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At a glance
Measured figures
1956 model 310 · Length
Single source27 ft 0 in (8.23 m)[source]
Falcon 900B · Length
Single sourceConfiguration
| Specification | Cessna 310 | Dassault Falcon 900 |
|---|---|---|
| Type | Twin-engine cabin monoplane[source] | Business jet[source] |
| Manufacturer | Cessna[source] | Dassault Aviation[source] |
| Primary user | United States Air Force[source] | — |
| Number built | 5,449 (310) 577 (320)[source] | >500[source] |
20.21 m (66 ft 4 in)[source]
1956 model 310 · Height
Single source10 ft 6 in (3.20 m)[source]
1956 model 310 · 2 × Continental O-470-B horizontally opposed piston engine each
Single source2 × Continental O-470-B horizontally opposed piston engine, 240 hp (180 kW) 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]
1956 model 310 · 1,700 ft/min (
Single source1,700 ft/min (8.6 m/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Manufactured | 1954–1980[source] | 1984–present[source] |
|---|
| Introduction date | 1954[source] | — |
|---|
| First flight | January 3, 1953[source] | 21 September 1984 ( 1984-09-21 )[source] |
|---|
| Developed into | Cessna 340 Cessna 411[source] | Dassault Falcon 2000 Dassault Falcon 7X[source] |
|---|
| Capacity | four passengers[source] | 19 passengers[source] |
|---|
| Fuel capacity | 100 US gal (83 imp gal; 380 L)[source] | 8,690 kg (19,160 lb)[source] |
|---|
| National origin | United States[source] | France[source] |
|---|
| Status | — | Active service, in production[source] |
|---|
| Primary users | — | French Air and Space Force Japan Coast Guard Nigerian Air Force Royal Malaysian Air Force[source] |
|---|
| Developed from | — | Dassault Falcon 50[source] |
|---|
| Aspect ratio | — | 7.63:1[source] |
|---|
| Stall speed | — | 158 km/h (98 mph, 85 kn) (wheels and flaps down)[source] |
|---|