER LIGHT DISCONNECTED, RE-CONNECTED LIGHT CONNECTOR, AND OPS GOOD. WORK PERFORMED IN REF TO CE 680A AMM 33-20-05, 
- [SDR DXTA2025020702220](https://openairdocs.org/sdr/DXTA2025020702220), Feb 3, 2025: BATTERY. INOPERATIVE. CABIN EMERG LIGHT: BATTERIES HOOKED UP. NO POWER TO AIRCRAFT. TURNING THE EMERGENCY LIGHTS SWITCH TO ON. EMERGENCY LIGHTS COME ON EXCEPT FOR THE TWO RED EXIT LI
- [SDR DXTA2024122301581](https://openairdocs.org/sdr/DXTA2024122301581), Dec 17, 2024: BATTERY. DAMAGED. CABIN EMERG LIGHT: CENTER SECTION OF CABIN EMERGENCY LIGHTS AND OVER WING LIGHTS ARE REQUIRING A CHARGE PROCEDURE TO PASS THE PREFLIGHT TEST AND WILL NOT HOLD T
- [SDR DXTA2024081600201](https://openairdocs.org/sdr/DXTA2024081600201), Aug 13, 2024: CONTACTOR. DAMAGED. MAIN CABIN ENTRY DOOR WOULD NOT OPEN UPON ARRIVAL. PRESSED RED BUTTON AND HANDLE WOULD NOT LIFT. NO WARNINGS OR CASS MESSAGES ASSOCIATED WITH DOOR FAILING TO OP
- [SDR DXTA2024051711792](https://openairdocs.org/sdr/DXTA2024051711792), May 16, 2024: SENSING ELEMENT. DEFECTIVE. WING BLD LEAK L AMBER CAS: WING BLEAD LEAK L ILLUMINATED ON FINAL. THE MESSAGE WAS ON UNTIL WE SHUT THE AIRPLANE COMPLETELY DOWN. THE FIRE DEPARTMENT THERMAL SC
- [SDR DXTA2024040311389](https://openairdocs.org/sdr/DXTA2024040311389), Apr 2, 2024: PCB. FAULTED. AFTER WE CLOSED CABIN DOOR DOOR WOULD NOT LOCK AND THE CABIN DOOR OPEN CAS MSG REMAINED ILLUMINATED. RAN CHECKLIST (AFM 3-510-29). FAULT DID NOT CLEAR. REMOVED 
- [SDR DXTA2023073192030](https://openairdocs.org/sdr/DXTA2023073192030), Jul 31, 2023: UNKNOWN. UNKNOWN. PASSENGER / CREW DOORS: MAIN CABIN DOOR MADE A CONTINUAL CLUNKING SOUND DURING FLIGHT. SIMILAR TO THE CLUNK SOUND HEARD FROM THE VENT DOOR WHEN CLOSING THE MAIN
- [SDR DXTA2023020179600](https://openairdocs.org/sdr/DXTA2023020179600), Jan 31, 2023: NONE. NONE. RIGHT MLG LANDING GEAR RETRACTION: AFTER TAKEOFF THE RIGHT MAIN LANDING GEAR DID NOT RETRACT. ACCOMPLISHED ABNORMAL PROCEDURES CHECKLIST AND AFTER ACHIEVING 3 D
- [SDR 2022F00051](https://openairdocs.org/sdr/2022F00051), Feb 1, 2022: STINGER. CRACKED. APU STINGER DEBRIS SHIELD CRACK.
- [SDR DXTA2022011755200](https://openairdocs.org/sdr/DXTA2022011755200), Jan 4, 2022: NONE. NONE. EMERG EXIT SIGN/LIGHT: INTERIOR EMERGENCY LIGHTS AROUND MAIN CABIN DOOR AND SEAT 10 FLOOR LIGHT WILL NOT EXTINGUISH AFTER POWERING DOWN (BATTERIES DISCONNECTED 
- [SDR DXTA2021062244030](https://openairdocs.org/sdr/DXTA2021062244030), Jun 21, 2021: WHEEL. DAMAGED. NLG LANDING GEAR RETRACTION: AFTER TAKEOFF, DURING GEAR RETRACTION SEVERE VIBRATION FELT. GEAR RETRACTION TERMINATED AND LANDING LEFT EXTENDED WITH NORMAL INDIC
- [SDR DXTA2021031839630](https://openairdocs.org/sdr/DXTA2021031839630), Mar 16, 2021: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS BATTERY: EMERGENCY LIGHTS DO NOT ILLUMINATE WHEN EMER.SWITCH IS PLACED INTO ON///SIGN-OFF//REMOVED AND REPLACED EMERGENCY BATTERY PACKS. IAW 68
- [SDR DXTA2020062603814](https://openairdocs.org/sdr/DXTA2020062603814), Jun 26, 2020: CONTROL HANDLE. DEFECTIVE. THE AUTO THROTTLES WOULD NOT ENGAGE DURING TAKEOFF ROLL, AT POSITIVE RATE, CALLED GEAR UP. MLG WOULD NOT RETRACT. GEAR HANDLE CAME OUT OF DETENT AND RAISED HAND
- [SDR DXTA2020030303529](https://openairdocs.org/sdr/DXTA2020030303529), Feb 29, 2020: UNKNOWN. MALFUNCTIONED. MAIN DOOR - WHEN UNLOCKING MAIN CABIN DOOR, IT NO LONGER UNLATCH ON ITS OWN AND REQUIRE AN EXCESSIVE AMOUNT OF PULLING/PUSHING TO OPEN IT. // SIGNOFF // COMPLIE

## Service difficulty reports on N624QS not matched to an aircraft (16)

They name N624QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA2019022502072](https://openairdocs.org/sdr/DXTA2019022502072), Feb 24, 2019: DISPLAY. DEFECTIVE. DISPLAY UNIT - DURING FLIGHT INTERMITTENT HOT ELECTRICAL ODOR IN COCKPIT. AMLCD VERY HOT TO THE TOUCH. FOUND AMLCD VERY HOT TO THE TOUCH . REMOVED AND REPLACED 
- [SDR EBVR20180212001](https://openairdocs.org/sdr/EBVR20180212001), Feb 12, 2018: SKIN. DELAMINATED. DURING INSPECTION, FOUND THE LT OUTBOARD FLAP IS DELAMINATED. INSTALLED A REPAIR IAW MM 57-50-01, AND 27-51-00.
- [SDR DXTA2018011800487](https://openairdocs.org/sdr/DXTA2018011800487), Jan 17, 2018: SWITCH. FAILED. WHILE CLIMBING, THE RT THRUST REVERSER UNLOCK LIGHT CAME ON FOLLOWED BY THE ARM LIGHT. TURNED ON THE EMERGENCY STOW SWITCH PERFORMED MEMORY ITEMS FOLLOWED BY TH
- [SDR DXTA2016060306253](https://openairdocs.org/sdr/DXTA2016060306253), Jun 9, 2016: ENGINE. UNSERVICEABLE. DURING CLIMBOUT AT APPROXIMATELY 12,000 FT, THE RT ENGINE OIL PRESSURE WENT TO ZERO. IT WAS IMMEDIATELY FOLLOWED BY A RED MASTER WARNING LIGHT AND A LOW OIL PRE
- [SDR DXTA201510056100](https://openairdocs.org/sdr/DXTA201510056100), Oct 4, 2015: DISPLAY. MALFUNCTIONED. APU ON & BLEED ON, TEMP WENT RAPIDLY TO 250 DEGREES & THEN AIR DUCT O'HEAT ANNUNCIATOR ILLUMINATED, FOLLOWED BY A VERY STRONG ACRID SMOKY SMELL IN THE CABIN. BL
- [SDR DXTA2014100605905](https://openairdocs.org/sdr/DXTA2014100605905), Oct 3, 2014: ENGINE. MALFUNCTIONED. RIGHT ENGINE OIL PRESSURE WENT TO 17 PSI INFLIGHT. SHUTDOWN ENGINE. R & R THE ENGINE & OPS & LEAK CHECKED GOOD. PERFORMED A 5 POINT PERFORMANCE CHECK.
- [SDR DXTA2014100605904](https://openairdocs.org/sdr/DXTA2014100605904), Oct 3, 2014: DISPLAY. FAILED. NR 1 DISPLAY UNIT INOPERATIVE, NOTICED SMOKE AS WELL. REMOVED AND REPLACED THE NR 1 DISPLAY UNIT, OPS CHECKED GOOD. NO DEFECTS NOTED, WORK COMPLETED IAW MM 31-5
- [SDR DXTA2010020203967](https://openairdocs.org/sdr/DXTA2010020203967), Feb 1, 2010: TRIMMER. CRACKED. RIGHT AFTER LIFTOFF, EXCESSIVE FWD PRESSURE REQUIRED (FULL FWD TRIM AND BOTH HANDS ON YOKE APPLYING FWD PRESSURE). AFTER FLAP/STAB RETRACTION AND 200KTS A/S, AC
- [SDR DXTA200803105](https://openairdocs.org/sdr/DXTA200803105), Jun 8, 2008: ACTUATOR. MALFUNCTIONED. THE NOSE WHEEL GREEN LIGHT WOULDN’T GO OUT AFTER THE GEAR WAS SELECTED UP. REMOVED & REPLACED ACTUATOR, COMPLIED WITH GEAR ANGLE, RETRACTION, LEAK & BLOWDOWN CH
- [SDR DXTA200803099](https://openairdocs.org/sdr/DXTA200803099), Jun 6, 2008: SERVO VALVE. MALFUNCTIONED. LT EEC FAILED DURING TO ROLL. REMOVED AND REPLACED NR 1 ENGINE SERVO VALVE. PERFORMED OPERATIONAL CHECK AND NO DEFECTS NOTED AT THIS TIME REF MM 75-30-01 & 71-0
- [SDR DXTA200702155](https://openairdocs.org/sdr/DXTA200702155), Apr 27, 2007: RUDDER PEDAL. DAMAGED. AFTER ROTATION, THE YAW DAMPER WOULD NOT ENGAGE AND WHEN WE TURNED LT, THE LT RUDDER PEDAL WOULD NOT MOVE. AFTER ENGAGING AND DISENGAGING THE YAW DAMPER THE RUD
- [SDR DXTA200701953](https://openairdocs.org/sdr/DXTA200701953), Feb 17, 2007: WINDSHIELD. FAILED. CAPT`S WINDSHIELD SHATTERED.
- [SDR DXTA200601710](https://openairdocs.org/sdr/DXTA200601710), Nov 4, 2006: THRUST REVERSER. VIBRATION. ACCELERATING THROUGH 250KTS, FELT EXCESSIVE VIBRATION. UPON LANDING, FOUND THAT THE RT TR BUCKET NOT FLUSH WITH ENGINE COWLING. M2B- REACTIVATED RT TR UPON APPL
- [SDR DXTA200500999](https://openairdocs.org/sdr/DXTA200500999), Oct 4, 2005: ACTUATOR. INOPERATIVE. AFTER SETTING T/O POWER ON DEPARTURE ROLL RUDDER PEDALS BECOME VERY STIFF (FEELS LIKE YAW-DAMP IS ON). ABORTED TAKEOFF AT STP AFTER REACHING 60 KIAS. A/C TAXI'S
- [SDR DXTA200500792](https://openairdocs.org/sdr/DXTA200500792), Jun 20, 2005: ENGINE. MALFUNCTIONED. ON TAKEOFF WITH THROTTLE IN THE T/O DETENT, THE LT ENGINE ITT EXCEEDED 720 DEG CELSIUS WITHIN 10 SECS. THE LT ITT INDICTED 724 DEG CELSIUS AND WAS STILL SLOWLY 
- [SDR DXTA200500514](https://openairdocs.org/sdr/DXTA200500514), Jan 4, 2005: LIMIT SWITCH. FAILED. NO TAKEOFF LIGHT WILL NOT GO OUT ON GROUND, HORN SOUNDS WHEN POWER IS ADVANCED ALL ASSOCIATED SYSTEMS CHECKED / NO PROBLEMS INDICATED. FOUND STAB POSITION SWITC

## 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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