| Specifications |
| Primary Function | Primary screener in specialized undergraduate pilot training |
| Contractors | Slingsby Aviation Ltd., and Northrop Worldwide Aircraft Services Inc. |
| Power Plant | One Textron Lycoming Ltd. AEIO-540-D4A5 engine |
| Thrust | 260 horsepower |
| Length | 24 feet, 9 inches (7.5 meters) |
| Height | 7 feet, 9 inches (2.3 meters) |
| Wingspan | 34 feet, 9 inches (10.6 meters) |
| Maximum Takeoff Weight | 2,550 pounds (1,159 kilograms) |
| Speed | 155 miles per hour (.21 Mach) |
| Ceiling | 19,000 feet (5,790 meters) |
| Range | 352 miles (305.89 nautical miles) |
| Armament | None |
| Crew | Two (student pilot and instructor pilot) |
| Unit Cost | $295,000 |
| Date Deployed | February 1994 |
| Inventory | Active force, 112; Reserve, 0; ANG, 0 |