Viking Air DHC 3 Turbine Otter
More info on Viking Air
| Basics | |
| Price New | N/A |
| Year Started | 1952 |
| Year Ended | 1969 |
| Pilots Required | 1 |
| Cabin | |
| Passengers (Typical) | 10 |
| Cabin Volume | 345 cu ft |
| Cabin Volume | 10 cu m |
| Cabin Height | 5 ft |
| Cabin Height | 1 m |
| Cabin Width | 5 ft |
| Cabin Width | 2 m |
| Cabin Length | 16 ft |
| Cabin Length | 5 m |
| Performance | |
| Range* | 748 nm |
| Range* | 1,204 km |
| Maximum Cruise Speed | 160 ktas |
| Maximum Cruise Speed | 296 km/hr |
| Maximum Takeoff Weight | 8,000 lb |
| Maximum Takeoff Weight | 3,629 kg |
| Payload with Maximum Fuel | 2,562 lb |
| Payload with Maximum Fuel | 1,162 kg |
| Maximum Altitude | Not Provided |
| Maximum Altitude | Not Provided |
| Balanced Field Length | 1,030 ft |
| Balanced Field Length | 314 m |
*Range is the maximum IFR range of the aircraft traveling at Long Range Cruise speed with all passenger seats occupied. Range figures use the NBAA IFR alternate fuel reserve calculation for a 200 nautical mile alternate.