FORCETALLY
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At a glance
Measured figures
Falcon 900B · Length
Single source20.21 m (66 ft 4 in)[source]
CAP 10B · Length
Single sourceConfiguration
| Specification | Dassault Falcon 900 | Mudry CAP 10 |
|---|---|---|
| Type | Business jet[source] | Aerobatic aircraft[source] |
| National origin | France[source] | — |
| Manufacturer | Dassault Aviation[source] | Avions Mudry & Cie Apex Aircraft Robin Aircraft[source] |
| Status | Active service, in production[source] | — |
| Primary users | French Air and Space Force Japan Coast Guard Nigerian Air Force Royal Malaysian Air Force |
7.16 m (23 ft 6 in)[source]
CAP 10B · Height
Single source2.55 m (8 ft 4 in)[source]
CAP 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 900B · 3 × Honeywell TFE731 -5BR-1C turbofans thrust each
Single source3 × Honeywell TFE731 -5BR-1C turbofans , 21.13 kN (4,750 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.
| — |
| Number built | >500[source] | 300+[source] |
|---|
| Manufactured | 1984–present[source] | 1970-2007 and 2021-[source] |
|---|
| First flight | 21 September 1984 ( 1984-09-21 )[source] | 1968[source] |
|---|
| Developed from | Dassault Falcon 50[source] | Piel Super Emeraude[source] |
|---|
| Developed into | Dassault Falcon 2000 Dassault Falcon 7X[source] | — |
|---|
| Capacity | 19 passengers[source] | — |
|---|
| Fuel capacity | 8,690 kg (19,160 lb)[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 | 7.63:1[source] | — |
|---|
| Stall speed | 158 km/h (98 mph, 85 kn) (wheels and flaps down)[source] | 100 km/h (62 mph, 54 kn) flaps up[source] |
|---|
| Designer | — | Nenad Hrisafović[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 |
|---|