N339QS2008 Cessna 680
Safety record in brief:No NTSB accidents or incidents since 19825 ADs may apply70 service difficulty reports
Registration
FAA Aircraft Registry · Oct 20, 2026- Registered owner
- Name not published by the FAA
- Certificate issued
- Dec 8, 2020
- Expires
- Dec 31, 2027
- Airworthiness
- Standard · Transport
- Airworthiness date
- Mar 19, 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 dataAirframe
- Manufacturer
- Cessna
- Model
- 680
- Year
- 2008
- Serial number
- 680-0191
- 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
- A3B8AD
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- 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, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs 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.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2018-07-13 | Landing Gear | May 15, 2018 | Airframe (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. |
| 2017-06-13 | Fuselage | May 2, 2017 | Airframe (680)Certain serial numbers: 680 680-0001; 680 680-0002; 680 680-0006; 680 680-0025; 680 680-0030; 680 680-0031; … |
| 2012-07-04 | Electrical power | May 15, 2012 | Airframe (680)Certain serial numbers: 680 -0001–-0289; 680 -0291–-0296 |
| 2007-26-16 | Cessna Model 680 Airplanes | Jan 18, 2008 | Airframe (680)Certain serial numbers: 680 -0001–-0152; 680 -0157; 680 -0158 |
| 2005-08-03 | Cessna Model 680 Airplanes | Apr 29, 2005 | Airframe (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 (70)
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.
- Fuselage · angle · corrodedSep 17, 2026
CORROSION FOUND ON LT VERTICAL CAP ANGLE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · bracket · corrodedApr 30, 2026
MECHANICALLY REMOVED 8 AREAS OF CORROSION WHERE 8 LOCK FASTENERS WERE PREVIOUSLY REMOVED ON FWD BRACKET INSIDE NLG WHEEL WELL, ON FWD FACE OF UP-LOCK BRACKET IAW SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYOND LIMITS IAW SRM 51-70-02 EXCEEDING .002" OF MATERIAL REMOVED FROM NOMINAL THICKNESS.…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · skin · corrodedApr 29, 2026
REPAIRED CORRODED AREAS AND TOOLING MARKS ON THE LH WING LOWER CENTER SKIN IN THE MLG WHEEL WELL COMMON TO THE LOWER SPAR CAP BY REMOVING FASTENERS AS REQUIRED, MECHANICALLY BLENDING, PERFORMING NDT, REPORTING FOR REPAIR DISPOSITION, FABRICATING AND INSTALLING REPAIR DOUBLERS PER ENGINEERING…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Wings · access panel · corrodedApr 29, 2026
REPAIRED RH FLAP ACCESS PANEL LAND BY BLENDING CORRODED AREAS, PERFORMING NDT, REPORTING FOR REPAIR DISPOSITION, FABRICATING AND INSTALLING REPAIR DOUBLERS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · access panel · corrodedApr 29, 2026
REPAIRED RH FLAP PANEL LAND RIBS BY BLENDING CORRODED AREAS, PERFORMING NDT, REPORTING FOR REPAIR DISPOSITION, FABRICATING AND INSTALLING REPAIR ANGLE DOUBLERS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · corrodedApr 28, 2026
FOUND MULTIPLE AREAS OF CORROSION UNDER AFT CHIN FAIRING. MECHANICALLY REMOVED AREAS OF CORROSION LOCATED UNDER AFT CHIN FAIRING ON FUSELAGE OUTER SKIN IAW CESSNA 680 SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYOND LIMITS IAW CESSNA 680 SRM 51-70-02 EXCEEDING .002" OF MATERIAL REMOVED FROM…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · doubler · corrodedApr 23, 2026
LH LOWER FUSELAGE CARRY-THROUGH DOUBLER UNDER BAGGAGE FLOOR IS CORRODED. MECHANICALLY REMOVED CORROSION LOCATED ON ELECTRICAL CARRY THROUGH DOUBLER ON THE LH SIDE UNDER THE BAGGAGE FLOOR IAW CESSNA 680 SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYOND LIMITS IAW CESSNA 680 SRM 51-70-02 EXCEEDING…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · nut plate · corrodedApr 23, 2026
FOUND 6 AREAS OF CORROSION AROUND NUT PLATES FOR PANEL 652DB, MECHANICALLY REMOVED 6 AREAS OF CORROSION WHERE 6 NUTPLATES LOCATED INSIDE RH WING ACCESS BAY 652DB WERE REMOVED IAW CESSNA 680 SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYOND LIMITS IAW CESSNA 680 SRM 51-70-02 EXCEEDING .002" OF…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · spar · corrodedApr 23, 2026
FOUND #8 SPOILER BOTH HYDRAULIC PRESSURE AND RETURN CARRY THROUGH'S HAVE CORROSION AROUND THEM ON RH WING AFT SPAR. MECHANICALLY REMOVED CORROSION WHERE #8 SPOILER HYD LINES ARE LOCATED ON RH WING, FLAP WELL, AFT SPAR, AFT FACE IAW CESSNA 680 SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYOND…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · deflector · corrodedApr 23, 2026
FOUND 7 AREAS OF CORROSION ON DEFLECTORS ON PANEL 323AC. MECHANICALLY REMOVED 7 AREAS OF CORROSION ON DEFLECTORS ON PANEL 323AC IAW CESSNA 680 SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYOND LIMITS IAW CESSNA SRM 51-70-02 EXCEEDING .002" OF MATERIAL REMOVED FROM NOMINAL THICKNESS. REPAIRED…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 70 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