Specifications |
| Primary Function | Long-range troop and cargo airlift. |
| Contractor | Lockheed-Georgia Co. |
| Power Plant | Four Pratt & Whitney TF33-P-7 turbofan engines. |
| Thrust | 20,250 pounds (9,112.5 kilograms), each engine. |
| Length | 168 feet, 4 inches (51 meters). |
| Height | 39 feet, 3 inches (11.9 meters). |
| Wingspan | 160 feet (48.5 meters). |
| Speed | 500 mph (Mach 0.66). |
| Ceiling | 41,000 feet (12,424 meters). |
| Maximum Takeoff Weight | 323,100 pounds (145,395 kilograms). |
| Range | 2,500 miles (2,174 nautical miles). |
| Unit Cost | $8.1 million (1992 dollars). |
| Crew | Six (pilot, co-pilot, two loadmasters, and two flight engineers). |
| Date Deployed | C-141A: May 1964; C-141B: December 1979. |
| Inventory | Active force, 241; ANG, 16; Reserve, 12. |
