| Specifications |
| Primary Function | Aeromedical evacuation |
| Contractor | McDonnell Douglas Corporation |
| Power Plant | Two Pratt & Whitney JT8D-9A turbofan engines |
| Thrust | 14,500 pounds (6,525 kilograms) each engine |
| Length | 119 feet, 3 inches (35.7 meters) |
| Wingspan | 93 feet, 3 inches (27.9 meters) |
| Height | 27 feet, 5 inches (8.2 meters) |
| Maximum Takeoff Weight | 108,000 pounds (48,600 kilograms) |
| Range | More than 2,000 miles (1,739 nautical miles) |
| Ceiling | 35,000 feet (10,606 meters) |
| Speed | 565 mph (Mach 0.86) at 25,000 feet (7583.3 meters), with maximum takeoff weight |
| Load | 40 litter patients or four litters and 40 ambulatory patients or other combinations |
| Crew | Eight (pilot, co-pilot, flight mechanic, two flight nurses and three aeromedical technicians) |
| Date Deployed | August 1968 |
| Unit Cost | $17 million |
| Inventory | Active force, 10; ANG, 0; Reserve, 0 |