The Falcon 100 is a HEAVY_JET jet aircraft with a maximum range of 1,620 nm, 6 seats. SkyAccess tracks 1 active Falcon 100 aircraft across 1 FAA Part 135 charter operators, with 0 upcoming empty legs published on this type.
The Dassault Falcon 100, an upgraded light business jet, succeeded the Falcon 10 in the mid-1980s. Introduced in 1983 and certificated in December 1986, the Falcon 100 boasts several significant improvements over its predecessor. Equipped with two Honeywell TFE 731-2-1C engines, each generating 3,230 lbs. of thrust, the Falcon 100 features several redesigned elements. These include an optional Electronic Flight Instrument System (EFIS) glass cockpit, a larger non-pressurized rear baggage compartment, and an increased maximum takeoff weight. Although the Falcon 100’s maximum payload of 1,547 lbs. is less than the Falcon 10’s 2,360 lbs., it excels in performance. It has a certified flight ceiling of 45,000 feet, a high-speed cruise of 476 knots (true airspeed), and a long-range cruise of 431 knots. Its maximum takeoff weight is 18,740 lbs. The cabin of the Dassault Falcon 100 seats six passengers in an executive-club configuration or up to nine in a high-density arrangement. The cabin dimensions—12.9 ft. in length, 4.8 ft. in height, and 5 ft. in width—make it spacious for a light jet. It also includes a lavatory at the front. The Dassault Falcon 100 was the first certified aircraft to incorporate EFIS technology with color screens in its cockpit. Its avionics system typically includes dual Collins VHF20A communication and VIR30A navigation systems, Sperry Primus 400 color weather radar, and APS 80 autopilot. By the end of production in 1989, Dassault had delivered 37 Falcon 100 aircraft.
| Tail | Year | Operator | Base |
|---|---|---|---|
| N707CX | — | Club Jet Charter, LLC | FCM |