FORCETALLY
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At a glance
Measured figures
Falcon 900B · Length
Single source20.21 m (66 ft 4 in)[source]
P2002-LSA · Length
Single sourceConfiguration
| Specification | Dassault Falcon 900 | Tecnam P2002 Sierra |
|---|---|---|
| Type | Business jet[source] | Two-seat light single[source] |
| National origin | France[source] | Italy[source] |
| Manufacturer | Dassault Aviation[source] | Tecnam[source] |
| Status | Active service, in production[source] | — |
P2002 Sierra MkII / Tecnam Means Flying with Style · Length
Single source6.61 m (21 ft 8 in)[source]
21.7 ft (6,63 m)[source]P2002 Sierra MkII / Tecnam Means Flying with Style
Empty; Falcon 900B · Empty weight
Single sourceMaximum take-off; Falcon 900B · Max takeoff weight
Single source10,255 kg (22,608 lb)[source]
20,640 kg (45,503 lb)[source]
Empty; P2002-LSA · Empty weight
Single sourceMaximum take-off; P2002-LSA · Max takeoff weight
Single sourceFalcon 900B · with 8 passengers
Single source7,400 km (4,600 mi, 4,000 nmi) with 8 passengers[source]
P2002-LSA · 1 × Rotax 912 S2
Single source1 × Rotax 912 S2 , 73.5 kW (100 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]
Falcon 900B · Service ceiling
Single source15,500 m (50,900 ft)[source]
P2002-LSA · 1,220 ft/min
Single source6.2 m/s (1,220 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Primary users |
|---|
French Air and Space Force Japan Coast Guard Nigerian Air Force Royal Malaysian Air Force[source] |
| — |
| Number built | >500[source] | — |
|---|
| Manufactured | 1984–present[source] | — |
|---|
| First flight | 21 September 1984 ( 1984-09-21 )[source] | — |
|---|
| Developed from | Dassault Falcon 50[source] | — |
|---|
| Developed into | Dassault Falcon 2000 Dassault Falcon 7X[source] | — |
|---|
| Capacity | 19 passengers[source] | 1 passenger[source] |
|---|
| Fuel capacity | 8,690 kg (19,160 lb)[source] | — |
|---|
| Aspect ratio | 7.63:1[source] | 6.4:1[source] |
|---|
| Stall speed | 158 km/h (98 mph, 85 kn) (wheels and flaps down)[source] | 71 km/h (44 mph, 38 kn) (flaps down)[source] |
|---|
| Propellers | — | 2-bladed, fixed pitch propeller[source] |
|---|
| Never exceed speed | — | 250 km/h (160 mph, 130 kn)[source] |
|---|
| g limits | — | +6g, -3g[source] |
|---|
| Takeoff run | — | 232 m (761 ft)[source] |
|---|
| Landing run | — | 186 m (610 ft)[source] |
|---|