N323QS2007 Cessna 680
Safety record in brief:No NTSB accidents or incidents since 19825 ADs may apply69 service difficulty reports
Registration
FAA Aircraft Registry · Oct 20, 2026- Registered owner
- Name not published by the FAA
- Certificate issued
- Nov 21, 2020
- Expires
- Nov 30, 2027
- Airworthiness
- Standard · Transport
- Airworthiness date
- Apr 20, 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
- 680-0134
- 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
- A37AE4
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 (69)
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.
- Engine · engine · making metalJun 20, 2026
ENROUTE AT FL410, RT ENG OIL PRESSURE BEGAN SLOWLY DECAYING UNTIL OIL PRESSURE LOW RT CAS ILLUM, FOLLOWED BY A ENG VIBRATION RT CAS. SUBSEQUENTLY SHUT DOWN RT ENG IAW QRH & DIVERTED TO KAPA. CHIP DETECTOR. METAL, SLUDGE & COKE PRESENT. LP & HP ROTATE FREELY W/ NO NOISE. REMOVED 1 QT OF OIL FROM…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · brake · faultedMay 21, 2026
AFTER TOUCHDOWN WHEN APPLYING BRAKES GRADUALLY BETWEEN 70 AND 80KTS THE LEFT MAIN BRAKE STARTS GRABBING AND SHIMMERING NOTICEABLY. WHEN BELOW ANTI SKID SPEED NO GRABBING NOR SHIMMERING IS OCCURRING. INSPECTED LT INBD AND OTBD BRAKE, WHEEL ASSEMBLIES AND SURROUNDING AREA WITH NO DEFECTS NOTED.…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Stabilizers · skin · damagedSep 26, 2025
MECHANICALLY BLENDED 8 AREAS ON RT H-STAB LOWER SKIN ON THE AFT EDGE, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED , TREATED, PRIMED AND TOP COATED AREAS PER NETJETS REQUEST FOR TECHNICAL DISPOSITION REPORT.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Lights · battery pack · unserviceableJun 24, 2025
MULTIPLE EMERGENCY LIGHTS IN THE CABIN AND EXTERIOR NOT ILLUMINATING WHEN EMERGENCY LIGHT SWITCH IN THE ARMED POSITION. RAN APU FOR 45 MINUTES TO CHARGE BATTERY PACKS, WITH NO SUCCESS. REMOVED # 1 EMERGENCY BATTERY, REMOVED #1 EMERGENCY BATTERY, INSTALLED REPAIRED CUSTOMER SUPPLIED EMERGENCY…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Lights · battery · inoperativeMar 30, 2025
FORWARD CABIN EMERGENCY LIGHTS DO NOT ILLUMINATE WITH THE SWITCH IN THE ON POSITION. AFT CABIN EMERGENCY LIGHTS DO ILLUMINATE. CORRECTIVE ACTION: TROUBLESHOT EMERGENCY LIGHTING SYSTEM AND VERIFIED THAT THE CABIN DOOR EXIT LIGHT AND FWD RH WORK SURFACE LIGHT WERE NOT ILLUMINATING. REMOVED #1…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Doors · nut plate · corrodedMar 25, 2025
FOUND 8 NUTPLATES WITH CORROSION LOCATED INSIDE OF PANEL 154BC. NUT PLATES HOLD ON THE MED SPADE DOOR. REMOVED EXISTING MED SPADE DOOR AND 8 NUTPLATES FOR ACCESS. MECHANICALLY BLENDED AREAS OF CORROSION IAW C680 SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYOND C680 SRM 51-70-02 LIMITATIONS…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Doors · skin · corrodedMar 24, 2025
FOUND THE EMERGENCY EXIT DOOR CORRODED OUTER SKIN ALONG CONTOUR RING EDGE AREA, REMOVED CONTOUR RINGS AND FOUND ADDITIONAL AREAS OF CORROSION. SENT DOOR OUT FOR REPAIRS. NOTE: EMERGENCY EXIT DOOR P/N 6911251-4.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · lug · corrodedMar 21, 2025
REMOVED RH MIDDLE FLAP ASSEMBLY TO WORK CORROSION ON FWD, OUTBD LUG. MECHANICALLY REMOVED RH MIDDLE FLAP ROLLER, OUTBD LUG CORROSION, INBD SURFACE IAW C680 SRM 51-70-02. FOUND CORROSION BLEND TO BE BEYOND C680 SRM 51-70-02 LIMITATIONS EXCEEDING .002" OF MATERIAL REMOVED FROM NOMINAL THICKNESS.…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · spar · corrodedMar 21, 2025
MECHANICALLY REMOVED 2 AREAS OF CORROSION FROM RH WING AFT SPAR, FWD FACE IN RH MLG WHEEL WELL. EVALUATED AND FOUND BLENDED AREAS WERE BEYOND LIMITS PER CESSNA 680 SRM 51-70-02 EXCEEDING .002" OF MATERIAL REMOVED FROM NOMINAL THICKNESS. REPAIRED CORROSION BLENDS IAW NETJETS ENGINEERING…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · tail cone · corrodedMar 21, 2025
MECHANICALLY REMOVED 4 AREAS OF CORROSION LOCATED ON TAILCONE SERVICE DOOR FRAME ASSEMBLY WITH ADDITIONAL 4 AREAS OF CORROSION AFTER FRAME ASSEMBLY WAS REMOVED IAW C680 SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYOND C680 SRM 51-70-02 LIMITATIONS EXCEEDING .002" OF MATERIAL REMOVED FOR NOMINAL…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 69 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