Credit
Tomás Del Coro from Las Vegas, Nevada, USA · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
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At a glance
Measured figures
SR20-G3 · Length
Single source26 ft 0 in (7.92 m)[source]
MA60 · Length
Single sourceConfiguration
| Specification | Cirrus SR20 | Xi'an MA60 |
|---|---|---|
| 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] | 110 (March 2013)[source] |
| Manufactured | 1999–present[source] | 2000–present |
24.71 m (81 ft 1 in)[source]
MA60 · Range
Single source1,600 km (990 mi, 860 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]
MA60 · 2 × Pratt & Whitney Canada PW127J turbo prop engines each
Single source2 × Pratt & Whitney Canada PW127J turbo prop engines, 2,051 kW (2,750 hp) each[source]
SR20-G3 · 828 ft/min (
Single source828 ft/min (4.21 m/s)[source]
MA60 · Wing area
Single source75 m 2 (810 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] | 25 February 2000[source] |
|---|
| Developed into | Cirrus SR22[source] | Xi'an MA600[source] |
|---|
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] | 62 passengers[source] |
|---|
| Propellers | 3-bladed[source] | 4-bladed Hamilton Sundstrand 247F-3 constant-speed propellers[source] |
|---|
| Stall speed | 56 kn (64 mph, 104 km/h) CAS[source] | — |
|---|
| National origin | United States[source] | China[source] |
|---|
| Status | — | In service, in production[source] |
|---|
| Primary users | — | People's Liberation Army Air Force People's Liberation Army Navy Air Force China Meteorological Administration Lao Skyway[source] |
|---|
| Introduction date | — | August 2000 with Sichuan Airlines[source] |
|---|
| Developed from | — | Xi'an Y-7[source] |
|---|
| Airfoil | — | root: TsAGI S-5-18; tip: TsAGI S-3-13[source] |
|---|