Blackhawk King Air C90 XP135A
| Basics | |
| Price New | N/A |
| Year Started | 1971 |
| Year Ended | 2005 |
| 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* | 739 nm |
| Range* | 1,189 km |
| Maximum Cruise Speed | 270 ktas |
| Maximum Cruise Speed | 500 km/hr |
| Maximum Takeoff Weight | 10,100 lb |
| Maximum Takeoff Weight | 4,581 kg |
| Payload with Maximum Fuel | 437 lb |
| Payload with Maximum Fuel | 198 kg |
| Maximum Altitude | 30,000 ft |
| Maximum Altitude | 9,144 m |
| Balanced Field Length | 4,000 ft |
| Balanced Field Length | 1,219 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.