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At a glance
Measured figures
AT-802 · Length
Single source35 ft 11 in (10.95 m)[source]
Y-9 · Length
Single sourceConfiguration
| Specification | Air Tractor AT-802 | Shaanxi Y-9 |
|---|---|---|
| Type | Agricultural / Fire-fighting aircraft[source] | Transport aircraft[source] |
| National origin | United States[source] | China[source] |
| Manufacturer | Air Tractor[source] | Shaanxi Aircraft Company[source] |
| Status | Active[source] | In service, in production |
36.065 m (118 ft 4 in)[source]
AT-802 · Range
Single source800 mi (1,300 km, 700 nmi)[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-9 · 4 × WoJiang WJ-6C turboprop engines (5,100 shp) each
Single source4 × WoJiang WJ-6C turboprop engines, 3,800 kW (5,100 shp) each[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] | 2010–present[source] |
|---|
| First flight | 1990[source] | November 2010[source] |
|---|
| Variant | L3Harris OA-1K Skyraider II[source] | — |
|---|
| Capacity | 820 US gal (683 imp gal; 3,104 L)[source] | 20,000 kg (44,092 lb) cargo / 106 paratroopers / 72 medevac +3 attendants[source] |
|---|
| Aspect ratio | 8.8:1[source] | — |
|---|
| Airfoil | NACA 4415[source] | root: C-5-18 ; tip: C-3-14[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 Namibian Air Force[source] |
|---|
| Number built | — | 150+[source] |
|---|
| Introduction date | — | 2012[source] |
|---|
| Developed from | — | Shaanxi Y-8[source] |
|---|
| Variants | — | Shaanxi KJ-500 Shaanxi Y-9JZ Shaanxi KQ-200[source] |
|---|
| Fuel capacity | — | 23,000 kg (50,706 lb)[source] |
|---|
| Propellers | — | 6-bladed JL-4 composite constant-speed fully-feathering reversible propellers[source] |
|---|
| Maximum operating altitude | — | 8,000 m (26,000 ft)[source] |
|---|
| Power/mass | — | 0.234 kW/kg (0.142 hp/lb)[source] |
|---|