Viking Air DHC 6-300 Twin Otter
More info on Viking Air
| Basics | |
| Price New | $1.9M |
| Year Started | 1970 |
| Year Ended | 1988 |
| Pilots Required | 2 |
| Cabin | |
| Passengers (Typical) | 10 |
| Cabin Volume | 384 cu ft |
| Cabin Volume | 11 cu m |
| Cabin Height | 5 ft |
| Cabin Height | 1 m |
| Cabin Width | 5 ft |
| Cabin Width | 2 m |
| Cabin Length | 19 ft |
| Cabin Length | 6 m |
| Performance | |
| Range* | 540 nm |
| Range* | 869 km |
| Maximum Cruise Speed | Not Provided |
| Maximum Cruise Speed | Not Provided |
| Maximum Takeoff Weight | 12,500 lb |
| Maximum Takeoff Weight | 5,670 kg |
| Payload with Maximum Fuel | 2,666 lb |
| Payload with Maximum Fuel | 1,209 kg |
| Maximum Altitude | 25,000 ft |
| Maximum Altitude | 7,620 m |
| Balanced Field Length | 2,700 ft |
| Balanced Field Length | 823 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.