- Owner type
- Co-owned, fractional ownership
- Serial number
- 680A0182
- Year built
- 2019
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- February 22, 2019
- Certificate issued
- April 14, 2026
- Expires
- April 30, 2033
- Mode S code
- A85575
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 3
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2018 | 1 |
|---|---|
| 2023 | 1 |
| 2026 | 1 |
Information bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N636QSMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Textron 680A aircraft
FAA incident reports
No FAA accident or incident reports matched to N636QSMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Textron 680A aircraft
Service difficulty reports · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026101910213Light · inoperativeSEAT 5 TOE KICK LIGHT NOT WORKING. EXTERIOR EMER LIGHTS CONSIDERED INOP PER MEL GAINED ACCESS TO TOE KICK LIGHT THROUGH THE SEAT ASSEMBLY AND FOUND THE LIGHT STRIP'S POWER CONNECTOR WAS UNPLUGGED AND ONE OF THE PINS WAS NOT IN THE CONNECTOR. REPINNED THE REMOSDR DXTA2026010206355Check Valve · faultedAFTER SELECTING GEAR UP ON TAKEOFF, WE RECIEVED A GEAR DISAGREE CAS MESSAGE. THE TWO MAIN GEAR SHOWED UP AND LOCKED HOWEVER THE NOSE GEAR DISPLAYED AN AMBER DN INDICATION WITH THE GEAR HANDLE IN THE UP POSITION. QRH PROCEDURE WAS COMPLIED WITH AND RESULTED WITSDR DXTA2024112501224Control Switch · damagedPARK BRAKE LOW PRESS AMBER CAS: DURING TAXI TO THE RUNWAY, WE RECEIVED A YELLOW PARK BRAKE LOW PRESS CAS MESSAGE. THIS MESSAGE OCCURRED WITH BOTH ENGINES RUNNING AND DURING MOVEMENT OF THE AIRCRAFT. WE PULLED OFF TO THE SIDE TO DIAGNOSE THE ISSUE. WHEN WE SET SDR DXTA2023122110389Battery · faultedEMER LIGHTS COMPLETELY DEAD. WE CHARGED THE BATT PACKS FOR 45 MINS ON THE APU AND RETESTED. NOT A SINGLE LIGHT CAME ON IN THE ON POSITION. ACCESSED CLOSEOUT PANEL TO THE LEFT AFT CLOSET ASSEMBLY AND REMOVED FAULTY #4 BATT PACK P/N CBS28-1 S/N 5792M, INSTALLEDSDR DXTA2023092596330Unknown · unknownAP STAB TRIM INOP AMBER CAS: PRI STAB TRIM FAIL CAS MESSAGE DISPLAYED IN LEVEL FLIGHT. IT WAS FOLLOWED BY AP STAB TRIM INOP AND AP FAIL MESSAGES. COMPLIED WITH QRH PROCEDURES.SDR DXTA2022022156960Apu · leakingAPU SMOKE: AFTER STARTING APU TURNED ON APU BLEED AIR AND THE CABIN FILLED WITH SMOKE. /// CORRECTIVE ACTION /// REMOVED AND REPLACED APU IAW AMM 49-10-00.SDR DXTA2021040540390Battery · defectiveCOCKPIT EMERG LIGHT: FRONT EMERGENCY LIGHTS REMAINS ON IN THE OFF POSITION , SUSPECT INERTIA SWITCH HAD BEEN TRIGGERED. REPLACED EMERGENCY BATTERY. IAW CE-680A AMM 33-50-00
Reports on N636QS not matched to an aircraft · 4
They name N636QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXT2007F00000Bolt · looseAIRCRAFT CAME INTO THE REPAIR STATION DUE TO THE ENGINE NR1 HIGH TT. DURING BORESCOPE INSPECTION OF THE HP COMPRESSOR AS PART OF THE TROUBLESHOOTING, THE TECHNICIAN OBSERVED 2 EACH LOOSE BOLTS (GAS GENERATOR CASE TO INTERMEDIATE CASE FLANGE, FLANGE C) THE ENSDR DXTA200601755Servo Valve · inoperativeON TAKEOFF ROLL AT ABOUT 70 KTS, THE RT EEC MANUAL LIGHT CAME ON. THE RT N2 WENT TO 102.4 FOR ABOUT 5 SEC. AFTER WE ABORTED, ALSO SAW 3 YELLOW DASH LINES ON THE RAT GAUGE. DOWNLOADED 32 ENG EEC DATA AND SENT TO MFG TECH SUPPORT. REMOVED AND REPLACED NR 2 ENG SDR DXTA200601496Relay · failedON LANDING LO BRAKE PRESS/ANTI SKID INOP LIGHT CAME ON. BRAKES FAILED AND EMERGENCY BRAKES APPLIED. ALL ECS NORMAL, ACCUMULATOR NORM, FLUID LEVEL NORM. TROUBLESHOT SYSTEM, REMOVED BRAKE CONTROL MOTOR RELAY KN003 P/N MS2416602, DUE TO INTERNAL FAILURE. REPL
STCs that may be installed · 16
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Textron 680A
STC ST04765NYUnprepared (Grass/Sod) Runway OperationsSTC ST00885LAInstallation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles.STC ST12344IBReplacement of the Halon Type 1211 portable fire extinguisher with Halotron BrX portable fire extinguisher with Halotron BrX portable fire extinguisher