| Type | CL-215 | CL-415
|
| Crew | 2 |
|
| Capacity | Up to 26 forward facing seats for passenger transport
|
| Length | 19.8 m (65 ft 0 in) | 65 feet (19.80 meters)
|
| Wingspan | 28.6 m (93 ft 10 in) | 93.83 feet (28.60 meters)
|
| Height | 8.92 m (29 ft 3 in) |
|
| Wing area | 100.33 m2 (1,079.9 sq ft) |
|
| Wing Aspect ratio | 8.15 |
|
| Cabin Height | | 6.23 feet (1.90 meters)
|
| Cabin Width | | 7.87 feet (2.40 meters)
|
| Cabin Length | | 30.84 feet (9.40 meters)
|
| Fuselage Diameter | | 8.83 feet (2.69 meters)
|
| Empty weight | 12,160 kg (26,808 lb)
|
| Max takeoff weight | 19,731 kg (43,499 lb) on land, 17,100 kg (37,700 lb) on water | 43,850 pounds (19,890.36 kilograms)
|
| Maximum Payload | | 6,400 pounds (2,903.04 kilograms)
|
| 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
| 1,530 U.S. gallons (5,791 liters)
|
| Fuel Economy | | 0.99 nautical miles/gallon (0.42 kilometers/liter)
|
| Powerplant | 2 × Pratt & Whitney R-2800-83AM 18-cyl air-cooled radial piston engines | Twin Pratt & Whitney Turboprop (PW123AF)
|
| Horsepower | 1,566 kW (2,100 hp) each | 2,380 HP
|
| Propellers | 3-bladed Hamilton Standard Hydromatic constant-speed fully feathering propeller
|
| Performance | |
|
| Cruise speed | 291 km/h (181 mph; 157 kn) at 18,595 kg (40,995 lb) and 3,050 m (10,010 ft)
|
| Maximum Cruise Speed | | 223 miles/hour (185 knots/hour)
|
| Drop Speed | | 121 to 127 miles/hour (105-110 knots/hour)
|
| Stall speed | 123 km/h (76 mph; 66 kn) 25° flap power off at 15,603 kg (34,399 lb)
|
| Range | 2,094 km (1,301 mi; 1,131 nmi) with 1,587 kg (3,499 lb) payload at long-range cruise power
|
| Rate of climb | 5.0833 m/s (1,000.65 ft/min)
|
| Rate of Climb Loaded | | 1,300 feet/minute Normal: 1,800 feet/minute
|
| Service Ceiling | | 14,700 feet (4,480.56 meters)
|
| Flight Time | | 4 hours (including reserve)
|
| Minimum Take-off Distance | | 2,670 feet (813.32 meters)
|
| Minimum Landing Distance | | 2,180 feet (664.46 meters)
|
| Avionics |
Dual VHF and VHF/FM comms,
VOR/ILS receivers
ADF
Marker Beacon Rx
Transponder
| 2 - VHF AM, 1- VHF –FM, AFF
|
| Water Tanks | |
|
| Capacity | | 1,621 U.S. gallons (6,056.66 liters)
|
| Tanking | | 2 Tanks/4 Doors
|
| Runway Surface | | Hard surface runway is the standard requirement with a runway, taxiway, and ramp capable of supporting 36,000 pounds. Gravel runways may only be used with prior approval of the vendor.
|
| Runway Length | | At least 3,500 feet.
|
| Airstrip Pressure Altitude | | CL-415s have a fight manual limitation of operating (takeoff or landing) from an airstrip no higher than 10,000’ Pressure Altitude.
|
| Fuel | | Jet A. Fueling by truck is preferred; however, non-truck fueling is an option on a case-by-case basis.
|
