| 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
|
