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Aircraft record

N968QS2025 Textron Aviation INC 680A

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:No NTSB accidents or incidents since 19821 AD may apply5 service difficulty reports

Registration
Valid
expires May 31, 2033
Owners
1
since 2026
NTSB events
None
since 1982
ADs may apply
1
confirm with A&P
Service reports
5
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
Co-owners
Certificate issued
May 28, 2026
Expires
May 31, 2033
Airworthiness
Standard · Transport
Airworthiness date
Mar 8, 2025

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
2025
Serial number
680A0422
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
AD7B4D

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 (5)

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.

  • Lights · elec connector · misinstalledSep 20, 2026

    EMERGENCY SIGN ON AFT DIVIDER IS INOP. SWAPPED INCORRECT CONNECTORS. OPS CHECK GOOD IAW 35-50-00.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Doors · pin · out of alignmentMay 20, 2026

    WHILE CLOSING THE MAIN ENTRY DOOR, WHEN TRYING TO CLOSE THE DOOR, THE HANDLE IS VERY DIFFICULT TO GET DOWN INTO THE STOWED POSITION. WE ALLOWED THE DOOR TO GO TO THE FULL OPEN POSITION CHECKING THE DOOR PINS AND LOOKING FOR MISALIGNMENT. WE THEN LIFTED THE DOOR TO THE FULLY CLOSED POSITION, AND…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Air conditioning and pressurization · unknown · odorNov 22, 2025

    I ENTERED THE AFT EQUIPMENT BAY FOR PREFLIGHT AND IMMEDIATLY DETECTED A STRONG ODOR OF BURNT ELECTRONICS. THE ONLY THING POWERING THE PLANE AT THE TIME WERE THE SHIPS BATTERIES. MY FO DETECED THE SAME ODOR. WE RAN THE APU FOR 15 MINUTES TO TRY AND VENT THE ODOR BUT WHEN I RE ENTERED THE BAY THE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 5 reports
  • Doors · door · bindingSep 14, 2025

    INTERMITTENT MAIN CABIN DOOR HANDLE BINDING, WON`T MOVE TO THE CLOSED POSITION. IF YOU PLAY WITH THE HANDLE, IT WILL CLOSE BUT THEN BIND AGAIN AFTER A COUPLE MORE CYCLES OF THE HANDLE. GAINED ACCESS TO DOOR INTERIOR AND VERIFIED RIGGING WAS WITHIN LIMITATIONS. LUBRICATEDCLOSED POSITION. IF YOU…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Flight controls · controller · faultedApr 25, 2025

    WHEN HORIZONTAL STAB TRIM IS ACTIVATED IN EITHER DIRECTION THE TRIM MOVES APPROX .2 DEGREES THEN STOPS AND THE AMBER "PRI STAB TRIM FAIL" CAS MESSAGE ILLUMINATES. POWERED UP AIRCRAFT. VERIFIED STAB TRIM TO FAIL FROM BOTH PILOT AND COPILOT YOKE CONTROL SWITCHES, STAB WOULD MOVE.2 DEGREES NOSE UP…

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

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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