N313QS2007 Cessna 680
Safety record in brief:No NTSB accidents or incidents since 19825 ADs may apply51 service difficulty reports
Registration
FAA Aircraft Registry · Oct 20, 2026- Registered owner
- Name not published by the FAA
- Certificate issued
- Jul 24, 2020
- Expires
- Jul 31, 2027
- Airworthiness
- Standard · Transport
- Airworthiness date
- May 16, 2007
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
- 2007
- Serial number
- 680-0140
- 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
- A35365
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 (51)
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.
- Stabilizers · skin · corrodedMay 16, 2026
BLENDED MULTIPLE AREAS OF CORROSION ON THE UPPER AND LOWER SKINS OF THE HORIZONTAL STABILIZER, NEAR LT AND RT TIP CAP, LH AND RH IB ELEVATOR HINGE, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, PRIMED, AND TOPCOATED AREAS.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Stabilizers · skin · corrodedMay 15, 2026
MECHANICALLY REMOVED 1 AREA OF CORROSION AND 1 AREA OF BARE METAL LOCATED ON LH HORIZONTAL STAB UPPER SKIN NEAR INBOARD ELEVATOR HINGE, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. FABRICATED AND INSTALLED REPAIR DOUBLERS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Stabilizers · skin · corrodedMay 15, 2026
MECHANICALLY REMOVED 1 AREA OF CORROSION AND 1 AREA OF BARE METAL LOCATED ON LH HORIZONTAL STAB UPPER SKIN NEAR INBOARD ELEVATOR HINGE, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. FABRICATED AND INSTALLED REPAIR DOUBLERS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Stabilizers · spar cap · corrodedMay 15, 2026
MECHANICALLY REMOVED 2 AREAS OF CORROSION LOCATED INSIDE LH HORIZONTAL STAB ELEVATOR COVE, LOWER SPAR CLIP BETWEEN INBOARD AND MIDDLE ELEVATOR HINGE ATTACHMENTS, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · spar · corrodedMay 15, 2026
MECHANICALLY REMOVED CORROSION LOCATED ON RH WING AFT SPAR, AFT FACE OF SPAR WEB BELOW SPOILER PANEL #9 AROUND PRESSURE AND RETURN HYDRAULIC LINE CARRY THROUGH FITTINGS, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · corrodedMay 15, 2026
MECHANICALLY REMOVED 1 AREA OF CORROSION ON THE UPPER AFT CORNER OF THE CUT OUT OF THE E-EXIT ON FUSELAGE SKIN, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · wing root · corrodedNov 21, 2025
CORROSION FOUND WHERE LT AND RT WING AND FUSELAGE MEET.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · wing root · corrodedNov 19, 2025
CORROSION FOUND WHERE LT AND RT WING AND FUSELAGE MEET.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Lights · battery pack · inoperativeJun 3, 2025
LIGHTS CONNECTED TO THEIR RESPECTIVE EMERGENCY LIGHTING BATTERY PACK FAILED TO OPERATE AFTER TWO 30 MINUTE CHARGING SESSIONS. THE TWO LOWER SIDES OF MAIN CABIN DOOR FRAME, ONE ABOVE EMERGENCY EXIT, ONE ON BULKHEAD BEHIND SEAT 9. CORRECTIVE ACTION: REMOVED AND REPLACED ALL EMERGENCY BATTERY PACKS…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Stabilizers · skin · corrodedOct 7, 2024
REPAIRED CORRODED AREAS OF THE VERTICAL STABILIZER SKINS LOCATED NEAR THE UPPER EDGE AND ONE NEAR THE FORWARD EDGE BY BLENDING, PERFORMING NDT, REPORTING FOR REPAIR DEPOSITION, CLEANING, TREATING, PRIMING AND FABRICATING AND INSTALLING REPAIR DOUBLERS IAW AEROSPACE QUALITY RESEARCH & DEVELOPMENT…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 51 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