N998CK1967 Dassault FALCON 20
Safety record in brief:No NTSB accidents or incidents since 19821 AD may apply9 service difficulty reports
Registration
FAA Aircraft Registry · Oct 20, 2026- Registered owner
- Kalitta Charters LLC
- Owner type
- LLC
- City, state
- Ypsilanti, MI
- Certificate issued
- Feb 11, 2003
- Expires
- Dec 31, 2029
- Airworthiness
- Standard · Transport
- Airworthiness date
- Oct 18, 1991
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
- Dassault
- Model
- FALCON 20
- Year
- 1967
- Serial number
- 98
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 10
- Engines
- 2
- Max takeoff weight
- 20,000 and over lb
- Mode S code
- ADF097
Engine
- Make and model
- Ge Cf700 Series
- Type
- Turbo-fan
- Power
- 4,200 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- 2003 – nowKalitta Charters LLCYpsilanti, MI · current
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 (1)
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 |
|---|---|---|---|
| 2000-01-09 | GE Aircraft Engines CJ610 Series Turbojet Engines and CF700 Turbofan Engines | Feb 11, 2000 | Engine (CF700 SERIES)Serial numbers per Appendix 1 of the AD. Only with: Engines with rotating parts listed by P/N and SN in Appendix 1 installed. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (9)
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 · frame · crackedMay 16, 2017
DURING EDDY CURRENT INSPECTION, A CRACK WAS FOUND IN THE BEND BETWEEN THE VERTICAL FRAME WEB AND FRAME FLANGE ON OF FRAME 33, APPROXIMATELY 20 MM BELOW STRINGER 5L, APPROXIMATELY 21 MM LONG AND OVER 1.3 MM IN DEPTH. CRACK TO BE REPAIRED.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · damagedSep 30, 2013
SMALL AREA OF SKIN WAS DAMAGED JUST FWD OF FUSELAGE FRAME 1, AND JUST ABOVE STRINGER 14R AT THE STATIC PORT NUT PLATE. THE DAMAGED SKIN IS TO BE REMOVED AND FLUSH PATCHED.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · corrodedSep 18, 2013
EDDY CURRENT INSPECTION OF SPOT WELDED ON FUSELAGE SKIN FOUND CORRODED AT FRAME 29-33, STRINGER 18L-22L.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 9 reportsShow fewer reports
- Fuselage · skin · corrodedSep 18, 2013
EDDY CURRENT INSPECTION OF SPOT WELDED FUSELAGE SKIN. FOUND CORROSION AT FRAME 17-19, STRINGERS 5L-19L.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · skin · corrodedSep 18, 2013
VISUAL INSPECTION OF WING TIPS, FOUND CORROSION ON THE TOP AFT SKIN SECTIONS, UNDER THE STATIC WICK BASES, BETWEEN RIBS 19-20.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · corrodedSep 18, 2013
EDDY CURRENT INSPECTION OF SPOT WELDED FUSELAGE SKIN FOUND CORROSION AT RT SIDE FUSELAGE FRAMES 29-33, STRINGER 18R-22R.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · corrodedSep 18, 2013
EDDY CURRENT INSPECTION OF SPOT WELDED FUSELAGE SKIN FOUND CORROSION AT RT SIDE FUSELAGE FRAME 6-7, STRINGER 21-22R.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Doors · door frame · crackedNov 6, 2009
DURING THE AIRCRAFT SCHEDULED INSPECTION, THE VISUAL INSPECTION OF THE CARGO DOOR STRUCTURE REVEALED CRACKS IN THE LOWER FORMERS AT FRAMES 11, 12 AND 13. THE CRACKED FORMERS AND ATTACH CLIPS WHERE REPLACED. FAA FORM 337 COMPLETED FOR THIS REPAIR.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Engine · engine · flamed outSep 29, 2005
RT ENGINE FLAMED OUT DUE TO TURBULANCE. ENGINE WAS RESTARTED AND CONTINUED TO ORIGINAL DESTINATION. CAPTAIN CONTACTED MAINTENANCE DEPARTMENT. ENGINE WAS INSPECTED IAW OPS MANUAL WITH NO DEFECTS NOTED. THE FLIGHT WAS CONTINUED WITH NO OTHER ABNORMAL ENGINE OPERATION. (K)
From FAA Service Difficulty Reports; matched by N-number and serial number.
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