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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]
CAP 10B · Length
Single sourceConfiguration
| Specification | Dassault Falcon 20 | Mudry CAP 10 |
|---|---|---|
| Type | Business jet[source] | Aerobatic aircraft[source] |
| Manufacturer | Dassault Aviation[source] | Avions Mudry & Cie Apex Aircraft Robin Aircraft[source] |
| Status | Out of production, in active service[source] | — |
| Primary users | Federal Express (formerly) French Navy United States Coast Guard[source] | — |
| Number built | 512 |
7.16 m (23 ft 6 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; CAP 10B · 75% power
Single sourceMaximum; CAP 10B · Maximum speed
Single sourceCAP 10B · 1 × Lycoming AEIO-360-B2F 4-cylinder air-cooled, horizontally opposed, fuel injected piston engine
Single source1 × Lycoming AEIO-360-B2F 4-cylinder air-cooled, horizontally opposed, fuel injected piston engine , 134 kW (180 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]
CAP 10B · (1,200 ft/min) max at sea level
Single source6 m/s (1,200 ft/min) max at sea level[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
300+[source] |
| Manufactured | 1965–1991[source] | 1970-2007 and 2021-[source] |
|---|
| Introduction date | 3 June 1965[source] | — |
|---|
| First flight | 4 May 1963[source] | 1968[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] | 72 L (19 US gal; 16 imp gal) + optional auxiliary tank of 75 L (20 US gal; 16 imp gal) capacity[source] |
|---|
| Aspect ratio | 6.4:1[source] | — |
|---|
| Stall speed | 152 km/h (94 mph, 82 kn)[source] | 100 km/h (62 mph, 54 kn) flaps up[source] |
|---|
| National origin | France[source] | — |
|---|
| Designer | — | Nenad Hrisafović[source] |
|---|
| Developed from | — | Piel Super Emeraude[source] |
|---|
| Airfoil | — | NACA 23012[source] |
|---|
| Propellers | — | 2-bladed Hoffmann fixed pitch wooden propeller[source] |
|---|
| Never exceed speed | — | 344 km/h (214 mph, 186 kn)[source] |
|---|
| g limits | — | +6 -4.5[source] |
|---|
| Country of origin | — | France[source]Inventory Origin column; table 1, row 34, cell 2; revision 1377359948; retrieved 2026-09-30 |
|---|