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]
360-300 · Length
Single sourceConfiguration
| Specification | Cirrus SR20 | Short 360 |
|---|---|---|
| Type | Light aircraft[source] | Transport aircraft[source] |
| Manufacturer | Cirrus Aircraft[source] | Short Brothers[source] |
| Number built | 2,084 (through 2025)[source] | 165[source] |
| Manufactured | 1999–present[source] | 1981–1991[source] |
21.58 m (70 ft 10 in)[source]
Cruise; SR20-G3 · TAS
Single source155 kn (178 mph, 287 km/h) TAS[source]
360-300 · full tanks, 2,569 kg (5,664 lb) payload
Single source1,595 km (991 mi, 861 nmi) full tanks, 2,569 kg (5,664 lb) payload[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]
360-300 · 2 × Pratt & Whitney Canada PT6 A-65AR turboprop (1,424 shp) each
Single source2 × Pratt & Whitney Canada PT6 A-65AR turboprop , 1,062 kW (1,424 shp) each[source]
360-300 · Wing area
Single source42.09 m 2 (454 sq ft)[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] | 1 June 1981[source] |
|---|
| Developed into | Cirrus SR22[source] | — |
|---|
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] | 36 passengers[source] |
|---|
| Propellers | 3-bladed[source] | — |
|---|
| Stall speed | 56 kn (64 mph, 104 km/h) CAS[source] | — |
|---|
| National origin | United States[source] | United Kingdom[source] |
|---|
| Status | — | In limited service[source] |
|---|
| Primary users | — | Air Cargo Carriers TransAir Skyway Enterprises Air Flamenco[source] |
|---|
| Introduction date | — | November 1982[source] |
|---|
| Developed from | — | Short 330[source] |
|---|
| Variant | — | Short C-23B/C Sherpa[source] |
|---|
| Airfoil | — | NACA 63A modified[source] |
|---|
| Fuel capacity | — | 2,182 L (480 imp gal; 576 US gal)[source] |
|---|
| Fuel consumption | — | 1.01 kg/km (3.57 lb/mi) 820 lb (370 kg)/h at 200 kn (370 km/h) TAS[source] |
|---|