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]
CL-415 · Length
Single sourceConfiguration
| Specification | Air Tractor AT-802 | Canadair CL-415 |
|---|---|---|
| Type | Agricultural / Fire-fighting aircraft[source] | — |
| National origin | United States[source] | Canada[source] |
| Manufacturer | Air Tractor[source] | Canadair Bombardier Aerospace De Havilland Canada[source] |
| Status | Active[source] | In service[source] |
20.4 m (66 ft 11 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]
CL-415 · 2 × Pratt & Whitney Canada PW123AF turboprop each ISA+20 °C Flat rated
Single source2 × Pratt & Whitney Canada PW123AF turboprop , 1,775 kW (2,380 hp) each ISA+20 °C Flat rated[source]
AT-802 · Service ceiling
Single source13,000 ft (4,000 m)[source]
CL-415 · at 200 nmi (370 km) from base
Single source3 hours at 200 nmi (370 km) from base[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Manufactured |
|---|
1990–present[source] |
CL-415: 1993–2015 DHC-515: 2026–[source] |
| First flight | 1990[source] | 6 December 1993[source] |
|---|
| Variant | L3Harris OA-1K Skyraider II[source] | — |
|---|
| Capacity | 820 US gal (683 imp gal; 3,104 L)[source] | 6,137 L (1,350 imp gal; 1,621 US gal) (waterbombing), up to 18 paratroops, up to 2,903 kg (6,400 lb) of cargo[source] |
|---|
| Aspect ratio | 8.8:1[source] | 8.03[source] |
|---|
| Airfoil | NACA 4415[source] | — |
|---|
| Stall speed | 91 mph (146 km/h, 79 kn) (power off, flaps down)[source] | 126 km/h (78 mph, 68 kn) MLW, Landing Configuration[source] |
|---|
| Role | — | Firefighting aircraft[source] |
|---|
| Primary users | — | Vigili del Fuoco (Italy) Sécurité Civile (France) Hellenic Air Force (Greece) Service Aérien Gouvernemental[source] |
|---|
| Number built | — | 95[source] |
|---|
| Introduction date | — | 1994[source] |
|---|
| Developed from | — | Canadair CL-215[source] |
|---|
| Fuel capacity | — | 4,650 kg (10,250 lb) 5812 L ( 1535 US Gal; 1278 imp Gal)[source] |
|---|
| Cabin volume | — | 35.6 m 3 (1,260 cu ft)[source] |
|---|
| Propellers | — | 4-bladed Hamilton Sundstrand 14SF-19, 3.97 m (13 ft 0 in) diameter Fully reversible, feathering blades[source] |
|---|
| g limits | — | +3.25−1.0 g[source] |
|---|
| Wing loading | — | 212.5 kg/m 2 (43.52 lb/sq ft) Maximum After-scooping[source] |
|---|
| Takeoff (ISA) | — | 783 m (2,569 ft) (land), 814 m (2,671 ft) (water)[source] |
|---|
| Landing (ISA) | — | 674 m (2,211 ft) (land), 665 m (2,182 ft) (water)[source] |
|---|
Maximum take-off; CL-415 · Firefighting, Land
Single source