FORCETALLY
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At a glance
Measured figures
Length
Single source155 ft 3 in (47.32 m)[source]
SR20-G3 · Length
Single sourceConfiguration
| Specification | Boeing C-32 | Cirrus SR20 |
|---|---|---|
| Type | VIP transport, special operations[source] | Light aircraft[source] |
| National origin | United States[source] | United States[source] |
| Manufacturer | Boeing[source] | Cirrus Aircraft[source] |
| Status | In service[source] | — |
| Primary user |
26 ft 0 in (7.92 m)[source]
Range
Single source5,650 nmi (6,500 mi, 10,460 km)[source]
SR20-G3 · 1 × Continental IO-360-ES six cylinder, horizontally-opposed piston aircraft engine
Single source1 × Continental IO-360-ES six cylinder, horizontally-opposed piston aircraft engine , 200 hp (150 kW)[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]
Wing area
Single source185.25 sq ft (17.210 m 2 )[source]
SR20-G3 · 828 ft/min (
Single source828 ft/min (4.21 m/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
United States Air Force[source]
| — |
| Number built | C-32A: 8 (4 acknowledged) C-32B: 2[source] | 2,084 (through 2025)[source] |
|---|
| Introduction date | June 1998[source] | — |
|---|
| Developed from | Boeing 757[source] | — |
|---|
| Capacity | 45[source] | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] |
|---|
| Fuel capacity | 13,334 US gal (11,103 imp gal; 50,475 L) with auxiliary tanks in fwd and aft cargo holds[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] | — |
|---|
| Manufactured | — | 1999–present[source] |
|---|
| First flight | — | 21 March 1995[source] |
|---|
| Developed into | — | Cirrus SR22[source] |
|---|
| Propellers | — | 3-bladed[source] |
|---|
| Stall speed | — | 56 kn (64 mph, 104 km/h) CAS[source] |
|---|