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]
330-200 · Length
Single sourceConfiguration
| Specification | Cirrus SR20 | Short 330 |
|---|---|---|
| Type | Light aircraft[source] | Transport aircraft[source] |
| Manufacturer | Cirrus Aircraft[source] | Short Brothers[source] |
| Number built | 2,084 (through 2025)[source] | 330-100: 68 330-200: 73[source] |
| Manufactured | 1999–present[source] | 1974–1992 |
17.69 m (58 ft 0 in)[source]
Cruise; SR20-G3 · TAS
Single source155 kn (178 mph, 287 km/h) TAS[source]
330-200 · (no reserves, passenger version, 1,966 kg (4,334 lb) payload)
Single source1,695 km (1,053 mi, 915 nmi) (no reserves, passenger version, 1,966 kg (4,334 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]
330-200 · 2 × Pratt & Whitney Canada PT6 A-45-R turboprop (1,198 shp) each
Single source2 × Pratt & Whitney Canada PT6 A-45-R turboprop , 893 kW (1,198 shp) each[source]
330-200 · Wing area
Single source42.1 m 2 (453 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] | 22 August 1974[source] |
|---|
| Developed into | Cirrus SR22[source] | Short 360[source] |
|---|
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] | — |
|---|
| Propellers | 3-bladed[source] | 5-bladed Hartzell constant-speed[source] |
|---|
| Stall speed | 56 kn (64 mph, 104 km/h) CAS[source] | 135 km/h (84 mph, 73 kn) (landing gear and flaps down)[source] |
|---|
| National origin | United States[source] | United Kingdom[source] |
|---|
| Status | — | In limited cargo service[source] |
|---|
| Primary users | — | Air Cargo Carriers Corporate Air[source] |
|---|
| Introduction date | — | 1976[source] |
|---|
| Developed from | — | Short Skyvan[source] |
|---|
| Variant | — | C-23A Sherpa[source] |
|---|
| Airfoil | — | NACA 63A series (modified)[source] |
|---|
| Fuel capacity | — | 2,546 L (560 imp gal; 673 US gal)[source] |
|---|