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. |