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]
Dornier 228NG · Length
Single sourceConfiguration
| Specification | Cirrus SR20 | Dornier 228 |
|---|---|---|
| Type | Light aircraft[source] | Utility aircraft[source] |
| Manufacturer | Cirrus Aircraft[source] | Dornier GmbH RUAG General Atomics AeroTec Systems GmbH[source] |
| Number built | 2,084 (through 2025)[source] | Dornier: 245 HAL: 125[source] |
| Manufactured | 1999–present[source] | Dornier: 1982–1997 HAL : 1985–present RUAG: 2010–2020 General Atomics: 2021-Present |
16.56 m (54 ft 4 in)[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]
Dornier 228NG · 2 × Honeywell TPE331-10 turboprop (776 shp) each
Single source2 × Honeywell TPE331-10 turboprop , 579 kW (776 shp) each[source]
SR20-G3 · 828 ft/min (
Single source828 ft/min (4.21 m/s)[source]
Dornier 228NG · Wing area
Single source32 m 2 (340 sq ft)[source]
Dornier 228NG · Endurance
Single source10 hours[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] | 28 March 1981[source] |
|---|
| Developed into | Cirrus SR22[source] | — |
|---|
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] | 19 passengers[source] |
|---|
| Propellers | 3-bladed[source] | 5-bladed MT-Propeller , 2.5 m (8 ft 2 in) diameter fully- feathering constant-speed propellers[source] |
|---|
| Stall speed | 56 kn (64 mph, 104 km/h) CAS[source] | 137 km/h (85 mph, 74 kn)[source] |
|---|
| National origin | United States[source] | — |
|---|
| Built by | — | Hindustan Aeronautics Limited[source] |
|---|
| Status | — | In service[source] |
|---|
| Primary users | — | Indian Air Force Indian Coast Guard Indian Navy[source] |
|---|
| Introduction date | — | July 1982[source] |
|---|
| Developed from | — | Dornier Do 28[source] |
|---|
| Fuel capacity | — | 1,885 kg (4,156 lb)[source] |
|---|
| Airfoil | — | Do A-5[source] |
|---|
| Fuel consumption | — | 0.945 kg/km (3.35 lb/mi) at 413 km/h (257 mph; 223 kn) IAS[source] |
|---|
| Take-off run | — | 792 m (2,600 ft) (MTOW, ISA, SL)[source] |
|---|
| Landing run | — | 451 m (1,480 ft) (MLW, ISA, SL)[source] |
|---|
| Country of origin | — | Germany[source] |
|---|