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]
L-410 UVP-E20 · Length
Single sourceConfiguration
| Specification | Cirrus SR20 | Let L-410 Turbolet |
|---|---|---|
| Type | Light aircraft[source] | Regional airliner , cargo aircraft[source] |
| Manufacturer | Cirrus Aircraft[source] | Let Kunovice[source] |
| Number built | 2,084 (through 2025)[source] | 1,200[source] |
| Manufactured | 1999–present[source] | 1971–present |
14.42 m (47 ft 4 in)[source]
L-410 UVP-E20 · 1,800 kg (3,968 lb) payload, ISA, FL140, 45 min reserve
Single source1,500 km (930 mi, 810 nmi) 1,800 kg (3,968 lb) payload, ISA, FL140, 45 min reserve[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]
L-410 UVP-E20 · 2 × General Electric H80-200 turboprop engines each
Single source2 × General Electric H80-200 turboprop engines, 597 kW (801 hp) each[source]
L-410 UVP-E20 · Wing area
Single source34.86 m 2 (375.2 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] | 16 April 1969[source] |
|---|
| Developed into | Cirrus SR22[source] | Let L-610[source] |
|---|
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] | 19 passengers / 1,800 kg (3,968 lb) payload[source] |
|---|
| Propellers | 3-bladed[source] | 5-bladed Avia AV 725, 2.3 m (7 ft 7 in) diameter[source] |
|---|
| Stall speed | 56 kn (64 mph, 104 km/h) CAS[source] | — |
|---|
| National origin | United States[source] | — |
|---|
| Status | — | In service[source] |
|---|
| Primary users | — | Russian Air Force Slovak Air Force Searca Aeroflot (historical)[source] |
|---|
| Introduction date | — | 1970[source] |
|---|
| Variant | — | Aircraft Industries L 410 NG[source] |
|---|
| Fuel capacity | — | 1,300 kg (2,866 lb)[source] |
|---|
| Endurance | — | Five hours and six minutes[source] |
|---|
| Aspect ratio | — | 11.45[source] |
|---|
| Airfoil | — | root: NACA 63A418 ; tip: NACA 63A412[source] |
|---|
| Fuel consumption | — | 240 kg/h (529 lb/h)[source] |
|---|
| Take-off run | — | 510 m (1,670 ft) (ISA, SL, MTOW)[source] |
|---|
| Landing run | — | 500 m (1,600 ft) (ISA, SL, MTOW)[source] |
|---|
| Alternative designation | — | L-410 Turbolet[source] |
|---|
| Country of origin | — | Czechoslovakia[source] |
|---|