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At a glance
Measured figures
Falcon 900B · Length
Single source20.21 m (66 ft 4 in)[source]
DA62 · Length
Single sourceConfiguration
| Specification | Dassault Falcon 900 | Diamond DA62 |
|---|---|---|
| Type | Business jet[source] | Twin engine light aircraft[source] |
| National origin | France[source] | Austria[source] |
| Manufacturer | Dassault Aviation[source] | Diamond Aircraft Industries Aeromot[source] |
| Status | Active service, in production[source] | In production (DA62) |
9.19 m (30 ft 2 in)[source]
DA62 · Height
Single source2.82 m (9 ft 3 in)[source]
Cruise; Falcon 900B · Mach 0.85 (at 11,000 m (36,000 ft))
Single sourceMach 0.84–0.87[source]
950 km/h (590 mph, 510 kn) ; Mach 0.85 (at 11,000 m (36,000 ft))[source]
Cruise; DA62 · (TAS) at 75% power
Single sourceMaximum; DA62 · True Air Speed (TAS) at Maximum Continuous Power (MCP) at 14,000 ft (4,267 m)
Single source356 km/h (221 mph, 192 kn) True Air Speed (TAS) at Maximum Continuous Power (MCP) at 14,000 ft (4,267 m).[source]
317 km/h (197 mph, 171 kn) (TAS) at 75% power[source]
DA62 · 2 × Austro AE330 turbocharged 2.0 liter diesel aircraft engines each
Single source2 × Austro AE330 turbocharged 2.0 liter diesel aircraft engines , 134 kW (180 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]
DA62 · Endurance
Single source10 h[source]
DA62 · 1,029 ft/min
Single source5.2 m/s (1,029 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] | 273 (April 2024)[source] |
|---|
| Manufactured | 1984–present[source] | 2015–present[source] |
|---|
| First flight | 21 September 1984 ( 1984-09-21 )[source] | 3 April 2012[source] |
|---|
| Developed from | Dassault Falcon 50[source] | Diamond DA50[source] |
|---|
| Developed into | Dassault Falcon 2000 Dassault Falcon 7X[source] | — |
|---|
| Capacity | 19 passengers[source] | up to six passengers[source] |
|---|
| Fuel capacity | 8,690 kg (19,160 lb)[source] | 326 litres (72 imp gal; 86 US gal)[source] |
|---|
| Aspect ratio | 7.63:1[source] | — |
|---|
| Stall speed | 158 km/h (98 mph, 85 kn) (wheels and flaps down)[source] | 125 km/h (78 mph, 67 kn)[source] |
|---|
| Introduction date | — | October 2015[source] |
|---|
| Propellers | — | 3-bladed MT propeller MTV-6-R-C-F/CF 194-80[source] |
|---|
| Never exceed speed | — | 379 km/h (235 mph, 205 kn)[source] |
|---|
| Fuel consumption | — | 7.4 US gal (28 L) per hour total at loiter, 11.8 US gal (45 L) per hour at 60% (12,000 ft) in total[source] |
|---|