Credit
Daniel VA · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
AT-802 · Length
Single source35 ft 11 in (10.95 m)[source]
CL-215 · Length
Single sourceConfiguration
| Specification | Air Tractor AT-802 | Canadair CL-215 |
|---|---|---|
| Crew | One or Two (AT-802A – single-seat)[source] | Two[source] |
| Type | Agricultural / Fire-fighting aircraft[source] | — |
| National origin | United States[source] | Canada[source] |
| Manufacturer | Air Tractor[source] | Canadair[source] |
19.82 m (65 ft 0 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]
CL-215 · 2 × Pratt & Whitney R-2800-83AM 18-cylinder air-cooled radial piston engines each
Single source2 × Pratt & Whitney R-2800-83AM 18-cylinder air-cooled radial piston engines, 1,566 kW (2,100 hp) each[source]
AT-802 · Service ceiling
Single source13,000 ft (4,000 m)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Status |
|---|
Active[source] |
In service[source] |
| Manufactured | 1990–present[source] | 1969–1990[source] |
|---|
| First flight | 1990[source] | 23 October 1967[source] |
|---|
| Variant | L3Harris OA-1K Skyraider II[source] | Canadair CL-415[source] |
|---|
| Capacity | 820 US gal (683 imp gal; 3,104 L)[source] | 5,450 L (1200 imp gal; 1,440 US gal) (waterbombing), up to 26 forward facing seats for passenger transport[source] |
|---|
| Aspect ratio | 8.8:1[source] | 8.15[source] |
|---|
| Airfoil | NACA 4415[source] | — |
|---|
| Stall speed | 91 mph (146 km/h, 79 kn) (power off, flaps down)[source] | 123 km/h (76 mph, 66 kn) 25° flap power off at 15,603 kg (34,399 lb)[source] |
|---|
| Role | — | Firefighting amphibious aircraft[source] |
|---|
| Primary users | — | Canada Greece Spain United States[source] |
|---|
| Number built | — | 125[source] |
|---|
| Introduction date | — | 1969[source] |
|---|
| In service | — | 1969–present[source] |
|---|
| Fuel capacity | — | 5,910 L (1,561.3 US gal; 1,300.0 imp gal) in two fuel tanks, of eight cells each, in the wings[source] |
|---|
| Propellers | — | 3-bladed Hamilton Standard Hydromatic constant-speed fully feathering propeller[source] |
|---|
Maximum take-off; CL-215 · on water
Single source