- Owner type
- Co-owned, fractional ownership
- Serial number
- 680A0138
- Year built
- 2018
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- May 25, 2018
- Certificate issued
- March 3, 2026
- Expires
- March 31, 2033
- Mode S code
- A77EC5
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 N582QSMatched 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 N582QSMatched 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 · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2025122206190Pump · leakingDURING DECENT APPLIED SPEED BRAKE HANDLE TO CONTROLL SPEED. THEN THE AMBER CAS HYD VOLUME LOW MESSAGE APPEARED. DECLARED EMERGENCY AND FOLLOWED THE QRH TO AN UNEVENTFUL LANDING. PERFORMED & SUBMITTED AN ARES DOWNLOAD, ON INLTIAL WALK AROUND FOUND HYD FLULD DRISDR DXTA2025081504605Warning Light · illuminatedRED AUTO THROTTLE HOLD FAIL CAS CAME ON AT 30KTS ON TAKEOFF AND THE AUTO THROTTLES WERE REDUCING POWER AS THIS OCCURRED. PERFORMED TWO SETS OF OPS CHECKS SUCCESSFULY AND SENT AN ARES DOWNLOAD TO MCC AND TEXTRON. MCC ELECTED TO KEEP ORIGINAL A/T INSTALLED DUESDR DXTA2024111501149Door · out of adjustFUSELAGE STRUCTURE: REPEAT RIGHT UP. THERE IS A VERY PRONOUNCED AIRFRAME VIBRATION. THE VIBRATION BEGINS AT VARIOUS ALTITUDES MORE OFTEN AT FL260 AND 295KTS. THE VIBRATION REMAINS AT ANY ALTITUDE UNTIL SLOWING TO 250 KN. AT 250 KN THE VIBRATION SLOWLY DISSIPASDR DXTA2023072491450Unknown · unknownFLOOR EMERG EXIT LIGHT: RIGHT HAND MAIN DOOR FLOOR EXIT LIGHT INOP. //SIGNOFF// RECONNECTED LOOSE WIRE OF RH MAIN DOOR EXIT EMERG LIGHT. WORK IN REF TO CE680A AMM 33-50-00. OPS CHECK GOOD.SDR DXTA2022122777210Switch · trippedWITH ALL AIRCRAFT POWER REMOVED AND EMER LIGHT SWITCH IN THE OFF POSITION THE EMER LIGHTS AT MAIN CABIN DOOR AREA AND BELOW SEAT 10 REMAIN ILLUMINATED. CYCLED THE EMER LIGHT SWITCH AND AIRCRAFT POWER AND PROBLEM REMAINS. UPON ARRIVAL, ALL. EMER LIGHTS DISGUISDR DXTA2022090970020None · noneEMERG EXIT SIGN/LIGHT: ON POST FLIGHT THE EMER EXIT SIGN OVER THE MAIN CABIN DOOR AND THE FLOOR LIGHTING INDER SEAT 10 IS ILLUMINATED. // SIGNOFF// RESOLUTION: ARRIVED AT AIRCRAFT IN TIME VERIFYING FWD ERNER BATT LIGHTS STILL ILLUMINATED. ACCESSED AS NECESSARSDR 2022F00157None · gougedR/H UPPER COWL GOUGED BY O/B BLEED AIR CLAMP AT AFT BLEED AIR COUPLING. TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ34079M1. DATED. MARCH 22, 2022. 680A-0138 (N582QS) ENGINE UPPER COWL (LEFT AND RIGHT) DAMAGE (GOUGE).SDR 2022F00151None · gougedL/H UPPER COWL GOUGED BY O/B BLEED AIR CLAMP AT AFT BLEED AIR COUPLING. TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ34079M1, DATED. MARCH 22,2022. 680A-0138 (N582QS) ENGINE UPPER COWL (LEFT AND RIGHT) DAMAGE (GOUGE).SDR 2022F00159None · chafedRH MLG ACTUATOR UPPER ATTACH FITTING GOUGED FROM CONTACT WITH ACTUATOR LUG. TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ34051M1, DATED: MARCH 21, 2022. 680A-0138 (N528QS) RIGHT MAIN LANDING SIDE BRACE ACTUATOR INBOARD FITTING CHAFE DAMAGE.SDR DXTA2021052042310G Switch · trippedFLOOR EMERG EXIT LIGHT: FLOOR LIGHT UNDER SEAT 10 WILL NOT EXTINGUISH. THE 3 EXIT SIGNS ON MAIN CABIN DOOR ALSO WON'T EXTINGUISH "CORRECTIVE ACTION" FOUND FWD "G" SWITCH ON THE R/H AFT CENTER PEDESTAL TO BE TRIPPED. RESET SWITCH AND STATED EMERGENCY LIGHTS EXSDR 2020F00373Doubler · crackedREPAIR TO NOSE LANDING GEAR WHEEL WELL CRACKS. TEXTRON AVIATION STANDARD REPAIR SR-680A-ATA53-25890 DATED 06/01/2020, STANDARD REPAIR-CRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW), FRAME, WEB, AND DOUBLERS, FS 75 WITH FAA FORM 8100-9 DATED 06/01/2020.SDR DXTA2020011303333Unknown · odorCOCKPIT ODOR - CLIMBING THROUGH 300FT TURNED ENGINE ANTI ICE ON AND NOTICED A FUME SMELL ABOUT 500FT. TURNED ENGINE ANTI ICE OFF AFTER ABOUT 2 MINUTES WHEN WE CLIMBED ABOVE THE THIN CLOUD LAYER. SMELL DID SEEM TO DISSIPATE A LITTLE BUT WAS STILL VERY NOTICEABLSDR DXTA2018071301172Proximity Switch · defectiveLEFT MAIN LANDING GEAR FAILED TO RETRACT. DOWN DISPLAYED IN YELLOW ON LEFT MAIN. UP DISPLAYED IN WHITE ON RIGHT MAIN AND NOSE GEAR. UPON COMPLETION OF CHECK LIST THREE DOWN GREEN INDICATION RESULTED IN A SAFE UNEVENTFUL LANDING. R&R MLG UPLOCK SWITCH P/N 69481
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