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]
PC-12NG · Length
Single sourceConfiguration
| Specification | Air Tractor AT-802 | Pilatus PC-12 |
|---|---|---|
| Crew | One or Two (AT-802A – single-seat)[source] | 1 or 2[source] |
| Type | Agricultural / Fire-fighting aircraft[source] | Passenger and cargo aircraft[source] |
| National origin | United States[source] | Switzerland[source] |
| Manufacturer | Air Tractor[source] | Pilatus Aircraft |
14.4 m (47 ft 3 in)[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]
PC-12NG · 1 × Pratt & Whitney Canada PT6A-67P turboprop engine 1,200 shp
Single source1 × Pratt & Whitney Canada PT6A-67P turboprop engine, 890 kW (1,200 shp)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Status | Active[source] | In production[source] |
|---|
| Manufactured | 1990–present[source] | 1991–present[source] |
|---|
| First flight | 1990[source] | 31 May 1991[source] |
|---|
| Variant | L3Harris OA-1K Skyraider II[source] | Pilatus U-28 Draco[source] |
|---|
| Capacity | 820 US gal (683 imp gal; 3,104 L)[source] | 6 to 9 passengers seats[source] |
|---|
| Aspect ratio | 8.8:1[source] | — |
|---|
| Airfoil | NACA 4415[source] | root : NASA LS(1)-0417MOD; tip : NASA LS(1)-0313[source] |
|---|
| Stall speed | 91 mph (146 km/h, 79 kn) (power off, flaps down)[source] | 124 km/h (77 mph, 67 kn)[source] |
|---|
| Primary users | — | PlaneSense Royal Flying Doctor Service Tradewind Aviation United States Air Force[source] |
|---|
| Number built | — | 2,000 (as of May 2023 )[source] |
|---|
| Introduction date | — | 1994[source] |
|---|
| Maximum landing weight | — | 4,500 kg (9,921 lb)[source] |
|---|
| Maximum zero fuel weight | — | 4,100 kg (9,039 lb)[source] |
|---|
| Fuel capacity | — | 1,226 kg (2,703 lb) / 1,521 L (402 US gal; 335 imp gal)[source] |
|---|
| Cabin | — | 5.16 metres (16.9 ft) long, 1.47 metres (4.8 ft) high, up to 1.52 metres (5.0 ft) wide[source] |
|---|
| Propellers | — | 4-bladed Hartzell Propeller composite, 2.67 m (8 ft 9 in) diameter composite constant-speed fully-feathering reversible propeller[source] |
|---|
| Take-off distance over 50 ft (15 m) | — | 793 m (2,602 ft)[source] |
|---|
| Landing distance over 50 ft (15 m) | — | 661 m (2,169 ft)[source] |
|---|
| Fuel consumption | — | 250 L/h (66 gal/h; 55 imp gal/h) (915 km (569 mi; 494 nmi) trip, including climb, cruise and descent, 491 km/h (305 mph; 265 kn) average block speed)[source] |
|---|