Beechcraft King Air C90A
More info on Beechcraft
| Basics | |
| Price New | $2.0M |
| Year Started | 1984 |
| Year Ended | 1992 |
| Pilots Required | 2 |
| Cabin | |
| Passengers (Typical) | 5 |
| Cabin Volume | 218 cu ft |
| Cabin Volume | 6 cu m |
| Cabin Height | 5 ft |
| Cabin Height | 1 m |
| Cabin Width | 5 ft |
| Cabin Width | 1 m |
| Cabin Length | 12 ft |
| Cabin Length | 4 m |
| Performance | |
| Range* | 830 nm |
| Range* | 1,336 km |
| Maximum Cruise Speed | 250 ktas |
| Maximum Cruise Speed | 463 km/hr |
| Maximum Takeoff Weight | 10,100 lb |
| Maximum Takeoff Weight | 4,581 kg |
| Payload with Maximum Fuel | 587 lb |
| Payload with Maximum Fuel | 266 kg |
| Maximum Altitude | 29,800 ft |
| Maximum Altitude | 9,083 m |
| Balanced Field Length | 5,300 ft |
| Balanced Field Length | 1,615 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.