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Aircraft record

N324QS2008 Cessna 680

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:No NTSB accidents or incidents since 19825 ADs may apply25 service difficulty reports

Registration
Valid
expires Dec 31, 2027
Owners
1
since 2020
NTSB events
None
since 1982
ADs may apply
5
confirm with A&P
Service reports
25
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
Name not published by the FAA
Certificate issued
Dec 18, 2020
Expires
Dec 31, 2027
Airworthiness
Standard · Transport
Airworthiness date
Dec 18, 2008

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
Cessna
Model
680
Year
2008
Serial number
680-0242
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
9
Engines
2
Max takeoff weight
20,000 and over lb
Mode S code
A37E9B

Engine

Make and model
P&W Canada Pw306c
Type
Turbo-fan
Power
6,040 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. 2020 – nowName not published by the FAAcurrent

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 (5)

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 (680)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.
2017-06-13FuselageMay 2, 2017Airframe (680)Certain serial numbers: 680 680-0001; 680 680-0002; 680 680-0006; 680 680-0025; 680 680-0030; 680 680-0031; …
2012-07-04Electrical powerMay 15, 2012Airframe (680)Certain serial numbers: 680 -0001–-0289; 680 -0291–-0296
2007-26-16Cessna Model 680 AirplanesJan 18, 2008Airframe (680)Certain serial numbers: 680 -0001–-0152; 680 -0157; 680 -0158
2005-08-03Cessna Model 680 AirplanesApr 29, 2005Airframe (680)Certain serial numbers: 680 -0001–-0021

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

Service Difficulty Reports (25)

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 · battery pack · inoperativeJun 24, 2026

    AFT LAV EMERGENCY EXIT LIGHT AND OVERHEAD LIGHT AS WELL AS THE AFT BULKHEAD EMERGENCY EXIT LIGHTS DO NO ILLUMINATE AS REQUIRED. GAINED ACCESS TO NR 3 AND 4 EMERGENCY LIGHT POWER SUPPLY. REMOVED BOTH POWER SUPPLYS AND INSTALLED 2 TRUE BLUE POWER EMERGENCY LIGHT POWER SUPPLYS. REINSTALLED ACCESS…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · light · malfunctionedJun 13, 2026

    EMER LIGHTS BY THE EMERGENCY EXIT AND EXTERIOR ARE INOP. EMER LIGHTS BY THE MAIN CABIN DOOR ARE STILL WORKING PROPERLY. ARRIVED AT AIRCRAFT, PERFORMED OPS CHECK OF EXTERIOR AND INTERIOR EMER LIGHTS. OPS CHECK GOOD. STARTED APU AND CHARGE THE EMERGENCY BATTERY, PERFORMED OPS CHECK OF THE EMERGENCY…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · check valve · faultedNov 22, 2025

    AFTER DEPARTURE AND AFTER LIFTING THE GEAR RETRACTION HANDLE, THE RIGHT MAIN GEAR LIGHT REMAINED ILLUMINATED. THE TOWER ALSO CONFIRMED THAT THE RIGHT MAIN GEAR WAS STILL EXTENDED IN THE DOWN POSITION. WE RAN THE QRH AND EXTENDED THE LANDING GEAR AND ALL THREE GREEN LIGHTS ILLUMINATED AND WE LANDED…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Hydraulic power · pump · leakingSep 28, 2025

    WHEN LEVEL IN FLIGHT, SELECTED CROSSFEED LEFT, AFTER APPROX 2 MIN SELECTED OFF AND RECEIVED AMBER FUEL BOOST PUMP ON RT, CONDUCTED QRH CHECKLIST AND COULD NOT CLEAR. CHECKLIST SAID TO LAND AS SOON AS PRACTICAL. THIS OCCURRED ON THE PREVIOUS FLIGHT/LEG. THE CAS MSG CLEARED ON THE GROUND. REMOVED…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · brake assy · vibrationSep 24, 2025

    THE MLG BRAKE ASSY GENERATING FRICTION & DRAGGING WHEN BRAKES RELEASED & ACFT IN MOTION. ACFT GROUND BEHAVIOR IS SLIGHTLY PULL TO RT WITHOUT BRAKING APPLIED. CANNOT DETERMINE WHICH BRAKE SYS ON RT MLG MALFUNCTIONING. CARBON SMOKE EMANATING FROM RT MLG. VIBRATION PRESENT THROUGHOUT AIRFRAME WHEN…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Flight controls · flap system · faultedMar 29, 2025

    FLAPS FAIL AMBER CAS: UPON FLAP SELECTION DURING APPROACH CAUSING A FLAPS FAIL CAS MESSAGE (ALSO TRIGGERED GRD PROX FAIL AND WINDSHEAR FAIL CAS MESSAGE). SYSTEM DID NOT RESET BY FOLLOWING QRC AND FLAPS FAIL STAYED ILLUMINATED. UPON POST FLIGHT NOTED FLAPS WERE EXTENDED FOR APPROXIMATELY 1 INCH.…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · spar · corrodedJan 31, 2025

    MECHANICALLY REMOVED 3 AREAS OF CORROSION WITH 1 ADDITIONAL AREA LOCATED ON THE LH AFT WING SPAR, AFT FACE AROUND THE CARRY THROUGH FITTINGS INSIDE FLAP WELL BAY 523AB. MECHANICALLY REMOVED 1 AREA OF CORROSION LOCATED AROUND SPOILER HYDRAULIC PRESSURE LINE CARRY THRU FITTING ON RH WING IN INBD…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · rib · corrodedJan 8, 2025

    LH MLG WING RIB LWS 52 INBD SIDE HAS 14 HI-LOK COLLARS WITH CORROSION AROUND THEM. MECHANICALLY REMOVED CORROSION LOCATED IN LH GEARWELL ON INBD/UPPER SIDE OF LWS 52.00 CROSSOVER RIB WHERE 14 HI-LOK'S PLUS 1 ADDITIONAL HI-LOK WERE REMOVED IAW C680 SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYOND…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · door frame · corrodedDec 16, 2024

    BLENDED TWO AREAS OF CORROSION FOUND ALONG THE EMERGENCY EXIT DOOR CONTOUR RINGS. REMOVED THE CONTOUR RINGS AND BLENDED ADDITIONAL CORROSION FOUND. PERFORMED NDT AND REPORTED RESULTS OR REPAIR DISPOSITION. EMERGENCY EXIT DOOR P/N 6911251-6 WAS SENT OUT FOR REPAIR.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Doors · unknown · unknownSep 11, 2023

    ON ENTRY TO THE AIRCRAFT NOTICED THAT IN THE FULL DOWN POSITION WITH THE ENTRY HANDLE IN THE OVER CENTER LOCKED POSITION. THE DOOR IS NOT LOCKED DOWN IT STILL TRYS TO GO BACK UP ABOUT 2-3 INCHES. THE DOOR IS LOOSE AND NOT SECURED. WHEN WEIGHT IS PUT BACK ON IT THE DOOR GOES BACK DOWN. //SIGNOFF//…

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

Showing the 10 most recent of 25 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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