| Specifications |
|---|
| Contractor
|
de Havilland Canada
|
|
Crew | 1-2
|
|
Wingspan | 19.8 m
|
|
Length | 15.1 m
|
|
Height | 5.7 m
|
|
Wing area | 39.0 sq. m
|
|
Empty weight | 2654 kg
|
|
Takeoff weight | 4761 kg
|
|
Engines | 2 x Pratt & Whitney of Canada PT6-27, 652 hp each
|
|
Max. speed | 343 km/h
|
|
Cruise speed | 297 km/h
|
|
Speed Range | 65-165 KIAS
|
|
Cruise ceiling | 3050 m
|
|
Ceiling | 25,000 ft. (Oxygen installed)
|
Rate of Climb | 1600 fpm, typical |
|
Range with maximum payload | 200 km
|
|
Endurance - Maximum |
| Altitude | Airspeed | Fuel Burn (lbs/hr) | Endurance (hrs) |
| Sea Level | 120 kts | 480 | 4.2 |
| 5,000' | 120 kts | 460 | 4.3 |
| 10,000' | 120 kts | 440 | 4.4 |
|
|
Endurance - Maximum | >12 Hour Missions with Extended Fuel Tank
|
|
Payload | 20 passengers or 1045 kg of payload
|
|
Payload | 4500 lbs.
|
|
Power Available | >4200 W
|
|
Communications | VHF, UHF, HF, UHF/FM
|
|
Avionics | Tacan, GPS, VHF/UHF Homing
|
| Unit Cost |
$2,000,000
|
| User Countries | Argentina, Canada, Chile, Colombia, Haiti, Kenya, Norway, Pakistan, Panama, Paraguay, People's Republic of China, Senegal, Sudan, Switzerland, USA.
|
