FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
Falcon 900B · Length
Single source20.21 m (66 ft 4 in)[source]
Length
Single sourceConfiguration
| Specification | Dassault Falcon 900 | Tecnam P2012 Traveller |
|---|---|---|
| Type | Business jet[source] | — |
| National origin | France[source] | Italy[source]P2012 Traveller |
| Manufacturer | Dassault Aviation[source] | Tecnam[source]P2012 Traveller |
| Status | Active service, in production[source] | — |
| Primary users | French Air and Space Force Japan Coast Guard Nigerian Air Force Royal Malaysian Air Force |
11.8 m (38 ft 9 in)[source]
2 × Lycoming TEO-540C1A 6-cylinder air-cooled horizontally-opposed turbocharged piston engines each
Single source2 × Lycoming TEO-540C1A 6-cylinder air-cooled horizontally-opposed turbocharged piston engines, 280 kW (375 hp) each[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]
1,140 ft/min
Single source(1,285 ft/min) on STOL variant
Single source5.8 m/s (1,140 ft/min) ; 6.53 m/s (1,285 ft/min) on STOL variant[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Cape Air FLN Frisia Luftverkehr APEX flight academy Pago Wings Pacific Air Charters[source]P2012 Traveller |
| Number built | >500[source] | 120[source]P2012 Traveller |
|---|
| Manufactured | 1984–present[source] | — |
|---|
| First flight | 21 September 1984 ( 1984-09-21 )[source] | 21 July 2016[source]P2012 Traveller |
|---|
| Developed from | Dassault Falcon 50[source] | — |
|---|
| Developed into | Dassault Falcon 2000 Dassault Falcon 7X[source] | — |
|---|
| Capacity | 19 passengers[source] | 9 passenger seats / 1,414 kg (3,117 lb) useful load including fuel[source] |
|---|
| Fuel capacity | 8,690 kg (19,160 lb)[source] | 880 L (230 US gal) usable fuel[source] |
|---|
| Aspect ratio | 7.63:1[source] | 7.7[source] |
|---|
| Stall speed | 158 km/h (98 mph, 85 kn) (wheels and flaps down)[source] | 120 km/h (75 mph, 65 kn) full flaps; 122 km/h (76 mph; 66 kn) full flaps on STOL variant[source] |
|---|
| Role | — | Utility aircraft[source]P2012 Traveller |
|---|
| Designer | — | Luigi Pascale[source]P2012 Traveller |
|---|
| Introduction date | — | 22 February 2020[source]P2012 Traveller |
|---|
| In service | — | 2020–present[source]P2012 Traveller |
|---|
| Propellers | — | 3 or 4-bladed MT-Propeller, 1.95 m (6 ft 5 in) diameter constant-speed fully-feathering propeller[source] |
|---|
| Never exceed speed | — | 419 km/h (260 mph, 226 kn)[source] |
|---|
| Wing loading | — | 145 kg/m 2 (30 lb/sq ft)[source] |
|---|
| Power/mass | — | 6.6 kg/kW (10.8 lb/hp)[source] |
|---|
| Takeoff run | — | 564 m (1,850 ft); 445 m (1,460 ft) on STOL variant[source] |
|---|
| Takeoff distance | — | 791 m (2,595 ft); 682 m (2,238 ft) on STOL variant[source] |
|---|
| Landing run | — | 365 m (1,198 ft); 290 m (950 ft) on STOL variant[source] |
|---|
| Landing distance | — | 743 m (2,438 ft); 590 m (1,940 ft) on STOL variant[source] |
|---|
| Fuel Consumption | — | 117 L/h (31 US gal/h)[source] |
|---|
Maximum take-off; Max takeoff weight
Single source