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]
Dornier 228NG · Length
Single sourceConfiguration
| Specification | Air Tractor AT-802 | Dornier 228 |
|---|---|---|
| Type | Agricultural / Fire-fighting aircraft[source] | Utility aircraft[source] |
| National origin | United States[source] | — |
| Manufacturer | Air Tractor[source] | Dornier GmbH RUAG General Atomics AeroTec Systems GmbH[source] |
| Status | Active[source] | In service[source] |
16.56 m (54 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]
Dornier 228NG · 2 × Honeywell TPE331-10 turboprop (776 shp) each
Single source2 × Honeywell TPE331-10 turboprop , 579 kW (776 shp) each[source]
AT-802 · 850 ft/min (
Single source850 ft/min (4.3 m/s)[source]
Dornier 228NG · Endurance
Single source10 hours[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Manufactured |
|---|
1990–present[source] |
Dornier: 1982–1997 HAL : 1985–present RUAG: 2010–2020 General Atomics: 2021-Present[source] |
| First flight | 1990[source] | 28 March 1981[source] |
|---|
| Variant | L3Harris OA-1K Skyraider II[source] | — |
|---|
| Capacity | 820 US gal (683 imp gal; 3,104 L)[source] | 19 passengers[source] |
|---|
| Aspect ratio | 8.8:1[source] | — |
|---|
| Airfoil | NACA 4415[source] | Do A-5[source] |
|---|
| Stall speed | 91 mph (146 km/h, 79 kn) (power off, flaps down)[source] | 137 km/h (85 mph, 74 kn)[source] |
|---|
| Built by | — | Hindustan Aeronautics Limited[source] |
|---|
| Primary users | — | Indian Air Force Indian Coast Guard Indian Navy[source] |
|---|
| Number built | — | Dornier: 245 HAL: 125[source] |
|---|
| Introduction date | — | July 1982[source] |
|---|
| Developed from | — | Dornier Do 28[source] |
|---|
| Fuel capacity | — | 1,885 kg (4,156 lb)[source] |
|---|
| Propellers | — | 5-bladed MT-Propeller , 2.5 m (8 ft 2 in) diameter fully- feathering constant-speed propellers[source] |
|---|
| Fuel consumption | — | 0.945 kg/km (3.35 lb/mi) at 413 km/h (257 mph; 223 kn) IAS[source] |
|---|
| Take-off run | — | 792 m (2,600 ft) (MTOW, ISA, SL)[source] |
|---|
| Landing run | — | 451 m (1,480 ft) (MLW, ISA, SL)[source] |
|---|
| Country of origin | — | Germany[source] |
|---|