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Aircraft record

N582QS2018 Textron Aviation INC 680A

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:No NTSB accidents or incidents since 19821 AD may apply13 service difficulty reports

Registration
Valid
expires Mar 31, 2033
Owners
1
since 2026
NTSB events
None
since 1982
ADs may apply
1
confirm with A&P
Service reports
13
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
Co-owners
Certificate issued
Mar 3, 2026
Expires
Mar 31, 2033
Airworthiness
Standard · Transport
Airworthiness date
May 25, 2018

We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.

Airframe & engine

FAA Registry + type data

Airframe

Manufacturer
Textron Aviation INC
Model
680A
Year
2018
Serial number
680A0138
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
10
Engines
2
Max takeoff weight
20,000 and over lb
Mode S code
A77EC5

Engine

Make and model
P&W Canada Pw306d1
Type
Turbo-fan
Power
5,907 lb thrust

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 2026 – nowCo-ownerscurrent

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

Accident history for this model

ADs published since 1998 that may apply (1)

These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.

ADSubjectEffectiveApplies to
2018-07-13Landing GearMay 15, 2018Airframe (680A)Serial numbers per UTC Service Bulletins 2-1706-1-32-1 Rev 1 and 2-1675-32-2 Rev 1 (brake assembly serial numbers). Only with: Equipped with brake assembly P/N 2-1706-1 (Model 510) or P/N 2-1675-1 (Models 680/680A) with serial number listed in table 1 of the applicable UTC service bulletin.

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (13)

Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.

  • Hydraulic power · pump · leakingDec 18, 2025

    DURING 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 DRIPPING FROM LT ENGINE DRIVEN HYD PUMP…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Autoflight · warning light · illuminatedAug 14, 2025

    RED 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 DUE TO PILOT INDUCED FAULT. REF. AMM 22-30-05

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Doors · door · out of adjustNov 14, 2024

    FUSELAGE 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 DISSIPATES AS THE AIRSPEED DECREASES. THERE IS…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Lights · unknown · unknownJul 21, 2023

    FLOOR 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.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · switch · trippedDec 26, 2022

    WITH 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 DISGUISHED. OPS OF EMER LIGHTING SYSTEM ON…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · none · noneSep 8, 2022

    EMERG 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 NECESSARY AND RESET FWD EMER BATT G SWITCH…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Power plant · none · gougedMar 23, 2022

    L/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).

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Power plant · none · gougedMar 23, 2022

    R/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).

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · none · chafedMar 22, 2022

    RH 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.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · g switch · trippedMay 19, 2021

    FLOOR 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 EXTINGUISHED. TESTED IAW CE-680AS AMM CH…

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Showing the 10 most recent of 13 reports.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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