Credit
Tomás Del Coro from Las Vegas, Nevada, USA · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
SR20-G3 · Length
Single source26 ft 0 in (7.92 m)[source]
Length
Cross-checkedConfiguration
| Specification | Cirrus SR20 | Saab 2000 |
|---|---|---|
| Type | Light aircraft[source] | Turboprop Regional airliner[source] |
| Manufacturer | Cirrus Aircraft[source] | Saab AB[source] |
| Number built | 2,084 (through 2025)[source] | 63[source] |
| Manufactured | 1999–present[source] | 1992–1999[source] |
Official specification · length; 27,28 m
Manufacturer claimSaab 2000 specs · Length
Cross-checkedRange
Single source2,869 km (1,783 mi, 1,549 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]
2 × Rolls-Royce AE 2100P turboprop engines each
Single source2 × Rolls-Royce AE 2100P turboprop engines, 3,096 kW (4,152 hp) each[source]
Wing area
Single source55.7 m 2 (600 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] | 26 March 1992[source] |
|---|
| Developed into | Cirrus SR22[source] | — |
|---|
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] | 50–58 passengers / 5,900 kg (13,007 lb) payload[source] 4.250 kg[source] 50–58 passengers / 5,900 kg (13,007 lb) payload[source] |
|---|
| Propellers | 3-bladed[source] | 6-bladed Dowty Propellers constant-speed composite fully feathering and reversible-pitch propellers[source] |
|---|
| Stall speed | 56 kn (64 mph, 104 km/h) CAS[source] | — |
|---|
| National origin | United States[source] | Sweden[source] |
|---|
| Status | — | In limited passenger service, in military service[source] |
|---|
| Introduction date | — | 30 August 1994[source] |
|---|
| Developed from | — | Saab 340[source] |
|---|
| Airfoil | — | root: NASA/Langley MS(1)-0316; tip: NASA/Langley MS(1)-0312[source] |
|---|
| Field length | — | 1,200 m[source] |
|---|