N361QS2008 Cessna 680
Safety record in brief:No NTSB accidents or incidents since 19825 ADs may apply48 service difficulty reports
Registration
FAA Aircraft Registry · Oct 20, 2026- Registered owner
- Name not published by the FAA
- Certificate issued
- Jan 4, 2021
- Expires
- Jan 31, 2028
- Airworthiness
- Standard · Transport
- Airworthiness date
- Oct 27, 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
- 680-0235
- 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
- A41172
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- 2021 – 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 (48)
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.
- Doors · spring · brokenSep 28, 2026
WHEN CLOSING THE MAIN ENTRY DOOR, THERE WAS A LOUD POP AND THE FORWARD CLOSING ASSIST CABLE BECAME SLACK. INSPECTED MED FOUND BROKEN FWD COUNTERBALANCE SPRING AND BROKEN MED OVER CENTER PUSHROD. REMOVED AND REPLACED MED FWD FAILED COUNTERBALANCE SPRING, AND PERFORMED A SATISFACTORY ADJUSTMENT AND…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · support · corrodedMay 18, 2026
FOUND CORROSION UNDER MULTIPLE NUTPLATES FOR PANEL 342AB.MECHANICALLY REMOVED CORROSION LOCATED WHERE 13 NUTPLATES WERE PREVIOUSLY REMOVED ON INNER AND OUTER SKIN SURFACES INCLUDING AREAS OF CORROSION LOCATED ALONG ANGLE STRAP EDGES 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 · landing · corrodedMay 18, 2026
BUBBLING PRIMER AND WHITE POWDER AROUND AND UNDER 26 NUTPLATES UNDER PANEL 154AC. MECHANICALLY REMOVED CORROSION LOCATED WHERE 26 NUTPLATES WERE PREVIOUSLY 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 MATERIAL…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Fuselage · landing · corrodedMay 18, 2026
FOUND SIGNS OF CORROSION UNDER 9 NUTPLATES UNDER PANEL 154BC. MECHANICALLY REMOVED 9 AREAS OF CORROSION LOCATED WHERE 8 NUTPLATES WERE PREVIOUSLY REMOVED INSIDE FUSELAGE BAY 154BC 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. - Fuselage · stringer · corrodedMay 12, 2026
CENTER STRINGER UNDER PANEL 164AC HAS 5 AREAS OF CORROSION. REMOVED BUBBLED PRIMER FROM 5 AREAS LOCATED IN FUSELAGE BAY 164AC ON CENTER STRINGER AND VERIFIED CORROSION. MECHANICALLY REMOVED CORROSION AND PITTING PER CESSNA 680 SRM 21-70-02. FOUND CORROSION BLENDS TO BE BEYOND LIMITS IAW CESSNA 680…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · landing · corrodedMay 12, 2026
CORROSION ON PANEL LANDS FOR PANEL 164AC. REPAIRED CORROSION ON PANEL LANDS FOR PANEL 164AC IN REFERENCE TO NETJETS REQUEST FOR TECHNICAL SERVICES (RFTS): RFTS-117178 REV. 0; TITLED: N361QS (680-0235) PANEL 164AC NUTPLATE CORROSION; DATED: 11 MAY 2026.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · stringer · corrodedMay 12, 2026
CENTER STRINGER UNDER PANEL 164BC HAS 3 AREAS OF CORROSION. REMOVED BUBBLED PRIMER FROM 3 AREAS AND VERIFIED CORROSION LOCATED INSIDE FUSELAGE BAY 164BC ON CENTER STRINGER. MECHANICALLY REMOVED CORROSION AND PITTING PER CESSNA 680 SRM 21-70-02. FOUND CORROSION BLENDS TO BE BEYOND LIMITS IAW CESSNA…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Lights · battery · dischargedMay 19, 2025
RIGHT REAR CABIN, EXTERIOR FORWARD WING AND WING INSPECTION EMERGENCY LIGHTS WOULD NOT ILLUMINATE AFTER 30 MINUTE CHARGE APPLIED AND POWER REMOVED. PERFORMED OPERATIONAL CHECK OF INTERIOR AND EXTERIOR EMERGENCY LIGHTS IAW CE-680 AMM 33-50-10. SOPS CHECK GOOD. NO OTHER DEFECTS NOTED AT THIS TIME.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Lights · battery pack · inoperativeMay 18, 2025
CABIN EMERG LIGHT: RIGHT REAR CABIN LIGHT DID NOT ILLUMINATE AFTER CHARGING FOR 30 MINUTES CORRECTIVE ACTION; C/W TC-FLT-33-1001 CESSNA 680 EMERGENCY LIGHTING POWER SUPPLY BATTERY EXERCISE PROCEDURE. OPS CHECK GOOD IAW CE-680 MM 33-50-00.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · spar · corrodedJan 29, 2025
FOUND AREA OF CORROSION AROUND SPOILER EXTEND HYDRAULIC LINE FITTING ON RH WING AFT SPAR. MECHANICALLY REMOVED CORROSION WHERE SPOILER AND SPEED BRAKE HYD LINES WERE DISCONNECTED AT CARRY THRU FITTING ON AFT FACE OF AFT SPAR LOCATED ON RH WING IN INBD FLAP COVE 2 OUTBD POSITIONS IAW C680 SRM…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 48 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