FORCETALLY
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At a glance
Measured figures
Length
Single source155 ft 3 in (47.32 m)[source]
Falcon 900B · Length
Single sourceConfiguration
| Specification | Boeing C-32 | Dassault Falcon 900 |
|---|---|---|
| Type | VIP transport, special operations[source] | Business jet[source] |
| National origin | United States[source] | France[source] |
| Manufacturer | Boeing[source] | Dassault Aviation[source] |
| Status | In service[source] | Active service, in production[source] |
20.21 m (66 ft 4 in)[source]
at MTOW
Single source44 ft 3 in (13.49 m) at MTOW[source]
2 × Pratt & Whitney PW2000 -40 turbofan engines thrust each
Single source2 × Pratt & Whitney PW2000 -40 turbofan engines, 40,100 lbf (178 kN) thrust 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]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Primary user | United States Air Force[source] | — |
|---|
| Number built | C-32A: 8 (4 acknowledged) C-32B: 2[source] | >500[source] |
|---|
| Introduction date | June 1998[source] | — |
|---|
| Developed from | Boeing 757[source] | Dassault Falcon 50[source] |
|---|
| Capacity | 45[source] | 19 passengers[source] |
|---|
| Fuel capacity | 13,334 US gal (11,103 imp gal; 50,475 L) with auxiliary tanks in fwd and aft cargo holds[source] | 8,690 kg (19,160 lb)[source] |
|---|
| Maximum zero-fuel weight | 186,000 lb (84,368 kg) MZFW[source] | — |
|---|
| Maximum landing weight | 210,000 lb (95,254 kg) MLW[source] | — |
|---|
| Approach speed | 137 kn (158 mph; 254 km/h)[source] | — |
|---|
| Initial cruising height | 35,400 ft (10,790 m)[source] | — |
|---|
| Wing loading | 127.88 lb/sq ft (624.4 kg/m 2 )[source] | — |
|---|
| Thrust/weight | 0.314[source] | — |
|---|
| Take-off field length | 7,800 ft (2,377 m) at sea level 29 °C (84 °F)[source] | — |
|---|
| Landing field length | 5,100 ft (1,554 m) at MLW[source] | — |
|---|
| Primary users | — | French Air and Space Force Japan Coast Guard Nigerian Air Force Royal Malaysian Air Force[source] |
|---|
| Manufactured | — | 1984–present[source] |
|---|
| First flight | — | 21 September 1984 ( 1984-09-21 )[source] |
|---|
| Developed into | — | Dassault Falcon 2000 Dassault Falcon 7X[source] |
|---|
| Aspect ratio | — | 7.63:1[source] |
|---|
| Stall speed | — | 158 km/h (98 mph, 85 kn) (wheels and flaps down)[source] |
|---|