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 V |
|---|---|---|
| Type | Light aircraft[source] | Business jet[source] |
| Manufacturer | Cirrus Aircraft[source] | Gulfstream Aerospace[source] |
| Number built | 2,084 (through 2025)[source] | 193[source] |
| Manufactured | 1999–present[source] | 1995–2002[source] |
96.4 ft (29.4 m)[source]
long range cruise with 4 crew, 8 passengers
Single source7,500 mi (12,000 km, 6,500 nmi) , long range cruise with 4 crew, 8 passengers[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 A1-10 turbofan thrust each
Single source2 × Rolls-Royce BR710 A1-10 turbofan, 14,750 lbf (65.6 kN) thrust each[source]
SR20-G3 · 828 ft/min (
Single source828 ft/min (4.21 m/s)[source]
Wing area
Single source1,137 sq ft (105.6 m 2 )[source]
Maximum Payload
Single source8,300 pounds (3,800 kg)[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] | November 28, 1995[source] |
|---|
| Developed into | Cirrus SR22[source] | Gulfstream G550[source] |
|---|
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] | 15–19[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 Coast Guard United States Navy[source] |
|---|
| Introduction date | — | June 1997[source] |
|---|
| Developed from | — | Gulfstream IV[source] |
|---|
| Aspect ratio | — | 7.68[source] |
|---|
| Maximum Landing Weight | — | 75,300 pounds (34,200 kg)[source] |
|---|
| Maximum Zero Fuel Weight | — | 54,500 pounds (24,700 kg)[source] |
|---|
| Maximum Fuel Load | — | 41,300 pounds (18,700 kg)[source] |
|---|
| Payload w/ Max Fuel | — | 3,400 pounds (1,500 kg)[source] |
|---|
| Cabin Length | — | 43.92 feet (13.39 m)[source] |
|---|
| Cabin floor Width | — | 5.25 feet (1.60 m)[source] |
|---|
| Cabin Height | — | 6.17 feet (1.88 m)[source] |
|---|
| Normal cruise range | — | 5,500 nautical miles (10,186 km), with 5 crew, 12 passengers[source] |
|---|
| Takeoff distance MTOW, ISA, SL | — | 6,100 feet (1,900 m)[source] |
|---|
| Climb rate | — | 4,188 feet per minute (21.28 m/s)[source] |
|---|
Maximum take-off; Max takeoff weight
Single source