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| The Mystère or Falcon 20 and 200 family remains Dassault's most successful business jet program thus far, with more than 500 built. Development of the original Mystère 20 traces back to a joint collaboration between Sud Aviation (which later merged into Aerospatiale) and Dassault in the late 1950s. Prototype construction began in January 1962, leading to a first flight on May 4 1963. This first prototype shared the roduction aircraft's overall configuration, but differed in the powerplant. The prototype was initially powered by 3300lb (14.7kN) Pratt & Whitney JT12A8 turbojets, whereas production Mystère 20s (or Falcon 20s outside France) were powered with General Electric CF700s. The first GE powered 20 flew on New Year's Day 1965. Throughout the type's production life Aerospatiale remained responsible for building the tail and rear fuselage. The Falcon 20F features Full Leading Edge Slats, Higher Fuel Capacity (1360 Gals), Single Point Refueling, Thrust Reversers, and an Auxiliary Power Unit. |
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| Seating (normal) |
9 |
Max Takeoff (lbs) |
28,660 |
| Seating (maximum) |
- |
Certified Ceiling (ft) |
42,000 |
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| Engines |
2 GE CF700-2D2 |
To (Sealevel, ISA Temp) (ft) |
4,950 |
| Output lbs ea. Flat Rating |
4,500 |
Landing Distance (ft) |
1,980 |
| Maximum Mach No. |
0.87 |
Max Range (fuel) (nm) |
1,432 |
| High Speed Cruise (Kts) |
410 |
Max Range (payload) (nm) |
1,401 |
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| Flight Time 300nm |
0 + 53 |
Flight Time 1000nm |
2 + 42 |
| Flight Time 600nm |
1 + 40 |
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| External |
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Internal |
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| Length (ft) |
56.30 |
Length (ft) |
24.00 |
| Height (ft) |
17.40 |
Height (ft) |
5.70 |
| Span (ft) |
53.50 |
Width: Max floor (ft) |
6.20 |
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