Credit
U.S. Air Force · Public domain · Resized · Public domain · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
VC-25A · Length
Single source231 ft 10 in (70.66 m)[source]
SR20-G3 · Length
Single sourceConfiguration
| Specification | Boeing VC-25 | Cirrus SR20 |
|---|---|---|
| Type | Presidential transport[source] | Light aircraft[source] |
| National origin | United States[source] | United States[source] |
| Manufacturer | Boeing[source] | Cirrus Aircraft[source] |
| Status | In service[source] | — |
| Primary user | United States Air Force |
26 ft 0 in (7.92 m)[source]
Cruise; VC-25A · / M0.84 at 35,000 ft (10,668 m)
Single sourceMaximum; VC-25A · at 35,000 ft (10,668 m)
Single source547.5 kn (630.1 mph, 1,014.0 km/h) at 35,000 ft (10,668 m)[source]
500 kn (580 mph, 930 km/h) / M0.84 at 35,000 ft (10,668 m)[source]
Cruise; SR20-G3 · TAS
Single source155 kn (178 mph, 287 km/h) TAS[source]
VC-25A · Range
Single source6,800 nmi (7,800 mi, 12,600 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]
VC-25A · 4 × General Electric CF6-80C2B1 turbofan engines thrust each
Single source4 × General Electric CF6-80C2B1 turbofan engines, 56,700 lbf (252 kN) thrust each[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.
| — |
| Number built | 2 (VC-25A)[source] | 2,084 (through 2025)[source] |
|---|
| Manufactured | 1986–1990; 2018–present[source] | 1999–present[source] |
|---|
| Introduction date | 23 August 1990[source] | — |
|---|
| First flight | 16 May 1987[source] | 21 March 1995[source] |
|---|
| Developed from | VC-25A: Boeing 747-200B VC-25B: Boeing 747-8I[source] | — |
|---|
| Variant | Boeing VC-25B Bridge[source] | — |
|---|
| Capacity | 76 passengers[source] | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] |
|---|
| Developed into | — | Cirrus SR22[source] |
|---|
| Propellers | — | 3-bladed[source] |
|---|
| Stall speed | — | 56 kn (64 mph, 104 km/h) CAS[source] |
|---|