C-22
| Specifications | |
|---|---|
| Primary Function | Passenger transportation
|
| Builder | Boeing Co. |
| Power Plant | Three JT8D-7 turbofan engines |
| Thrust | 14,000 pounds each engine |
| Length | 133 feet, 2 inches (40.3 meters) |
| Height | 34 feet, (10.3 meters) |
| Wingspan | 108 feet (32.7 meters) |
| Maximum Take-off Weight | 170,000 pounds (76,500 kilograms) |
| Maximum Payload | 20,000 pounds (9,000 kilograms) |
| Maximum Speed | 619 mph (Mach 0.82) |
| Range | 2,000 miles (1,739 nautical miles) |
| Endurance | 5.5 hours |
| Crew | Pilot, co-pilot, flight engineer, flight mechanic, and three or four in-flight passenger specialists |
| Unit Cost | No longer available. |
| Date Deployed | 1963. |
| Inventory | Active force, 0; ANG, 3; Reserve, 0. |
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