Credit
Daniel VA · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
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At a glance
Measured figures
AT-802 · Length
Single source35 ft 11 in (10.95 m)[source]
Y-7-100 · Length
Single sourceConfiguration
| Specification | Air Tractor AT-802 | Xi'an Y-7 |
|---|---|---|
| Type | Agricultural / Fire-fighting aircraft[source] | Regional airliner / military transport[source] |
| National origin | United States[source] | China[source] |
| Manufacturer | Air Tractor[source] | Xi'an Aircraft Industrial Corporation[source] |
| Status | Active[source] | In military service, in production |
24.218 m (79 ft 5 in)[source]
Cruise; AT-802 · at 8,000 ft (2,440 m)
Single source221 mph (356 km/h, 192 kn) at 8,000 ft (2,440 m)[source]
AT-802 · 1 × Pratt & Whitney PT6A -67AG turboprop , 1,350 shp (
Single source1 × Pratt & Whitney PT6A -67AG turboprop , 1,350 shp (1,010 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]
AT-802 · 850 ft/min (
Single source850 ft/min (4.3 m/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Manufactured | 1990–present[source] | 1977-present[source] |
|---|
| First flight | 1990[source] | 20 February 1984[source] |
|---|
| Variant | L3Harris OA-1K Skyraider II[source] | — |
|---|
| Capacity | 820 US gal (683 imp gal; 3,104 L)[source] | 52 passengers max[source] |
|---|
| Aspect ratio | 8.8:1[source] | 11.69[source] |
|---|
| Airfoil | NACA 4415[source] | root: TsAGI S-5-18; tip: TsAGI S-3-13[source] |
|---|
| Stall speed | 91 mph (146 km/h, 79 kn) (power off, flaps down)[source] | — |
|---|
| Primary users | — | People's Liberation Army Air Force People's Liberation Army Navy Air Force People's Liberation Army Ground Force Aviation[source] |
|---|
| Number built | — | 200+[source] |
|---|
| Developed from | — | Antonov An-24 Antonov An-26[source] |
|---|
| Developed into | — | Xi'an MA60[source] |
|---|
| Max zero-fuel weight | — | 19,655 kg (43,332 lb)[source] |
|---|
| Max landing weight | — | 21,800 kg (48,061 lb)[source] |
|---|
| Propellers | — | 4-bladed constant-speed feathering propellers, 3.9 m (12 ft 10 in) diameter[source] |
|---|
| Take-off run | — | 640 m (2,100 ft) at MTOW[source] |
|---|
| Landing run | — | 645 m (2,116 ft) at MLW[source] |
|---|