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]
Y-7-100 · Length
Single sourceConfiguration
| Specification | Cirrus SR20 | Xi'an Y-7 |
|---|---|---|
| Type | Light aircraft[source] | Regional airliner / military transport[source] |
| Manufacturer | Cirrus Aircraft[source] | Xi'an Aircraft Industrial Corporation[source] |
| Number built | 2,084 (through 2025)[source] | 200+[source] |
| Manufactured | 1999–present[source] | 1977-present[source] |
24.218 m (79 ft 5 in)[source]
Y-7-100 · maximum payload
Single source910 km (570 mi, 490 nmi) maximum payload[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]
Y-7-100 · 2 × Dongan WJ-5A turboprop engines (2,400 shp) each equivalent
Single source2 × Dongan WJ-5A turboprop engines, 1,800 kW (2,400 shp) each equivalent[source]
SR20-G3 · 828 ft/min (
Single source828 ft/min (4.21 m/s)[source]
Y-7-100 · Wing area
Single source75.26 m 2 (810.1 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] | 20 February 1984[source] |
|---|
| Developed into | Cirrus SR22[source] | Xi'an MA60[source] |
|---|
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] | 52 passengers max[source] |
|---|
| Propellers | 3-bladed[source] | 4-bladed constant-speed feathering propellers, 3.9 m (12 ft 10 in) diameter[source] |
|---|
| Stall speed | 56 kn (64 mph, 104 km/h) CAS[source] | — |
|---|
| National origin | United States[source] | China[source] |
|---|
| Status | — | In military service, in production[source] |
|---|
| Primary users | — | People's Liberation Army Air Force People's Liberation Army Navy Air Force People's Liberation Army Ground Force Aviation[source] |
|---|
| Developed from | — | Antonov An-24 Antonov An-26[source] |
|---|
| Aspect ratio | — | 11.69[source] |
|---|
| Airfoil | — | root: TsAGI S-5-18; tip: TsAGI S-3-13[source] |
|---|
| Max zero-fuel weight | — | 19,655 kg (43,332 lb)[source] |
|---|
| Max landing weight | — | 21,800 kg (48,061 lb)[source] |
|---|
| Take-off run | — | 640 m (2,100 ft) at MTOW[source] |
|---|
| Landing run | — | 645 m (2,116 ft) at MLW[source] |
|---|