Credit
Daniel VA · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
AT-802 · Length
Single source35 ft 11 in (10.95 m)[source]
An-28 · Length
Single sourceConfiguration
| Specification | Air Tractor AT-802 | Antonov An-28 |
|---|---|---|
| Type | Agricultural / Fire-fighting aircraft[source] | Short-range airliner , utility aircraft[source] |
| National origin | United States[source] | — |
| Manufacturer | Air Tractor[source] | — |
| Status | Active[source] | In service[source] |
| Manufactured | 1990–present[source] |
13.10 m (43 ft 0 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]
An-28 · 2 × Glushenkov TVD-10B turboprop engines (960 shp) each
Single source2 × Glushenkov TVD-10B turboprop engines, 720 kW (960 shp) each[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
1975–1993[source] |
| First flight | 1990[source] | September 1969[source] |
|---|
| Variant | L3Harris OA-1K Skyraider II[source] | PZL M28 Skytruck[source] |
|---|
| Capacity | 820 US gal (683 imp gal; 3,104 L)[source] | 17 passengers or 1,750 kg (3,860 lb)[source] |
|---|
| Aspect ratio | 8.8:1[source] | 12.3[source] |
|---|
| Airfoil | NACA 4415[source] | TsAGI R-II-14 (14% thickness)[source] |
|---|
| Stall speed | 91 mph (146 km/h, 79 kn) (power off, flaps down)[source] | — |
|---|
| Designer | — | Antonov[source] |
|---|
| Built by | — | WSK PZL Mielec[source] |
|---|
| Primary user | — | Aeroflot (former)[source] |
|---|
| Number built | — | 191[source] |
|---|
| Introduction date | — | 1986[source] |
|---|
| Developed from | — | Antonov An-14[source] |
|---|
| Developed into | — | Antonov An-38[source] |
|---|
| Fuel capacity | — | 1,960 L (430 imp gal; 520 US gal)[source] |
|---|
| Propellers | — | 3-bladed AW-24AN, 2.80 m (9 ft 2 in) diameter[source] |
|---|
| Never exceed speed | — | 390 km/h (240 mph, 210 kn)[source] |
|---|
| g limits | — | +3[source] |
|---|
| Take-off run to 10.7 m (35 ft) | — | 410 m (1,350 ft)[source] |
|---|
| Landing run from 15 m (50 ft) | — | 315 m (1,033 ft)[source] |
|---|