FORCETALLY
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At a glance
Measured figures
337D · Length
Single source29 ft 9 in (9.07 m)[source]
Falcon 900B · Length
Single sourceConfiguration
| Specification | Cessna Skymaster | Dassault Falcon 900 |
|---|---|---|
| Type | Personal use and air taxi aircraft[source] | Business jet[source] |
| National origin | United States[source] | France[source] |
| Manufacturer | Cessna Reims Aviation[source] | Dassault Aviation[source] |
| Number built | 2,993[source] |
20.21 m (66 ft 4 in)[source]
337D · Height
Single source9 ft 4 in (2.84 m)[source]
337D · 2 × Continental IO-360-C air-cooled flat-six piston engine each
Single source2 × Continental IO-360-C air-cooled flat-six piston engine, 210 hp (160 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]
337D · 1,200 ft/min (
Single source1,200 ft/min (6.1 m/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
>500[source] |
| Manufactured | 1963–1982[source] | 1984–present[source] |
|---|
| Introduction date | 1962[source] | — |
|---|
| First flight | February 28, 1961[source] | 21 September 1984 ( 1984-09-21 )[source] |
|---|
| Variants | Cessna O-2 Skymaster Conroy Stolifter Spectrum SA-550[source] | — |
|---|
| Capacity | 5 passengers[source] | 19 passengers[source] |
|---|
| Aspect ratio | 7.18:1[source] | 7.63:1[source] |
|---|
| Airfoil | NACA 2412 at root, NACA 2409 at tip[source] | — |
|---|
| Fuel capacity | 92 US gal (77 imp gal; 350 L) normal, 128 US gal (107 imp gal; 480 L) with auxiliary tanks[source] | 8,690 kg (19,160 lb)[source] |
|---|
| Propellers | 2-bladed McCauley fully-feathering, constant-speed propeller, 6 ft 4 in (1.93 m) diameter[source] | — |
|---|
| Stall speed | 69 mph (111 km/h, 60 kn) (flaps and undercarriage down)[source] | 158 km/h (98 mph, 85 kn) (wheels and flaps down)[source] |
|---|
| Takeoff distance to 50 ft (15m) | 1,545 ft (471 m)[source] | — |
|---|
| Landing distance from 50 ft (15m) | 1,650 ft (500 m)[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] |
|---|
| Developed into | — | Dassault Falcon 2000 Dassault Falcon 7X[source] |
|---|