# N808CK: 1967 Dassault/Sud FAN JET FALCON

- Status: Valid registration
- Airframe: [Dassault/Sud FAN JET FALCON](https://openairdocs.org/model/dassault-sud-fan-jet-falcon) (registry code 2720302, 12 seats)
- Engine: [GE CF700 series](https://openairdocs.org/engine/ge-cf700-series) (registry code 30010)
- Data sheets: [TCDS A7EU](https://openairdocs.org/tcds/A7EU) (Dassault Aviation), [TCDS E7EA](https://openairdocs.org/tcds/E7EA) (General Electric Company) (OpenAirDocs)
- Serial number: 108
- Year built: 1967
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 23, 1971
- Certificate issued: February 11, 2003
- Expires: December 31, 2029
- Mode S code: AAFFD1
- 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=808CK
- Page: https://openairdocs.org/aircraft/N808CK

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): 50 in force

### Matched by airframe (Dassault/Sud FAN JET FALCON)

- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2026-09-10](https://openairdocs.org/ad/2026-09-10): Time Limits/Maintenance Checks · Dassault Fan Jet Falcon, Fan Jet Falcon Series C, Fan Jet Falcon Series D and 3 more. Effective Jun 18, 2026
- [AD 2026-09-07](https://openairdocs.org/ad/2026-09-07): Time Limits/Maintenance Checks · Dassault Fan Jet Falcon, Fan Jet Falcon Series C, Fan Jet Falcon Series D and 3 more. Effective Jun 17, 2026
- [AD 2010-26-05 R1](https://openairdocs.org/ad/2010-26-05-R1): Air conditioning · Dassault Falcon 10, Fan Jet Falcon, Fan Jet Falcon Series C and 14 more. Effective Dec 6, 2023
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2018-11-10](https://openairdocs.org/ad/2018-11-10): Doors · Dassault Fan Jet Falcon, Fan Jet Falcon Series C, Fan Jet Falcon Series D and 9 more. Effective Jul 9, 2018
- [AD 2018-07-07](https://openairdocs.org/ad/2018-07-07): Landing gear · Dassault Fan Jet Falcon, Fan Jet Falcon Series D, Fan Jet Falcon Series E and 6 more. Effective May 14, 2018
- [AD 2017-21-01](https://openairdocs.org/ad/2017-21-01): Fire protection · Dassault Fan Jet Falcon, Fan Jet Falcon Series C, Fan Jet Falcon Series D and 7 more. Effective Nov 27, 2017
- [AD 2017-10-01](https://openairdocs.org/ad/2017-10-01): Fuselage · Dassault Fan Jet Falcon, Fan Jet Falcon Series C, Fan Jet Falcon Series D and 7 more. Effective Jun 13, 2017
- [AD 2015-20-08](https://openairdocs.org/ad/2015-20-08): Fire protection · Dassault Fan Jet Falcon, Fan Jet Falcon Series C, Fan Jet Falcon Series D and 8 more. Effective Nov 12, 2015
- [AD 2015-08-05](https://openairdocs.org/ad/2015-08-05): Fire Protection · Dassault Fan Jet Falcon, Fan Jet Falcon Series C, Fan Jet Falcon Series D and 8 more. Effective May 8, 2015
- [AD 2013-22-10](https://openairdocs.org/ad/2013-22-10): Fire Protection · Dassault Fan Jet Falcon, Mystere-Falcon 20 - C5, Mystere-Falcon 20 - D5 and 3 more. Effective Dec 19, 2013
- [AD 2008-05-07](https://openairdocs.org/ad/2008-05-07): Divan compartment · Dassault Fan Jet Falcon, Fan Jet Falcon Series C, Fan Jet Falcon Series D and 8 more. Effective Apr 8, 2008
- [AD 2008-04-14](https://openairdocs.org/ad/2008-04-14): Overwing emergency exit · Dassault Falcon 10, Falcon 900EX, Fan Jet Falcon and 14 more. Effective Apr 1, 2008
- [AD 2004-19-02](https://openairdocs.org/ad/2004-19-02): Vertical posts of the window frames · Dassault Fan Jet Falcon, Fan Jet Falcon Series C, Fan Jet Falcon Series D and 7 more. Effective Oct 25, 2004
- [AD 2002-13-07](https://openairdocs.org/ad/2002-13-07): Inertial Reference Units (IRU) · Dassault Falcon 10, Falcon 900EX, Fan Jet Falcon and 8 more. Effective Aug 9, 2002
- [AD 2000-11-03](https://openairdocs.org/ad/2000-11-03): Pitch Feel System · Dassault Falcon 900EX, Fan Jet Falcon, Fan Jet Falcon Series C and 12 more. Effective Jun 16, 2000
- [AD 2000-05-20](https://openairdocs.org/ad/2000-05-20): Passenger Oxygen Masks · Dassault Falcon 10, Falcon 900EX, Fan Jet Falcon and 13 more. Effective Apr 18, 2000
- [AD 98-26-10](https://openairdocs.org/ad/98-26-10): AFM Limitations Section · Dassault Fan Jet Falcon, Fan Jet Falcon Series D, Fan Jet Falcon Series E and 5 more. Effective Jan 22, 1999
- [AD 98-13-15](https://openairdocs.org/ad/98-13-15): Wing-To-Fuselage Upper Fairings · Dassault Fan Jet Falcon, Mystere-Falcon 20 - C5, Mystere-Falcon 20 - D5 and 3 more. Effective Jul 23, 1998
- [AD 88-13-06](https://openairdocs.org/ad/88-13-06): Main Landing Gear Rear Lock · Dassault Fan Jet Falcon, Fan Jet Falcon Series C, Fan Jet Falcon Series D and 3 more. Effective Jul 11, 1988
- [AD 82-18-09](https://openairdocs.org/ad/82-18-09): Refueling System · Single point pressure fueling system (Rogerson ATS STC SA1851WE or 4 others). Effective Oct 4, 1982
- [AD 79-21-02](https://openairdocs.org/ad/79-21-02): Passenger Door · Dassault Fan Jet Falcon. Effective Nov 12, 1979
- [AD 77-07-02](https://openairdocs.org/ad/77-07-02): Horizontal Stabilizer · Dassault Fan Jet Falcon. Effective Apr 7, 1977
- [AD 76-22-10](https://openairdocs.org/ad/76-22-10): Main Landing Gear Downlocks · Dassault Fan Jet Falcon. Effective Nov 22, 1976
- [AD 76-19-05](https://openairdocs.org/ad/76-19-05): Engine Emergency Fuel Shut-Off Valves · Dassault Fan Jet Falcon. Effective Oct 7, 1976
- [AD 76-19-02](https://openairdocs.org/ad/76-19-02): Air Contamination · Dassault Fan Jet Falcon. Effective Sep 30, 1976
- [AD 75-08-17](https://openairdocs.org/ad/75-08-17): Digital Flight Data Recorders · BAE Systems HS 748 Series 2A, HS 748 Series 2B, 727-100 Series and 90 more. Effective Dec 19, 1975
- [AD 73-15-03](https://openairdocs.org/ad/73-15-03): Leakage of Hot Air into Rear Compartment · Dassault Fan Jet Falcon. Effective Aug 15, 1973
- [AD 70-06-07](https://openairdocs.org/ad/70-06-07): Relay for APU Oil Pump · Dassault Fan Jet Falcon. Effective Apr 18, 1970
- [AD 69-22-03](https://openairdocs.org/ad/69-22-03): Landing Gear Microswitch · Dassault Fan Jet Falcon and Fan Jet Falcon Series D. Effective Nov 26, 1969
- [AD 69-11-06](https://openairdocs.org/ad/69-11-06): Aspirator Hose · Dassault Fan Jet Falcon and Fan Jet Falcon Series D. Effective Jun 2, 1969
- [AD 69-02-03](https://openairdocs.org/ad/69-02-03): Autopilot Operating Limitation · Dassault Fan Jet Falcon with STC SA1131WE. Effective Jan 25, 1969
- [AD 68-20-02](https://openairdocs.org/ad/68-20-02): Landing Gear Switch · Dassault Fan Jet Falcon. Effective Oct 25, 1968
- [AD 68-03-05](https://openairdocs.org/ad/68-03-05): Selector Valve Control Cables · Dassault Fan Jet Falcon. Effective Feb 13, 1968
- [AD 67-27-02](https://openairdocs.org/ad/67-27-02): Fuselage Attach Bolts · Dassault Fan Jet Falcon. Effective Oct 9, 1967
- [AD 67-27-01](https://openairdocs.org/ad/67-27-01): Engine Power Lever · Dassault Fan Jet Falcon. Effective Oct 9, 1967
- [AD 67-07-02](https://openairdocs.org/ad/67-07-02): Horizontal Stabilizer Actuator · Dassault Fan Jet Falcon. Effective Mar 2, 1967
- [AD 68-10-01](https://openairdocs.org/ad/68-10-01): Janitrol Fuel Heater · Dassault Fan Jet Falcon

### 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 2023-22-10](https://openairdocs.org/ad/2023-22-10) (historical): Time Limits/Maintenance Checks · Dassault Fan Jet Falcon, Fan Jet Falcon Series C, Fan Jet Falcon Series D and 3 more. Effective Dec 26, 2023
- [AD 2023-22-05](https://openairdocs.org/ad/2023-22-05) (historical): Time Limits/Maintenance Checks · Dassault Fan Jet Falcon, Fan Jet Falcon Series C, Fan Jet Falcon Series D and 3 more. Effective Dec 26, 2023
- [AD 2020-23-10](https://openairdocs.org/ad/2020-23-10) (historical): Time Limits/Maintenance Checks · Dassault Fan Jet Falcon, Fan Jet Falcon Series C, Fan Jet Falcon Series D and 3 more. Effective Dec 23, 2020
- [AD 2019-07-01](https://openairdocs.org/ad/2019-07-01) (historical): Time Limits and Maintenance Checks · Dassault Fan Jet Falcon, Fan Jet Falcon Series C, Fan Jet Falcon Series D and 3 more. Effective May 24, 2019
- [AD 2017-01-07](https://openairdocs.org/ad/2017-01-07) (historical): Doors · Dassault Fan Jet Falcon, Fan Jet Falcon Series C, Fan Jet Falcon Series D and 9 more. Effective Feb 10, 2017
- [AD 2014-26-07](https://openairdocs.org/ad/2014-26-07) (historical): Time Limits and Maintenance Checks · Dassault Fan Jet Falcon, Fan Jet Falcon Series C, Fan Jet Falcon Series D and 3 more. Effective Feb 25, 2015
- [AD 2013-26-05](https://openairdocs.org/ad/2013-26-05) (historical): Fire Protection · Dassault Fan Jet Falcon, Fan Jet Falcon Series C, Fan Jet Falcon Series D and 8 more. Effective Oct 20, 2014
- [AD 2010-26-05](https://openairdocs.org/ad/2010-26-05) (historical): Air Conditioning · Dassault Falcon 10, Falcon 900EX, Fan Jet Falcon and 14 more. Effective Jan 25, 2011
- [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 N808CK.

## FAA accident and incident reports

None matched to N808CK.

## Reports on N808CK not matched to an aircraft (1)

They name N808CK, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19950117001449I](https://openairdocs.org/incident/19950117001449I), Jan 17, 1995: Doug DC8F55 (N808CK), Philadelphia, PA, Minor damage. Narrative: aircraft experienced a failure of the #2 main wheel assembly during taxi to takeoff from phl to yip. Flightcrew was unaware of the wheel failure.…

## Service difficulty reports (1)

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 KC8A20180221001](https://openairdocs.org/sdr/KC8A20180221001), Feb 21, 2018: FRAME. CRACKED. DURING EDDY CURRENT INSPECTION, CRACKS WHERE FOUND IN THE BENDS BETWEEN THE VERTICAL FRAME AND FRAME FLANGE ON THE LEFT AND RIGHT SIDES OF FRAME 33.

## Service difficulty reports on N808CK not matched to an aircraft (39)

They name N808CK, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR TC8A96074](https://openairdocs.org/sdr/TC8A96074), Dec 31, 1996: POWER BYPASS. OUT OF ADJUST. ON TAXI DURING CONTROL CHECK, AILERONS WENT INTO MANUAL REVERSION AND SYSTEM PRESS 800 PSI. ADJUSTED LT AND RT AILERON POWER BYPASS IAW DACO MM 27-5-2, OPS CHEC
- [SDR TC8A96070](https://openairdocs.org/sdr/TC8A96070), Dec 11, 1996: FUEL CONTROL. MALFUNCTIONED. NR 2 ENGINE COMPRESSOR STALLED AT HIGH ENGINE RPMS, HIGH FUEL FLOW NOTED. REMOVED AND REPLACED FUEL CONTROL, RAN ENGINE, TRIMMED IDLE AND PART POWER, OPS CHECKS
- [SDR TC8A96062](https://openairdocs.org/sdr/TC8A96062), Oct 4, 1996: EPR GUAGE. MALFUNCTIONED. NR 2 ENGINE NOT PRODUCING T/O POWER, ABORTED AT 88 KNOTS. SWAPPED NR 1 AND NR 2 EPR GAUGES IAW DC-8 MM CHAPTER 77-1-0, OPS CHECKED GOOD.
- [SDR TC8A96055](https://openairdocs.org/sdr/TC8A96055), Aug 24, 1996: FITTING. LOOSE. AT TAKEOFF POWER 1.87 EPR ALL ENGINE BLEEDS ON, MANIFOLD AIR PRESSURE DROPPED TO ZERO. ABORTED TAKEOFF AND RETURNED TO RAMP. FOUND LOOSE FITTING ON MANIFOLD PRE
- [SDR TC8A96053](https://openairdocs.org/sdr/TC8A96053), Aug 9, 1996: HYD LINE. FAILED. HYDRAULIC QUANTITY LOST DURING CLIMBOUT, RETURNED TO SBGR. FOUND HYDRAULIC STANDBY RUDDER PUMP PRESSURE LINE BUSTED. REMOVED AND REPLACED LINE, OPS CHECKED GOOD
- [SDR TC8A96051](https://openairdocs.org/sdr/TC8A96051), Aug 2, 1996: PRESSURIZATION. MALFUNCTIONED. LOST PRESSURIZATION DURING CRUISE, UNABLE TO OPERATE NASI FLOW CONTROL SYSTEM. CHECKED NASI SYSTEM AND GROUND RUN, SYSTEM CHECKED GOOD IAW NASI M/M CHAPTER 21-7
- [SDR TC8A96048](https://openairdocs.org/sdr/TC8A96048), Jun 27, 1996: THROTTLE DRUM. LACK OF LUBE. NR 2 POWER LEVER BINDING, ENGINE WOULD NOT DEVELOP MAX POWER. CLEANED AND LUBED THROTTLE DRUM, OPS CHECK NORMAL AT ALL POWER SETTINGS IAW 71-00.
- [SDR TC8A96044](https://openairdocs.org/sdr/TC8A96044), Jun 3, 1996: FLOW CONTL VLV. MALFUNCTIONED. AFTER TAKEOFF, UNABLE TO PRESSURIZE THE SYSTEM DUE FLOW CONTROL VALVES WEREN'T WORKING PROPERLY. CHECKED FLOW CONTROL VALVES, CONNECTIONS, RESEATED C/B'S AND TE
- [SDR TC8A96042](https://openairdocs.org/sdr/TC8A96042), Apr 14, 1996: FLEX LINE. FAILED. SBSV-SBSV - FLT NR 10501 - TAXIING OUT FROM SBSV, NO SPOILER PRESSURE. REMOVED AND REPLACED HYDRAULIC PRESSURE LINE. CHECK GROUND OPS OK IAW MM 27-33-1. (X)
- [SDR TC8A96012](https://openairdocs.org/sdr/TC8A96012), Mar 28, 1996: WIRE. BROKEN. CAPTAINS ATTITUDE INDICATOR TUMBLED ON TAKEOFF ROLL. TAKEOFF ABORTED AT 90 KNOTS. REPAIRED BROKEN WIRE AT CAPTAINS ATTITUDE INDICATOR. PERFORMED HIGH SPEED TAXI
- [SDR TC8A96040](https://openairdocs.org/sdr/TC8A96040), Mar 16, 1996: SUPPORT. CORRODED. LOWER AFT CARGO COMPARTMENT, 'D' ENTRANCE DOOR CENTER METAL PANEL SUPPORT HAS LEVEL 2 CORROSION AND SHEARED NUTS. MADE AND INSTALLED DOOR CENTER METAL PANEL SUP
- [SDR TC8A96039](https://openairdocs.org/sdr/TC8A96039), Mar 15, 1996: FLOOR BEAM. CORRODED. FUSELAGE AFT SECTION FS 1530, FLOOR BEAM HAS CORROSION AT 2 PLACES LEVEL 2, REQUIRES REPAIRING, 2 INCH BY 3 INCH AND 2 INCH BY 4 INCH. REPAIRED AFFECTED AREA AS
- [SDR TC8A96038](https://openairdocs.org/sdr/TC8A96038), Mar 12, 1996: FLOOR. CORRODED. MAIN CARGO COMPARTMENT FLOOR RT SIDE STATION 460, STATION 480 AND STATION 500, TRACK AND WEB AREA HAS CORROSION, LEVEL 2, 5 AREAS. REMOVED AND REPAIRED TRACK AS
- [SDR TC8A96037](https://openairdocs.org/sdr/TC8A96037), Mar 12, 1996: FLOOR TRACKS. BROKEN. MAIN CARGO COMPARTMENT FLOOR 5 TRACKS ARE BROKEN. REPAIRED TRACKS AS PER 52-1-0. (M)
- [SDR TC8A96016](https://openairdocs.org/sdr/TC8A96016), Mar 12, 1996: FLOOR. CORRODED. COCKPIT FLOOR FROM FS 141 THROUGH FS 245 LEFT SIDE (AROUND NR 91 ACCESS PANEL), HAS CORROSION, LEVEL 2. REMOVED CORROSION AND REPAIRED AFFECTED AREA PROPERLY AS
- [SDR TC8A96036](https://openairdocs.org/sdr/TC8A96036), Mar 11, 1996: FLOOR BEAM. CORRODED. AFT MAIN CARGO COMPARTMENT FS 1504 BEAM UPPER SIDE HAS CORROSION, LEVEL 2. REPAIRED AFFECTED AREA AS REQUIRED PER SRM 52-2-0. (M)
- [SDR TC8A96035](https://openairdocs.org/sdr/TC8A96035), Mar 11, 1996: FLOOR. CORRODED. MAIN CARGO COMPARTMENT, GALLEY AND FWD LAV AREA FLOOR HAS LEVEL 2 CORROSION, STATION 265 TO 295. MADE AND INSTALLED GALLEY AND FWD LAV AREA FLOOR AS PER SRM 52-
- [SDR TC8A96022](https://openairdocs.org/sdr/TC8A96022), Mar 11, 1996: BRACKET. CORRODED. TAIL CONE, HORIZONTAL SUPPORT AND BRACKET BASE RIGHT SIDE HAS LEVEL 2 CORROSION. MADE AND INSTALLED DOUBLER AS REQUIRED PER SRM 53-2-5. (M)
- [SDR TC8A96015](https://openairdocs.org/sdr/TC8A96015), Mar 11, 1996: DOUBLER. CORRODED. MAIN CARGO COMPARTMENT AROUND FORWARD LAVATORY FLOOR TRACK DOUBLER HAS CORROSION, LEVEL 2, BETWEEN STATION 265 AND 275 (RT SIDE). (M)
- [SDR TC8A96014](https://openairdocs.org/sdr/TC8A96014), Mar 11, 1996: RIB. CORRODED. RIGHT HORIZONTAL STABILIZER L/E INTERNAL PART RIB HAS CORROSION, LEVEL 2. REMOVED CORROSION, TREATED AREA, AND REPAIRED INTERNAL PART RIB AS NECESSARY PER SRM 5
- [SDR TC8A96013](https://openairdocs.org/sdr/TC8A96013), Mar 11, 1996: RIBS. CRACKED. LEFT HORIZONTAL STAB L/E HAS 3 RIBS CORRODED, LEVEL 2. REPAIRED AFFECTED AREA PROPERLY AS PER SRM 55-3-0. (M)
- [SDR TC8A96024](https://openairdocs.org/sdr/TC8A96024), Mar 10, 1996: SPAR CAP. CRACKED. RIGHT WING REAR SPAR CAP AT XW 69.50 HAS 2 CRACKS BETWEEN STIFFENERS, 2.5-7 INCHES. REPAIRED AFFECTED AREA AS PER SRM 57-5-0. (M)
- [SDR 96ZZZM695](https://openairdocs.org/sdr/96ZZZM695), Mar 10, 1996: SPAR CAP. CRACKED. RIGHT WING REAR SPAR CAP AT XW 69.50 HAS 2 CRACKS BETWEEN STIFFENERS, 2.5 THROUGH 7 INCHES. REPAIRED AFFECTED AREA AS PER SRM 57-5-0. REFERENCE TC8A96024.
- [SDR TC8A96034](https://openairdocs.org/sdr/TC8A96034), Mar 9, 1996: DOUBLER. BROKEN. CARGO COMPARTMENT FLOOR STATION 880 MLG UPPER SKIN DOUBLER BETWEEN STACK AND WEB IS BROKEN. REPAIRED AFFECTED AREA AS PER SRM 52-1-0. (M)
- [SDR TC8A96032](https://openairdocs.org/sdr/TC8A96032), Mar 8, 1996: DOUBLER. CORRODED. LOWER AFT CARGO COMPARTMENT STATION 1120 RIGHT SIDE 532R, CARGO DOOR DOUBLER IS BROKEN, ALSO CORRODED, LEVEL 2. REPAIRED AFFECTED AREA AND CCONTROLLED CORROSION
- [SDR TC8A96031](https://openairdocs.org/sdr/TC8A96031), Mar 8, 1996: DOUBLER. CRACKED. LOWER FORWARD CARGO COMPARTMENT STATION 520 TOP SURFACE RIGHT SIDE LINING SPLICE DOUBLER CRACKED, 2 INCHES. REPAIRED DOUBLER AT AFFECTED AREA AS REQUIRED PER SR
- [SDR TC8A96030](https://openairdocs.org/sdr/TC8A96030), Mar 8, 1996: DOUBLER. BROKEN. LOWER FORWARD CARGO COMPARTMENT LINING STATION 560 TOP SURFACE RIGHT SIDE AFT DOOR HOUSING HAS DOUBLER BROKEN. MADE AND INSTALLED DOUBLER AT AFFECTED AREA AS RE
- [SDR TC8A96029](https://openairdocs.org/sdr/TC8A96029), Mar 8, 1996: WALL. CRACKED. LOWER FORWARD CARGO COMPARTMENT WALL, STATION 560, BOTTOM AREA RIGHT SIDE EDGE CRACKED, 2 INCHES. AFFECTED AREA REPAIRED AS REQUIRED PER SRM 51-1-19, 52-4-0. (M
- [SDR TC8A96023](https://openairdocs.org/sdr/TC8A96023), Mar 8, 1996: DOOR SKIN. CRACKED. RIGHT MAIN LANDING GEAR DOOR UPPER SURFACE SKIN CRACKED, 1 INCH. REPAIRED AFFECTED AREA AS PER SRM 57-2-1. (M)
- [SDR TC8A96028](https://openairdocs.org/sdr/TC8A96028), Mar 7, 1996: DOUBLER. CORRODED. AFT FUSELAGE FS 1080, RIGHT STRINGER NR 34 DOUBLER HAS CORROSION, LEVEL 2. MADE AND INSTALLED NEW DOUBLER AS PER SRM 51-10-O. (M)
- [SDR TC8A96027](https://openairdocs.org/sdr/TC8A96027), Mar 7, 1996: STRINGER. CORRODED. AFT FUSELAGE FS 1220 AND 1240, RIGHT STRINGER NR 34 HAS CORROSION, LEVEL 2. NR 34 STRINGER REPAIRED AS PER SRM 53-4-0. (M)
- [SDR TC8A96026](https://openairdocs.org/sdr/TC8A96026), Mar 7, 1996: STRINGER. CORRODED. AFT FUSELAGE STATION 1080 AND STATION 1040, RIGHT STRINGER NR 32 HAS CORROSION LEVEL 2. TREATED AND REPAIRED STRINGER 32 RT, MADE AND INSTALLED UPPER PLATE AS P
- [SDR TC8A96025](https://openairdocs.org/sdr/TC8A96025), Mar 7, 1996: DOUBLER. CORRODED. AFT FUSELAGE STATION 1080 AND STATION 1040, RIGHT STRINGER NR 34 DOUBLER HAS LEVEL 2 CORROSION. REPAIRED DOUBLER AS PER SRM 53-4-0. (M)
- [SDR TC8A96021](https://openairdocs.org/sdr/TC8A96021), Mar 7, 1996: DOUBLER. BROKEN. RIGHT WING ERS 300.344, TE STEEL DOUBLER LOWER SURFACE IS BROKEN. MADE AND INSTALLED DOUBLER AT AFFECTED AREA AS REQUIRED PER SRM 57-2-3. (M)
- [SDR TC8A96020](https://openairdocs.org/sdr/TC8A96020), Mar 7, 1996: DOUBLER. BROKEN. RW T/E FLAP LOWER SURFACE ACTUATOR ROD DOUBLER BROKEN, 1 INCH. MADE AND INSTALLED DOUBLER AT AFFECTED AREA AS EPR SRM 57-2-1. (M)
- [SDR TC8A96019](https://openairdocs.org/sdr/TC8A96019), Mar 7, 1996: DOUBLER. CRACKED. LW T/E LOWER SURFACE XW 60.250, DOUBLER HAS A CRACK 4.5 INCH. REPLACED DOUBLER AS PER SRM 57-2-1. (M)
- [SDR TC8A96018](https://openairdocs.org/sdr/TC8A96018), Mar 7, 1996: RIVETS. LOOSE. LEFT WING, STATION XRS 230.500 T/E LOWER PART SHOWS STRUCTURAL REPAIR WITH 4 LOOSE RIVETS AND BUCKED HEAD OVERSIZED. REPAIRED AFFECTED AREA AS REQUIRED PER SRM 
- [SDR TC8A96017](https://openairdocs.org/sdr/TC8A96017), Mar 7, 1996: DOUBLER. BROKEN. LW T/E LOWER SURFACE XW 408.343 HAS DOUBLER BROKEN AND CRACKED (5 INCHES). MADE AND INSTALLED NEW DOUBLER AS PER SRM 57-2-3. (M)
- [SDR 95ZZZZ54](https://openairdocs.org/sdr/95ZZZZ54), Jan 17, 1995: MAIN WHEEL. BROKEN. NR 2 MAIN TIRE MISSING AFTER LANDING YIP. FOUND OUTBOARD FLANGE BROKEN OFF. REPLACED NR 2 AND NR 1 MAIN WHEEL ASSY.

## STCs that may be installed (OpenAirDocs) (211, first 50)

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 airframe (Dassault/Sud FAN JET FALCON)

- [STC SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc
- [STC ST01833WI](https://openairdocs.org/stc/ST01833WI): Modification of a Rockwell Collins Global Positioning System (GPS) installation. Rockwell Collins Inc
- [STC ST03424CH](https://openairdocs.org/stc/ST03424CH): Certification of Automatic Dependent Surveillance - Broadcast (ADS-B) Out System with Rockwell Collins TDR-94/-94D Transponders. CMD Flight Solutions LLC
- [STC ST04575AT](https://openairdocs.org/stc/ST04575AT): Installation of the Rockwell Collins ALT-1000+/ -4000+ with 5G Filtering. Chippewa Aerospace Inc
- [STC ST02004WI](https://openairdocs.org/stc/ST02004WI): Installation of the Garmin GI-275 Instantaneous Vertical Speed Indicators (IVSI). Peregrine
- [STC ST04528AT](https://openairdocs.org/stc/ST04528AT): Installation of the 5 Parameter Flight Data Recorder (FDR) System. Chippewa Aerospace Inc
- [STC ST04448CH](https://openairdocs.org/stc/ST04448CH): Avionics upgrade installation of a Garmin GTN (TM) 750 Touchscreen Navigator interfaced to existing pilot side instruments and existing Collins AP-105 autopilot and added GWX (TM) 70 Weather Radar. The Garmin GTN (TM) 750 GPS is paired with the added GTX (TM) 345R Transponders for Automatic Broadcast Surveillance (ADS-B) OUT and ADS-B IN capability with wireless download connectivity utilizing Garmin Connext®. Optional second Garmin GTN (TM) 650/750 interfaced to existing copilot side instruments only. Royal Air Inc
- [STC ST01930LA](https://openairdocs.org/stc/ST01930LA): Installation of Sandel Avionics SN4500 Electronic Horizontal Situation Indicator (EHSI). Sandel Avionics LLC
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC SA2315CE-D](https://openairdocs.org/stc/SA2315CE-D): Installation of Bendix/King 5 tube EFS-10 electronic flight instrument system. Honeywell International Inc
- [STC ST04447CH](https://openairdocs.org/stc/ST04447CH): Installation of Garmin GTS (TM) 8000 TCAS/ACAS II Traffic Surveillance system, dual GTX (TM) 3000 Mode-S Extended Squitter Transponders and GDL® 88 receiver for a complete ADS-B In/Out capability and a Flight Stream 210 for wireless download connectivity using Garmin Connext®. Installation in accordance with Royal Air Master Document List No. RACB-MDL-3000, Revision A, dated January 06, 2020, or later FAA approved revision. Royal Air Inc
- [STC SA2404SW](https://openairdocs.org/stc/SA2404SW): System to disable the take off out of trim warning system when high power is applied during operation of thrust reversers after landing. Air Comm Corporation
- [STC SA2474SW](https://openairdocs.org/stc/SA2474SW): Install horn silence switch. Air Comm Corporation
- [STC ST00835DE](https://openairdocs.org/stc/ST00835DE): Installation of Automatic Dependent Surveillance - Broadcast (ADS-B) Out and In functionality using the Garmin GTX 335R and GTX 345R Transponders plus qualified position sensor. Peregrine
- [STC ST00347BO](https://openairdocs.org/stc/ST00347BO): Modification to upgrade a BendixKing CAS 67A TCAS II system to CAS 67B TCAS II Change 7.1. Pro Star Aviation, LLC
- [STC SA785SW](https://openairdocs.org/stc/SA785SW): Installation of Collins AL-101 radio altimeter system. Associated Air Center, Inc. - c/o CT Corporation System
- [STC SA786SW](https://openairdocs.org/stc/SA786SW): Installation of AP/ADN-153(V) Doppler System. Associated Air Center, Inc. - c/o CT Corporation System
- [STC SA833SW](https://openairdocs.org/stc/SA833SW): Installation of VOR antenna. Associated Air Center, Inc. - c/o CT Corporation System
- [STC SA839SW](https://openairdocs.org/stc/SA839SW): Installation of VOR antenna. Associated Air Center, Inc. - c/o CT Corporation System
- [STC SA856SW](https://openairdocs.org/stc/SA856SW): Bendix ALA-51A radio altimeter. Associated Air Center, Inc. - c/o CT Corporation System
- [STC SA871SW](https://openairdocs.org/stc/SA871SW): 28 volt 4 amp hour nickel cadmium battery. Associated Air Center, Inc. - c/o CT Corporation System
- [STC ST04273AT](https://openairdocs.org/stc/ST04273AT): Replace Original Main Battery Connector with Concorde Connector, Part Number 4000. Concorde Battery Corporation
- [STC SA1588SW](https://openairdocs.org/stc/SA1588SW): Installation of Foxtronics/TRAMM BT1 600 nickel cadmium battery temperature system. FoxCart GSE, LLC
- [STC SA5212NM](https://openairdocs.org/stc/SA5212NM): Installation of cabin air conditioning system. Air Comm Corporation
- [STC SA2492SW](https://openairdocs.org/stc/SA2492SW): Installation of dual Sperry SPI-80/81 flight director system and SPZ-500 autopilot system (two axis). Contact Aviation LLC
- [STC ST01457WI](https://openairdocs.org/stc/ST01457WI): Installation of Dual Thommen AD 30 Altimeter Repeaters and a Skylight Air Data Converter (ADC-600). 3S Certification LLC
- [STC ST01433WI-D](https://openairdocs.org/stc/ST01433WI-D): Modification of a Collins GPS-4000 or GPS-4000A. Rockwell Collins Inc
- [STC ST376AT](https://openairdocs.org/stc/ST376AT): Installation of Pyrotcctor, Inc. smoke detector. Royal Air Inc
- [STC SA472CE](https://openairdocs.org/stc/SA472CE): Install Twilight MKIII Supplementary lighting system with model A wing tip and Model L tail lights. BF Goodrich Aerospace
- [STC ST01576CH-D](https://openairdocs.org/stc/ST01576CH-D): Installation of a Collins Pro Line 21 Continuum Retrofit Integrated Avionics System. Standard Aero
- [STC ST01384LA](https://openairdocs.org/stc/ST01384LA): Installation of MASS Systems P/N M811456 engine fire extinguisher. This fire extinguisher is in accordance with MASS Systems Master Drawing List (MDL) No. M811456, Revision C, dated August 22, 2002, or later FAA approved revision. AMETEK AMERON LLC d/b/a MASS Systems
- [STC ST00673WI-D](https://openairdocs.org/stc/ST00673WI-D): Modification of Collins VHF-22A/VHF-22B VHF COMM Receiver Transmitter with CTL-22 Control Pro Line II System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II System installation. Rockwell Collins Inc
- [STC ST00682WI-D](https://openairdocs.org/stc/ST00682WI-D): Modification of Collins VHF-20/VHF-20A/VHF-20B VHF COMM Receiver Transmitter with CTL-20 Control Pro Line I System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II System Installation in accordance with Collins Installation Instructions as listed on AML No. ST00682WI-D, Revision -, or later FAA approved revisions. Rockwell Collins Inc
- [STC SA2490SO](https://openairdocs.org/stc/SA2490SO): Enlargement of forward passenger door, and installation of flight crew emergency exit. Royal Air Inc
- [STC SA1213SW](https://openairdocs.org/stc/SA1213SW): Alteration for battery charging from ground power unit. JSF Aviation Services Inc
- [STC SA1464SW](https://openairdocs.org/stc/SA1464SW): Installation of collins AVR-101 Voice. JSF Aviation Services Inc
- [STC SA740SW](https://openairdocs.org/stc/SA740SW): Collins AP103F/FD108 Flight Director Systems and Sensors, equipment for Category II. JSF Aviation Services Inc
- [STC SA805SW](https://openairdocs.org/stc/SA805SW): Collins AP-103F/FD-109G flight director system and associated sensors for 2-axis. JSF Aviation Services Inc
- [STC SA891SW](https://openairdocs.org/stc/SA891SW): Dorne & Margolin DMN4-15-5 antenna. JSF Aviation Services Inc
- [STC SA993SW](https://openairdocs.org/stc/SA993SW): Collins AP-104 Autopilot and FD-109H/FD-109F Flight Directors. JSF Aviation Services Inc
- [STC ST1001SO](https://openairdocs.org/stc/ST1001SO): Installation of Federal Express Corp. brake mount flange. JSF Aviation Services Inc
- [STC ST02136CH](https://openairdocs.org/stc/ST02136CH): Installation of a Honeywell Mark VII Enhanced Ground Proximity Warning System (EGPWS). Flying Investment LLC
- [STC ST02500CH](https://openairdocs.org/stc/ST02500CH): Certification for Reduced Vertical Separation Minimum (RVSM) operational capability and installation of IS&S Air Data Display System and Rosemount model 0856LR Pitot-Static Probes. Royal Air Inc
- [STC ST01349WI](https://openairdocs.org/stc/ST01349WI): Reduced Vertical Separation Minimum (RVSM) group airworthiness approval of specific Dassault Aviation Fan Jet Falcon and Mystere-Falcon 20 aircraft. Flying Investment LLC
- [STC SA1102EA](https://openairdocs.org/stc/SA1102EA): Installation of Teledyne Avionics angle of attack indicating system, P/N SL112B2300. Aerosonic Corporation
- [STC SA1137SW](https://openairdocs.org/stc/SA1137SW): Installation of Teledyne Avionics normalized angle of attack indicating system. Aerosonic Corporation
- [STC SA829EA](https://openairdocs.org/stc/SA829EA): Installation of Teledyne Avionics Auto Throttle System No. SL104A100-1. Aerosonic Corporation
- [STC SA894EA](https://openairdocs.org/stc/SA894EA): Installation of Grimes three light strobe kit P/N 34-0302-1 as supplemental lighting. Honeywell International Inc

All 211: https://openairdocs.org/aircraft/N808CK/stcs.md

## Related

- Other Dassault/Sud FAN JET FALCON aircraft: https://openairdocs.org/model/dassault-sud-fan-jet-falcon/aircraft.md
- The GE CF700 series engine: https://openairdocs.org/engine/ge-cf700-series.md

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