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]
Super 748 · Length
Single sourceConfiguration
| Specification | Air Tractor AT-802 | Hawker Siddeley HS 748 |
|---|---|---|
| Type | Agricultural / Fire-fighting aircraft[source] | Airliner[source] |
| National origin | United States[source] | United Kingdom[source] |
| Manufacturer | Air Tractor[source] | Avro Hawker Siddeley Hindustan Aeronautics[source] |
| Status | Active[source] | In limited service with the Indian Air Force |
67 ft 0 in (20.42 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]
Super 748 · 2 × Rolls-Royce RDa.7 Dart Mk 536-2 turboprop engines, 2,280 shp ( ) each equivalent
Single source2 × Rolls-Royce RDa.7 Dart Mk 536-2 turboprop engines, 2,280 shp (1,700 kW) 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] | 1961–1988[source] |
|---|
| First flight | 1990[source] | 24 June 1960[source] |
|---|
| Variant | L3Harris OA-1K Skyraider II[source] | — |
|---|
| Capacity | 820 US gal (683 imp gal; 3,104 L)[source] | 40–58 passengers / 11,323 lb (5,136 kg) payload[source] |
|---|
| Aspect ratio | 8.8:1[source] | 11.967[source] |
|---|
| Airfoil | NACA 4415[source] | root: NACA 23018 ; tip: NACA 4412[source] |
|---|
| Stall speed | 91 mph (146 km/h, 79 kn) (power off, flaps down)[source] | — |
|---|
| Primary users | — | British Airways Air Creebec Dan-Air Air North Varig[source] |
|---|
| Number built | — | 380[source] |
|---|
| Developed into | — | Hawker Siddeley Andover BAe ATP[source] |
|---|
| Fuel capacity | — | 1,440 imp gal (1,730 US gal; 6,500 L) in two wing integral tanks[source] |
|---|
| Propellers | — | 4-bladed Dowty Rotol constant-speed fully-feathering propellers, 12 ft 0 in (3.66 m) diameter[source] |
|---|
| Wing loading | — | 56.1 lb/sq ft (274 kg/m 2 )[source] |
|---|
| Power/mass | — | 0.0981 hp/lb (0.1613 kW/kg)[source] |
|---|
| Take-off distance to 50 ft (15 m) | — | 3,800 ft (1,200 m)[source] |
|---|
| Landing distance from 50 ft (15 m) | — | 2,034 ft (620 m)[source] |
|---|
| Take-off distance | — | 2,624 ft (800 m)[source] |
|---|
| Landing distance | — | 1,968 ft (600 m)[source] |
|---|