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]
Gulfstream II-B · Length
Single sourceConfiguration
| Specification | Cirrus SR20 | Grumman Gulfstream II |
|---|---|---|
| Type | Light aircraft[source] | Business jet[source] |
| Manufacturer | Cirrus Aircraft[source] | Grumman / Gulfstream Aerospace[source] |
| Number built | 2,084 (through 2025)[source] | 256[source] |
| Manufactured | 1999–present[source] | 1967–1980 |
79 ft 11 in (24.36 m)[source]
Cruise; SR20-G3 · TAS
Single source155 kn (178 mph, 287 km/h) TAS[source]
Gulfstream II-B · with 8 passengers, NBAA IFR reserves, crew of 3, 2,000 lb (900 kg) / pax
Single source3,550 nmi (4,090 mi, 6,570 km) with 8 passengers, NBAA IFR reserves, crew of 3, 2,000 lb (900 kg) / pax[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]
Gulfstream II-B · 2 × Rolls-Royce Spey 511-8 turbofan engines thrust each
Single source2 × Rolls-Royce Spey 511-8 turbofan engines, 11,400 lbf (51 kN) thrust each[source]
Gulfstream II-B · Wing area
Single source934.6 sq ft (86.83 m 2 )[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] | 2 October 1966[source] |
|---|
| Developed into | Cirrus SR22[source] | Gulfstream III[source] |
|---|
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] | 19 (maximum certified) / 2,900 lb (1,315 kg) maximum payload[source] |
|---|
| Propellers | 3-bladed[source] | — |
|---|
| Stall speed | 56 kn (64 mph, 104 km/h) CAS[source] | 105 kn (121 mph, 194 km/h) at MLW, flaps down[source] |
|---|
| National origin | United States[source] | United States[source] |
|---|
| Status | — | In service[source] |
|---|
| Airfoil | — | stn.50: NACA 0012 modified ; stn 145: NACA 63A-009.5 ; stn 385: NACA 64 series modified[source] |
|---|
| Maximum zero-fuel weight | — | 42,000 lb (19,051 kg)[source] |
|---|
| Maximum landing weight | — | 58,500 lb (26,535 kg)[source] |
|---|
| Fuel capacity | — | 28,300 lb (12,837 kg) maximum[source] |
|---|
| Maximum cruising Mach number | — | M0.85 at max power at 30,000 ft (9,144 m) and AUW of 55,000 lb (24,948 kg)[source] |
|---|
| Maximum Mach speed | — | M0.85[source] |
|---|
| Economical cruise speed | — | M0.77[source] |
|---|
| Take-off run (FAA) | — | 5,850 ft (1,783 m)[source] |
|---|
| Landing run (FAA) | — | 3,400 ft (1,036 m)[source] |
|---|
| Operational Noise levels (FAR Pt.36) | — | Take-off: 91 EPNdB Approach: 97 EPNdB Sideline: 103 EPNdB[source] |
|---|
| Take-off | — | 91 EPNdB[source] |
|---|
| Approach | — | 97 EPNdB[source] |
|---|
| Sideline | — | 103 EPNdB[source] |
|---|
Maximum take-off; Gulfstream II-B · Max takeoff weight
Single source