N338QS2004 Cessna 680
This N-number isn't registered right now. Below is its last known registration, canceled Jun 21, 2023.
Safety record in brief:No NTSB accidents or incidents since 19825 ADs may apply42 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 20, 2026- Last registered owner
- Netjets Sales INC
- Owner type
- Corporation
- City, state
- Oklahoma City, OK
- Certificate issued
- Dec 22, 2020
- Canceled
- Jun 21, 2023
- Airworthiness
- Standard · Transport
- Airworthiness date
- Dec 14, 2004
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
- 2004
- Serial number
- 680-0011
- 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
- A3B4F6
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 – 2023Netjets Sales INCOklahoma City, OK
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 (42)
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.
- Wings · spar · damagedMar 19, 2021
REPAIRED THE LH WING REAR SPAR LOWER FORWARD ANGLE, LOCATED IN THE LH MAIN LANDING GEAR WHEEL WELL, BY BLENDING CORRODED AREA PERFORMING NDT AND INSTALLING A REPAIR DOUBLER PER ENGINEERING REPAIR ORDER.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Doors · structure · corrodedMar 19, 2021
REMOVED THE EXISTING EMERGENCY EXIT DOOR AND FOUND CORROSION ON THE DOOR AROUND THE CONTOUR RINGS. REMOVED THE CONTOUR RINGS FROM THE DOOR AND FOUND ADDITIONAL CORROSION. REPLACED CORRODED EMERGENCY EXIT DOOR WITH A NEW DOOR TEXTRON P/N 6911251-200.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Doors · bolt · failedJan 17, 2021
WHEN THE MAIN CABIN DOOR HANDLE IS OPENED FROM THE INSIDE, THE HANDLE HITS A METAL CYLINDER THAT PROTRUDES FROM THE GROUND. IF THE HANDLE IS FORCED ALL THE WAY TO THE GROUND THE HANDLE WILL SLIDE AFT AND BECOME TRAPPED UNDERNEATH THE LIP OF THE METAL CYLINDER. REMOVED AND REPLACED BOLTS PN:…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Wings · skin · corrodedSep 16, 2020
REMOVED CORRODED RT UPPER INBOARD BONDED SKIN ASSY, P/N UNKNOWN, AND INSTALLED A NEW BONDED SKIN ASSY P/N 6922680-28 ONTO RT UPPER INBOARD WING. WORK PERFORMED IN REFERENCE TO CESSNA 680 SRM 51-40-03, 51-40-06 AND 51-40-08.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · skin · corrodedSep 14, 2020
REMOVE AND REPLACE CORRODED RT WING TRAILING EDGE SKIN P/N 6922681-70. REMOVED AND REPLACED CORRODED RT WING TRAILING EDGE SKIN BOND ASSEMBLY WITH NEW P/N 6922681-70 S/N LOT NR 29598079.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · skin · corrodedSep 14, 2020
BLENDED MULTIPLE AREAS OF CORROSION ON LT UPPER WING SKIN AT WS 37 FROM FS 408.46 THRU 482.46. PERFORMED AN EDDY CURRENT INSPECTION AND AN ULTRASONIC THICKNESS INSPECTION ON BLENDED AREAS. REMOVED BLENDED FASTENERS AND REPLACED FASTENERS AS NECESSARY WITH HL19PB5 AND HL19PB6 HI LOKS, HL70 COLLARS…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · spar · corrodedSep 2, 2020
LT MLG WHEEL WELL LOWER AFT SPAR HAS 2 AREAS OF VERIFIED CORROSION. REMOVED 3 EACH HI-LOKS FROM LT MLG WHEEL WELL LOWER AFT SPAR FOR ACCESS. BLENDED 2 EACH AREAS OF CORROSION ON LT MLG WHEEL WELL LOWER AFT SPAR. OTBD AREA WAS FOUND TO BE MILD SURFACE CORROSION PER CESSNA 680 SRM 51-10-01 AND…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Stabilizers · hinge fitting · corrodedAug 27, 2020
RUDDER UPPER HINGE POINT, LOWER BRACKET HAS VERIFIED CORROSION AROUND ATTACH BOLT. HAND SANDED AREA OF CORROSION LOCATED ON UPPER RUDDER HINGE, LOWER PLATE, LT SIDE. FOUND CORROSION DAMAGE TO BE LEVEL 2, PER NJA GMM 2.2.2. REMOVED AND REPLACED CORRODED LOWER PLATE FROM RUDDER UPPER HINGE ASSEMBLY…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · drag angle · corrodedAug 27, 2020
RT WING AFT DRAG ANGLE HAS 7 AREAS OF VERIFIED CORROSION ALONG OUTBOARD EDGE AND 6 AREAS OF VERIFIED CORROSION ON MIDDLE DRAG ANGLE OUTBOARD EDGE. REPAIRED DELAMINATED AREA ON RT WING UPPER MIDDLE DRAG ANGLE, PER S-750-ATA51-01RD REV A, DATED 17 FEB 09, SUPPORTED BY TEXTRON AVIATION MEMO DQ26672M1…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Stabilizers · spar cap · corrodedSep 17, 2018
VERTICAL STAB AFT SPAR CORROSION. ACCOMPLISHED ENGINEERING LETTER DQ15722M1 DATED SEPTEMBER 13, 2018; 680-0011. VERTICAL STABILIZER AFT SPAR CAP/RIM (P/N 6961526-5) DAMAGE (CORROSION).
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 42 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