# N998CK: 1967 Dassault-Breguet FALCON 20 - Status: Valid registration - Airframe: [Dassault-Breguet FALCON 20](https://openairdocs.org/model/dassault-breguet-falcon-20) (registry code 2730103, 10 seats) - Engine: [GE CF700 series](https://openairdocs.org/engine/ge-cf700-series) (registry code 30010) - Data sheets: [TCDS E7EA](https://openairdocs.org/tcds/E7EA) (General Electric Company) (OpenAirDocs) - Serial number: 98 - Year built: 1967 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: October 18, 1991 - Certificate issued: February 11, 2003 - Expires: December 31, 2029 - Mode S code: ADF097 - Registered owner: [Kalitta Charters LLC](https://openairdocs.org/faa-owner/KALITTA%20CHARTERS%20LLC) - Location: [Ypsilanti, MI](https://openairdocs.org/faa-place/MI/Ypsilanti) - Owner type: LLC - Owner's area on the map: 42.2751° N, 83.5863° W: Placed by OpenAirDocs at the center of ZIP code 48198, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=998CK - Page: https://openairdocs.org/aircraft/N998CK From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every GE CF700 model are included. ## ADs that may apply (OpenAirDocs): 11 in force ### Matched by airframe (Dassault-Breguet FALCON 20) None in force. ### Matched by engine (GE CF700 series) - [AD 2010-09-08](https://openairdocs.org/ad/2010-09-08): AFT Technologies combustion liners · General Electric CF700-2C, CF700-2D, CF700-2D-2 and 7 more. Effective May 28, 2010 - [AD 2001-10-12](https://openairdocs.org/ad/2001-10-12): Unapproved Parts · General Electric CF700-2C, CF700-2D, CF700-2D-2 and 7 more. Effective Jun 7, 2001 - [AD 98-23-06](https://openairdocs.org/ad/98-23-06): Combustion Liner Assemblies · General Electric CF700-2C, CF700-2D, CF700-2D-2 and 7 more. Effective Nov 20, 1998 - [AD 97-25-08](https://openairdocs.org/ad/97-25-08): General Electric CF700-2C, CF700-2D, CF700-2D-2 and 7 more. Effective Jan 2, 1998 - [AD 97-13-10](https://openairdocs.org/ad/97-13-10): Aft fan disk · General Electric CF700-2C, CF700-2D and CF700-2D-2. Effective Aug 26, 1997 - [AD 85-18-03](https://openairdocs.org/ad/85-18-03): Stage 1 Turbine Disk · General Electric CF700-2D, CF700-2D-2, CJ610-8A and 1 more. Effective Nov 15, 1985 - [AD 80-08-06 R1](https://openairdocs.org/ad/80-08-06-R1): Turbine Disks · General Electric CF700-2D, CF700-2D-2, CJ610-8A and 1 more. Effective Feb 2, 1981 - [AD 75-05-13](https://openairdocs.org/ad/75-05-13): Compound Turbine And Fan Blade · General Electric CF700-2C, CF700-2D and CF700-2D-2. Effective Mar 3, 1976 - [AD 75-19-05](https://openairdocs.org/ad/75-19-05): Horizontal Drive Shaft · General Electric CF700-2C, CF700-2D, CF700-2D-2 and 1 more. Effective Sep 26, 1975 - [AD 78-07-06](https://openairdocs.org/ad/78-07-06): Compressor Disks · General Electric CF700-2C, CF700-2D, CF700-2D-2 and 2 more - [AD 73-23-05](https://openairdocs.org/ad/73-23-05): First Stage Turbine Discs · General Electric CF700-2C, CJ610-1, CJ610-4 and 2 more ### Historical (superseded or no longer in force) - [AD 2000-01-09](https://openairdocs.org/ad/2000-01-09) (historical): General Electric Aircraft Engines CF700-2C, CF700-2D and CF700-2D-2. Effective Feb 11, 2000 ## Information bulletins (advisory) (2 in force) - [SAIB NE-08-49R1](https://openairdocs.org/saib/NE-08-49R1): Turbine Engine Combustion Section. Issued Sep 17, 2008 - [SAIB NE-00-31](https://openairdocs.org/saib/NE-00-31): . Issued Aug 29, 2000 - [SAIB NE-08-49](https://openairdocs.org/saib/NE-08-49) (historical): Turbine Engine Combustion Section. Issued Sep 9, 2008 ## NTSB investigations None matched to N998CK. ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20091119051749I](https://openairdocs.org/incident/20091119051749I), Nov 19, 2009: Dassault-Br FALCON 20 (N998CK), Colorado Spring, CO, No damage. Pilot departed cos for sli. Aircraft failed to pressurize during ascent. Aircraft returned to cos. ## Service difficulty reports (9) As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR KC8A20170516002](https://openairdocs.org/sdr/KC8A20170516002), May 16, 2017: FRAME. CRACKED. 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 - [SDR KC8A20130918007](https://openairdocs.org/sdr/KC8A20130918007), Sep 30, 2013: SKIN. DAMAGED. 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 FLU - [SDR KC8A20130918005](https://openairdocs.org/sdr/KC8A20130918005), Sep 18, 2013: SKIN. CORRODED. EDDY CURRENT INSPECTION OF SPOT WELDED FUSELAGE SKIN FOUND CORROSION AT RT SIDE FUSELAGE FRAME 6-7, STRINGER 21-22R. - [SDR KC8A20130918004](https://openairdocs.org/sdr/KC8A20130918004), Sep 18, 2013: SKIN. CORRODED. EDDY CURRENT INSPECTION OF SPOT WELDED FUSELAGE SKIN FOUND CORROSION AT RT SIDE FUSELAGE FRAMES 29-33, STRINGER 18R-22R. - [SDR KC8A20130918003](https://openairdocs.org/sdr/KC8A20130918003), Sep 18, 2013: SKIN. CORRODED. VISUAL INSPECTION OF WING TIPS, FOUND CORROSION ON THE TOP AFT SKIN SECTIONS, UNDER THE STATIC WICK BASES, BETWEEN RIBS 19-20. - [SDR KC8A20130918002](https://openairdocs.org/sdr/KC8A20130918002), Sep 18, 2013: SKIN. CORRODED. EDDY CURRENT INSPECTION OF SPOT WELDED FUSELAGE SKIN. FOUND CORROSION AT FRAME 17-19, STRINGERS 5L-19L. - [SDR KC8A20130918001](https://openairdocs.org/sdr/KC8A20130918001), Sep 18, 2013: SKIN. CORRODED. EDDY CURRENT INSPECTION OF SPOT WELDED ON FUSELAGE SKIN FOUND CORRODED AT FRAME 29-33, STRINGER 18L-22L. - [SDR KC8AN998CK](https://openairdocs.org/sdr/KC8AN998CK), Nov 6, 2009: DOOR FRAME. CRACKED. 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 CR - [SDR KCB2005F00000](https://openairdocs.org/sdr/KCB2005F00000), Sep 29, 2005: ENGINE. FLAMED OUT. RT ENGINE FLAMED OUT DUE TO TURBULANCE. ENGINE WAS RESTARTED AND CONTINUED TO ORIGINAL DESTINATION. CAPTAIN CONTACTED MAINTENANCE DEPARTMENT. ENGINE WAS INSPECT ## STCs that may be installed (OpenAirDocs) (5) Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do. ### Approved for the engine (GE CF700 series) - [STC SE976SO](https://openairdocs.org/stc/SE976SO): Installation of an oil tank sight gauge on a G.E. oil tank, P/N6003T09P04. JSF Aviation Services Inc - [STC SE8674SW](https://openairdocs.org/stc/SE8674SW): Modification of the following engine oil tanks by adding a sight glass: 6002T03P01, 6002T03P03, 6003T09P01, 6003T09P02, 6003T09P03, 6003T09P04, 6003T89P01, 6003T89P02, 6003T03P02, 6002T03P04. Bizjet International Sales & Support Inc. Lists CF700-2C - [STC SE966SO](https://openairdocs.org/stc/SE966SO): Manufacture and installation of Axis C gearshaft plugs per Fed Ex Drawing F-72-003, Sheets 1 and 2. JSF Aviation Services Inc. Lists CF700-2C - [STC SE1057SO](https://openairdocs.org/stc/SE1057SO): Installation of capacitance type probe with oil quantity indicating system in oil tank. Aircraft Equipment Certification Corporation - [STC SE949SO](https://openairdocs.org/stc/SE949SO): Installation of an oil level sight gauge. Aircraft Equipment Certification Corporation. Lists CF700-2C ## Related - Other Dassault-Breguet FALCON 20 aircraft: https://openairdocs.org/model/dassault-breguet-falcon-20/aircraft.md - The GE CF700 series engine: https://openairdocs.org/engine/ge-cf700-series.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.