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At a glance
Measured figures
SR20-G3 · Length
Single source26 ft 0 in (7.92 m)[source]
Y-8 · Length
Single sourceConfiguration
| Specification | Cirrus SR20 | Shaanxi Y-8 |
|---|---|---|
| Type | Light aircraft[source] | Military transport aircraft / Maritime patrol aircraft[source] |
| Manufacturer | Cirrus Aircraft[source] | Shaanxi Aircraft Corporation[source] |
| Number built | 2,084 (through 2025)[source] | 169 (2010)[source] |
| Manufactured | 1999–present[source] | 1981–present |
34.02 m (111 ft 7 in)[source]
Y-8 · Range
Single source5,615 km (3,489 mi, 3,032 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]
Y-8 · 4 × Zhuzhou WoJiang-6 (WJ-6) turboprop engines each
Single source4 × Zhuzhou WoJiang-6 (WJ-6) turboprop engines, 3,170 kW (4,250 hp) each[source]
Y-8 · Wing area
Single source121.9 m 2 (1,312 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 December 1974[source] |
|---|
| Developed into | Cirrus SR22[source] | Shaanxi Y-9[source] |
|---|
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] | ≈90 equipped troops / 20,000 kg (44,092 lb) payload[source] |
|---|
| Propellers | 3-bladed[source] | 4-bladed 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 Myanmar Air Force Pakistan Air Force[source] |
|---|
| Developed from | — | Antonov An-12[source] |
|---|
| Variant | — | Shaanxi KJ-200[source] |
|---|
| Guns | — | 2× 23 mm (0.906 in) cannon in tail turret (early models only)[source] |
|---|
| Airfoil | — | root: C-5-18; tip: C-3-14[source] |
|---|