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]
MA600 · Length
Single sourceConfiguration
| Specification | Cirrus SR20 | Xi'an MA600 |
|---|---|---|
| Type | Light aircraft[source] | Turboprop Regional airliner[source] |
| Manufacturer | Cirrus Aircraft[source] | Xi'an Aircraft Industrial Corporation[source] |
| Number built | 2,084 (through 2025)[source] | 18[source] |
| Manufactured | 1999–present[source] | — |
24.71 m (81 ft 1 in)[source]
MA600 · per passenger with reserve + 45min., ISA
Single sourceMA600 · with 56 passengers and 198 lb (90kg)
Single source1,430 km (890 mi, 770 nmi) with 56 passengers and 198 lb (90kg) per passenger with reserve: 185 km + 45min., ISA[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]
MA600 · 2 × Pratt & Whitney Canada PW127J turboprop engines each
Single source2 × Pratt & Whitney Canada PW127J turboprop engines, 2,148 kW (2,881 hp) each[source]
SR20-G3 · 828 ft/min (
Single source828 ft/min (4.21 m/s)[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] |
10 October 2008[source] |
| Developed into | Cirrus SR22[source] | Xi'an MA700[source] |
|---|
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] | 60 passengers[source] |
|---|
| Propellers | 3-bladed[source] | — |
|---|
| Stall speed | 56 kn (64 mph, 104 km/h) CAS[source] | — |
|---|
| National origin | United States[source] | China[source] |
|---|
| Designer | — | Avic[source] |
|---|
| Status | — | In service[source] |
|---|
| Primary users | — | Civil Aviation Administration of China Laos Government Malawi Air Force Lao Skyway[source] |
|---|
| Introduction date | — | 2010[source] |
|---|
| Developed from | — | Xi'an MA60[source] |
|---|
| Taking off altitude limitation | — | 3,680 m (12,073 ft) AMSL[source] |
|---|