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At a glance
Measured figures
SR20-G3 · Length
Single source26 ft 0 in (7.92 m)[source]
JetStar II · Length
Single sourceConfiguration
| Specification | Cirrus SR20 | Lockheed JetStar |
|---|---|---|
| Type | Light aircraft[source] | Transport[source] |
| Manufacturer | Cirrus Aircraft[source] | Lockheed Corporation[source] |
| Number built | 2,084 (through 2025)[source] | 202[source] |
| Manufactured | 1999–present[source] | 1961–1980 |
60 ft 5 in (18.41 m)[source]
JetStar II · Range
Single source2,995 mi (4,820 km, 2,604 nmi)[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]
JetStar II · 4 × Garrett TFE731-3 turbofan thrust each
Single source4 × Garrett TFE731-3 turbofan , 3,700 lbf (16 kN) thrust each[source]
JetStar II · Wing area
Single source542.5 sq ft (50.4 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] | 4 September 1957[source] |
|---|
| Developed into | Cirrus SR22[source] | — |
|---|
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] | 8–10 passengers[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 limited service[source] |
|---|
| Primary users | — | United States Air Force (historical) Mexican Air Force Islamic Republic of Iran Air Force[source] |
|---|
| Introduction date | — | 1961[source] |
|---|
| Retired | — | 1990s ( United States Air Force )[source] |
|---|
Maximum take-off; JetStar II · Max takeoff weight
Single source