- Registered owner
- Kalitta Charters LLC
- Location
- Ypsilanti, MI
- Owner type
- LLC
- Serial number
- 98
- Year built
- 1967
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- October 18, 1991
- Certificate issued
- February 11, 2003
- Expires
- December 31, 2029
- Mode S code
- ADF097
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every GE CF700 model are included below.
On this page
Airworthiness directives that may apply · 11
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1975 | 1 |
|---|---|
| 1976 | 1 |
| 1981 | 1 |
| 1985 | 1 |
| 1997 | 1 |
| 1998 | 2 |
| 2000 | 1 |
| 2001 | 1 |
| 2010 | 1 |
Engine · GE CF700 series
AD 2010-09-08AFT Technologies combustion linersAD 2001-10-12Unapproved PartsAD 98-23-06Combustion Liner AssembliesAD 97-25-08Airworthiness Directives; General Electric Company CJ610 Series Turbojet and CF700 Series Turbofan EnginesAD 97-13-10Aft fan diskAD 85-18-03Stage 1 Turbine DiskAD 80-08-06 R1Turbine DisksAD 75-05-13Compound Turbine And Fan BladeAD 75-19-05Horizontal Drive ShaftAD 78-07-06Compressor DisksAD 73-23-05First Stage Turbine DiscsSuperseded and historical ADs · 1
Information bulletins that may apply · 2
Advisory, not mandatory.
Historical bulletins · 1
NTSB investigations
No NTSB investigations matched to N998CKMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Dassault-Breguet FALCON 20 aircraft
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 9
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR KC8A20170516002Frame · crackedDURING 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.SDR KC8A20130918007Skin · damagedSMALL 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.SDR KC8A20130918005Skin · corrodedEDDY CURRENT INSPECTION OF SPOT WELDED FUSELAGE SKIN FOUND CORROSION AT RT SIDE FUSELAGE FRAME 6-7, STRINGER 21-22R.SDR KC8A20130918004Skin · corrodedEDDY CURRENT INSPECTION OF SPOT WELDED FUSELAGE SKIN FOUND CORROSION AT RT SIDE FUSELAGE FRAMES 29-33, STRINGER 18R-22R.SDR KC8A20130918003Skin · corrodedVISUAL INSPECTION OF WING TIPS, FOUND CORROSION ON THE TOP AFT SKIN SECTIONS, UNDER THE STATIC WICK BASES, BETWEEN RIBS 19-20.SDR KC8A20130918002Skin · corrodedEDDY CURRENT INSPECTION OF SPOT WELDED FUSELAGE SKIN. FOUND CORROSION AT FRAME 17-19, STRINGERS 5L-19L.SDR KC8A20130918001Skin · corrodedEDDY CURRENT INSPECTION OF SPOT WELDED ON FUSELAGE SKIN FOUND CORRODED AT FRAME 29-33, STRINGER 18L-22L.SDR KC8AN998CKDoor Frame · crackedDURING 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.SDR KCB2005F00000Engine · flamed outRT 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
STCs that may be installed · 5
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Engine · GE CF700 series
STC SE976SOInstallation of an oil tank sight gauge on a G.E. oil tank, P/N6003T09P04.STC SE8674SWModification of the following engine oil tanks by adding a sight glass: 6002T03P01, 6002T03P03, 6003T09P01, 6003T09P02, 6003T09P03, 6003T09P04, 6003T89P01, 6003T89P02, 6003T03P02, 6002T03P04.STC SE966SOManufacture and installation of Axis C gearshaft plugs per Fed Ex Drawing F-72-003, Sheets 1 and 2.STC SE1057SOInstallation of capacitance type probe with oil quantity indicating system in oil tank.STC SE949SOInstallation of an oil level sight gauge.