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]
Learjet 36A · Length
Single sourceConfiguration
| Specification | Cirrus SR20 | Learjet 35 |
|---|---|---|
| Type | Light aircraft[source] | Business jet[source] |
| Manufacturer | Cirrus Aircraft[source] | Learjet[source] |
| Number built | 2,084 (through 2025)[source] | 738[source] |
| Manufactured | 1999–present[source] | 1973–1994[source] |
48 ft 8 in (14.83 m)[source]
Cruise; SR20-G3 · TAS
Single source155 kn (178 mph, 287 km/h) TAS[source]
Learjet 36A · 4 passengers
Single source2,857 nmi (3,288 mi, 5,291 km) (4 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]
Learjet 36A · 2 × Garrett TFE731-2-2B turbofans thrust each
Single source2 × Garrett TFE731-2-2B turbofans , 3,500 lbf (16 kN) thrust each[source]
Learjet 36A · Wing area
Single source253.3 sq ft (23.53 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] | 22 August 1973[source] |
|---|
| Developed into | Cirrus SR22[source] | — |
|---|
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] | — |
|---|
| Propellers | 3-bladed[source] | — |
|---|
| Stall speed | 56 kn (64 mph, 104 km/h) CAS[source] | 96 kn (110 mph, 178 km/h) (wheels and flaps down)[source] |
|---|
| National origin | United States[source] | — |
|---|
| Status | — | Operational[source] |
|---|
| Primary user | — | General aviation, United States Air Force[source] |
|---|
| Developed from | — | Learjet 25[source] |
|---|
| Fuel capacity | — | 1,110 US gal (920 imp gal; 4,200 L) usable fuel[source] |
|---|
| Aspect ratio | — | 5.74:1[source] |
|---|
| Airfoil | — | NACA 64A-109 (mod)[source] |
|---|
| Take-off run to 30 ft (9 m) | — | 4,784 ft (1,458 m)[source] |
|---|
| Landing run from 50 ft (15 m) | — | 2,884 ft (879 m)[source] |
|---|
| Country of origin | — | United States[source] |
|---|