Aircraft Performance Data
Engines: | Pratt & Whitney PT6A-34. 750 shp flat rated to 620 shp | |
Propellers: | Hartzell, HC-B3TN, three bladed | |
Maximum Take-off Weight: | 14,000 lb | 6,350 kg |
Typically Equipped Operating Weight*: | 8,264 lb | 3,748 kg |
Useful Load: | 5,736 lb | 2,602 kg |
Standard Fuel Capacity: | 3,110 lb | 1,757 litres |
Extended Fuel Capacity: | 3,586 lb | 2,026 litres |
Maximum Cruise Speed: | 182 TAS | 337 km/h |
Loiter Speed: | 86 IAS | 86 IAS |
STOL Take-off Distance to 50 feet: | 1,200 feet | 366 m |
STOL Landing Distance from 50 feet: | 1,050 feet | 320 m |
Max Endurance Cruise Fuel Burn (10,000 feet): | 328 lb/hour | 185 l/hr |
Loiter Speed Fuel Burn (5,000 feet): | 352 lb/hour | 199 l/hr |
Max Cruise Speed Fuel Burn (10,000 feet): | 652 lb/hour | 368 l/hr |
Endurance and Range Data
Std Fuel | Ext Fuel | |
Endurance Time (hrs): | 8.7 | 10.15 |
Time on Station with 100nm transit: | 6.7 | 8.05 |
Range with Maximum Fuel (nm): | 983 | 1,134 |
Range with Maximum Fuel (km): | 1,821 | 2,100 |
*Features include: one workstation with seat, five single seats, one stretcher rack, extended wing tip tanks, and two S.C.A.R. - Pods.