Credit
Rijkswaterstaat · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
402C Businessliner · Length
Single source36 ft 4 + 1 ⁄ 2 in (11.09 m)[source]
Falcon 900B · Length
Configuration
| Specification | Cessna 402 | Dassault Falcon 900 |
|---|---|---|
| Type | Corporate transport and airliner[source] | Business jet[source] |
| National origin | United States[source] | France[source] |
| Manufacturer | Cessna[source] | Dassault Aviation[source] |
| Status | In service[source] | Active service, in production |
20.21 m (66 ft 4 in)[source]
402C Businessliner · Height
Single source11 ft 5 + 1 ⁄ 2 in (3.49 m)[source]
Empty; 402C Businessliner · Empty weight
Single sourceMaximum take-off; 402C Businessliner · Max takeoff weight
Single source4,077 lb (1,849 kg)[source]
6,850 lb (3,107 kg)[source]
Empty; Falcon 900B · Empty weight
Single sourceMaximum take-off; Falcon 900B · Max takeoff weight
Single source402C Businessliner · 2 × Continental TSIO-520-VB air-cooled turbocharged flat-six engines each
Single source2 × Continental TSIO-520-VB air-cooled turbocharged flat-six engines, 325 hp (242 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]
402C Businessliner · 1,450 ft/min (
Single source1,450 ft/min (7.4 m/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Primary user | Cape Air[source] | — |
|---|
| Number built | 2,000+[source] | >500[source] |
|---|
| Manufactured | 1966–1985[source] | 1984–present[source] |
|---|
| Introduction date | 1967[source] | — |
|---|
| First flight | August 26, 1965[source] | 21 September 1984 ( 1984-09-21 )[source] |
|---|
| Developed from | Cessna 411[source] | Dassault Falcon 50[source] |
|---|
| Developed into | Cessna 404 Titan Cessna 414[source] | Dassault Falcon 2000 Dassault Falcon 7X[source] |
|---|
| Capacity | Six passengers[source] | 19 passengers[source] |
|---|
| Airfoil | NACA 23018 (root) NACA 23015 (tip)[source] | — |
|---|
| Fuel capacity | 206 US gal (172 imp gal; 780 L) usable fuel[source] | 8,690 kg (19,160 lb)[source] |
|---|
| Propellers | 3-bladed McCauley 0850334-34 constant speed propeller[source] | — |
|---|
| Stall speed | 68 kn (78 mph, 126 km/h) (flaps down, power off) (CAS)[source] | 158 km/h (98 mph, 85 kn) (wheels and flaps down)[source] |
|---|
| Never exceed speed | 231 kn (266 mph, 428 km/h) ( CAS )[source] | — |
|---|
| Takeoff distance to 50 ft (15m) | 2,195 ft (669 m)[source] | — |
|---|
| Landing distance from 50 ft (15m) | 2,485 ft (757 m)[source] | — |
|---|
| Primary users | — | French Air and Space Force Japan Coast Guard Nigerian Air Force Royal Malaysian Air Force[source] |
|---|
| Aspect ratio | — | 7.63:1[source] |
|---|