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]
Length
Single sourceConfiguration
| Specification | Cirrus SR20 | Gulfstream G550 |
|---|---|---|
| Type | Light aircraft[source] | Business jet[source] |
| Manufacturer | Cirrus Aircraft[source] | Gulfstream Aerospace[source] |
| Number built | 2,084 (through 2025)[source] | >600[source] |
| Manufactured | 1999–present[source] | 2003–2021[source] |
96 ft 5 in (29.39 m)[source]
Cruise; SR20-G3 · TAS
Single source155 kn (178 mph, 287 km/h) TAS[source]
Range
Single source6,750 nmi (7,770 mi, 12,500 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 × Rolls-Royce BR710 C4-11 turbofan engines thrust each
Single source2 × Rolls-Royce BR710 C4-11 turbofan engines, 15,385 lbf (68.44 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] | 31 August 2001[source] |
|---|
| Developed into | Cirrus SR22[source] | — |
|---|
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] | 14–19 passengers / 6,200 lb (2,812 kg) payload[source] |
|---|
| Propellers | 3-bladed[source] | — |
|---|
| Stall speed | 56 kn (64 mph, 104 km/h) CAS[source] | — |
|---|
| National origin | United States[source] | United States[source] |
|---|
| Status | — | In service[source] |
|---|
| Primary users | — | United States Air Force United States Navy Israeli Air Force[source] |
|---|
| Introduction date | — | 2004[source] |
|---|
| Developed from | — | Gulfstream V[source] |
|---|
| Variant | — | L3Harris EA-37B Compass Call[source] |
|---|
| Successors | — | Gulfstream G600[source] |
|---|
| Fuel capacity | — | 41,300 lb (18,733 kg)[source] |
|---|
| Cabin dimensions: height × width × length | — | 6 ft 2 in × 7 ft 4 in × 43 ft 11 in (1.88 m × 2.24 m × 13.39 m); total length including baggage hold: 50 ft 1 in (15.27 m)[source] |
|---|
| Cabin volume | — | 1,669 cu ft (47.26 m 3 ); usable baggage compartment volume: 170 cu ft (4.81 m 3 )[source] |
|---|
| Cabin altitude | — | 6,000 ft (1,829 m)[source] |
|---|
| Airfoil | — | root: NACA 0012; tip: NACA 0012[source] |
|---|
| Maximum landing weight | — | 75,300 lb (34,156 kg)[source] |
|---|
| High Speed Cruise | — | M0.85 at 41,000 ft (12,000 m)[source] |
|---|
| Long Range Cruise | — | M0.80 at 41,000 ft (12,000 m)[source] |
|---|
| Maximum Mach Operating (MMO) | — | M0.885 at 41,000 ft (12,000 m)[source] |
|---|
| Take-off run | — | 5,910 ft (1,800 m)[source] |
|---|
| Landing run | — | 2,770 ft (840 m)[source] |
|---|
Maximum take-off; Max takeoff weight