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Aeroprints.com · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
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At a glance
Measured figures
Falcon 20F · Length
Single source17.15 m (56 ft 3 in)[source]
T-35A · Length
Single sourceConfiguration
| Specification | Dassault Falcon 20 | ENAER T-35 Pillán |
|---|---|---|
| Type | Business jet[source] | Trainer[source] |
| Manufacturer | Dassault Aviation[source] | ENAER[source] |
| Status | Out of production, in active service[source] | In service[source] |
| Primary users | Federal Express (formerly) French Navy United States Coast Guard[source] | Chilean Air Force Spanish Air and Space Force National Air and Naval Service of Panama Paraguayan Air Force |
8 m (26 ft 3 in)[source]
Cruise; Falcon 20F · at 12,200 m (40,000 ft) (econ. cruise)
Single sourceMaximum; Falcon 20F · at 7,620 m (25,000 ft) (max cruise)
Single source862 km/h (536 mph, 465 kn) at 7,620 m (25,000 ft) (max cruise)[source]
750 km/h (470 mph, 400 kn) at 12,200 m (40,000 ft) (econ. cruise)[source]
Cruise; T-35A · 75% power at 2,680 m (8,793 ft)
Single sourceMaximum; T-35A · at sea level
Single sourceT-35A · 1 × Avco Lycoming AEIO-540-K1K5 6-cylinder air-cooled horizontally-opposed piston engine
Single source1 × Avco Lycoming AEIO-540-K1K5 6-cylinder air-cooled horizontally-opposed piston engine, 224 kW (300 hp)[source]
Falcon 20F · 2 × General Electric CF700 -2D-2 turbofans thrust each
Single source2 × General Electric CF700 -2D-2 turbofans , 20 kN (4,500 lbf) thrust each[source]
T-35A · 75% power at sea level
Single source75% power at sea level 4 hours 24 minutes[source]
T-35A · 1,526 ft/min
Single source7.75 m/s (1,526 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Number built | 512[source] | 154[source] |
|---|
| Manufactured | 1965–1991[source] | 28 December 1984 – 1991[source] |
|---|
| Introduction date | 3 June 1965[source] | — |
|---|
| First flight | 4 May 1963[source] | 6 March 1981[source] |
|---|
| Developed into | Dassault Falcon 10 Dassault Falcon 50[source] | — |
|---|
| Capacity | 8–14 passengers[source] | — |
|---|
| Fuel capacity | 5,200 L (1,100 imp gal; 1,400 US gal)[source] | 291.5 L (77.0 US gal; 64.1 imp gal) in two wing leading edge integral tanks / 210 kg (463 lb) (272.5 L (72.0 US gal; 59.9 imp gal) usable)[source] |
|---|
| Aspect ratio | 6.4:1[source] | — |
|---|
| Stall speed | 152 km/h (94 mph, 82 kn)[source] | 125 km/h (78 mph, 67 kn) flaps up[source] |
|---|
| National origin | France[source] | Chile[source] |
|---|
| Developed from | — | Piper PA-32R[source] |
|---|
| Airfoil | — | root: NACA 65 2 -415 ; tip: NACA 65 2 -415 modified[source] |
|---|
| Propellers | — | 3-bladed Hartzell HC-C3YR-4BF/FC7663R, 1.93 m (6 ft 4 in) diameter constant-speed propeller[source] |
|---|
| Maximum flap extension speed | — | 218 km/h (135 mph; 118 kn)[source] |
|---|
| Maximum undercarriage extension speed | — | 256 km/h (159 mph; 138 kn)[source] |
|---|
| Approach speed over 15 m (49 ft) obstacle | — | 148 km/h (92 mph; 80 kn)[source] |
|---|
| Landing speed | — | 120 km/h (75 mph; 65 kn)[source] |
|---|
| Never exceed speed | — | 446 km/h (277 mph, 241 kn)[source] |
|---|
| Absolute ceiling | — | 6,250 m (20,505 ft)[source] |
|---|
| g limits | — | + 6 - 3[source] |
|---|
| Time to altitude | — | 1,830 m (6,004 ft) in 4 minutes 42 seconds[source] |
|---|
| Wing loading | — | 97.73 kg/m 2 (20.02 lb/sq ft)[source] |
|---|
| Power/mass | — | 0.167 kW/kg (0.102 hp/lb)[source] |
|---|
| Take-off run | — | 287 m (942 ft)[source] |
|---|
| Take-off distance to 15 m (49 ft) | — | 494 m (1,621 ft)[source] |
|---|
| Landing run | — | 238 m (781 ft)[source] |
|---|
| Landing distance from 15 m (49 ft) | — | 509 m (1,670 ft)[source] |
|---|