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]
DA62 · Length
Single sourceConfiguration
| Specification | Cirrus SR20 | Diamond DA62 |
|---|---|---|
| Type | Light aircraft[source] | Twin engine light aircraft[source] |
| Manufacturer | Cirrus Aircraft[source] | Diamond Aircraft Industries Aeromot[source] |
| Number built | 2,084 (through 2025)[source] | 273 (April 2024)[source] |
| Manufactured | 1999–present[source] | 2015–present |
9.19 m (30 ft 2 in)[source]
Cruise; SR20-G3 · TAS
Single source155 kn (178 mph, 287 km/h) TAS[source]
Cruise; DA62 · (TAS) at 75% power
Single sourceMaximum; DA62 · True Air Speed (TAS) at Maximum Continuous Power (MCP) at 14,000 ft (4,267 m)
Single source356 km/h (221 mph, 192 kn) True Air Speed (TAS) at Maximum Continuous Power (MCP) at 14,000 ft (4,267 m).[source]
317 km/h (197 mph, 171 kn) (TAS) at 75% power[source]
DA62 · Range
Single source2,380 km (1,480 mi, 1,290 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]
DA62 · 2 × Austro AE330 turbocharged 2.0 liter diesel aircraft engines each
Single source2 × Austro AE330 turbocharged 2.0 liter diesel aircraft engines , 134 kW (180 hp) each[source]
DA62 · Wing area
Single source17.10 m 2 (184.1 sq ft)[source]
DA62 · Endurance
Single source10 h[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] | 3 April 2012[source] |
|---|
| Developed into | Cirrus SR22[source] | — |
|---|
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] | up to six passengers[source] |
|---|
| Propellers | 3-bladed[source] | 3-bladed MT propeller MTV-6-R-C-F/CF 194-80[source] |
|---|
| Stall speed | 56 kn (64 mph, 104 km/h) CAS[source] | 125 km/h (78 mph, 67 kn)[source] |
|---|
| National origin | United States[source] | Austria[source] |
|---|
| Status | — | In production (DA62)[source] |
|---|
| Introduction date | — | October 2015[source] |
|---|
| Developed from | — | Diamond DA50[source] |
|---|
| Fuel capacity | — | 326 litres (72 imp gal; 86 US gal)[source] |
|---|
| Never exceed speed | — | 379 km/h (235 mph, 205 kn)[source] |
|---|
| Fuel consumption | — | 7.4 US gal (28 L) per hour total at loiter, 11.8 US gal (45 L) per hour at 60% (12,000 ft) in total[source] |
|---|