Credit
Tomás Del Coro from Las Vegas, Nevada, USA · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
SR20-G3 · Length
Single source26 ft 0 in (7.92 m)[source]
Hawker 400XPR · Length
Single sourceConfiguration
| Specification | Cirrus SR20 | Hawker 400 |
|---|---|---|
| Type | Light aircraft[source] | Business jet[source] |
| Manufacturer | Cirrus Aircraft[source] | Hawker Beechcraft[source] |
| Number built | 2,084 (through 2025)[source] | 951: 92 Mitsubishi MU-300, 859 Beechjet 400[source] |
| Manufactured | 1999–present[source] | 1978–2009[source] |
48 ft 5 in (14.76 m)[source]
Cruise; SR20-G3 · TAS
Single source155 kn (178 mph, 287 km/h) TAS[source]
Hawker 400XPR · at 45,000 ft (13,700 m)
Single source2,160 nmi (2,490 mi, 4,000 km) at 45,000 ft (13,700 m)[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]
Hawker 400XPR · 2 × Williams International FJ44 -4A-32 turbofan thrust each
Single source2 × Williams International FJ44 -4A-32 turbofan , 3,200 lbf (14 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.
| First flight | 21 March 1995[source] | August 29, 1978 (as Mitsubishi Diamond)[source] |
|---|
| Developed into | Cirrus SR22[source] | — |
|---|
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] | 7–9 passengers, 5,600 lb (2,500 kg) useful load[source] |
|---|
| Propellers | 3-bladed[source] | — |
|---|
| Stall speed | 56 kn (64 mph, 104 km/h) CAS[source] | 92 kn (106 mph, 171 km/h) (full flaps)[source] |
|---|
| National origin | United States[source] | Japan/United States[source] |
|---|
| Status | — | Out of production, in service[source] |
|---|
| Primary users | — | Flight Options Travel Management Co.[source] |
|---|
| Variants | — | T-1 Jayhawk Nextant 400XT[source] |
|---|
| Pressurization | — | 9.1 psi (0.63 bar)[source] |
|---|
| Cabin height | — | 4.75 ft (1.45 m)[source] |
|---|
| Cabin width | — | 4.92 ft (1.50 m)[source] |
|---|
| Fuel burn at high-speed cruise | — | 913 lb/h (414 kg/h) at 447 kn TAS at FL450[source] |
|---|
| Fuel burn at long-range cruise | — | 761 lb/h (345 kg/h) at 425 kn TAS at FL450[source] |
|---|