C-21A Learjet
| Specifications | |
|---|---|
| Primary Function | Passenger and cargo airlift. |
| Builder | Learjet, Inc. (formerly Gates Learjet) |
| Power Plant | Two Garrett TFE-731-2-2B turbofan engines. |
| Thrust | 3,500 pounds (1,575 kilograms) each engine. |
| Length | 48 feet, 7 inches (14.71 meters). |
| Height | 12 feet, 3 inches (3.71 meters). |
| Maximum Takeoff Weight | 18,300 pounds (8,235 kilograms). |
| Wingspan | 39 feet, 6 inches (11.97 meters) |
| Range | 2,306 miles (2,005 nautical miles). |
| Speed | 530 mph (Mach 0.81, 461 knots, 848 kph) |
| Unit Cost | $2.8 million. |
| Crew | Two (pilot and co-pilot). |
| Date Deployed | April 1984. |
| Inventory | Active forces, 70; ANG, 4; Reserve, 0. |
|
NEWSLETTER
|
| Join the GlobalSecurity.org mailing list |
|
|
|
