| Power Plant | 4 Allison 501-D22C Turboprop Engines |
| Propellers | 4 Hamilton Standard 54H60-123 Hydromatic |
| Cruise Speed at 25,000 Feet | 290 mph |
| Range with IFR Reserves | 2,000 miles |
| Useable Fuel Weight | 52,500 pounds |
| Maximum Payload | 52,500 pounds |
| Aircraft Empty Weight | 101,500 pounds |
| Maximum Zero Fuel Weight | 154,000 pounds |
| Maximum Landing Weight | 160,000 pounds |
| Maximum Takeoff Weight | 170,000 pounds |
| Height to top of fuselage | 36 feet, 8 inches |
| Height to top of tail | 48 feet, 6 inches |
| Length | 143 feet, 10 inches |
| Wingspan | 156 feet, 3 inches |
| Cargo Pallet | |
| Width | 8 feet, 8 inches |
| Length | 24 feet (single section) |
| Maximum Length | 72 feet (three sections) |
| Floor load limit | 125 pounds/running inch (cargo rail) |
| Cargo Compartment Dimensions | |
| Height above ground level | 11 feet, 0 inches |
| Maximum width (floor level) | 13 feet, 0 inches |
| Maximum width | 25 feet, 1 inch |
| Maximum height | 25 feet, 6 inches |
| Length (Constant section) | 32 feet, 0 inches |
| Length (Overall) | 111 feet, 6 inches |
| Volume (absolute) | 49,750 cubic feet |
| Volume (Useable) | 39,000 cubic feet |