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C-17 Globemaster III - Wikipedia, the free encyclopedia |
 | | Maximum payload capacity of the C-17 is 170,900 lb (77,500 kg), and its maximum gross takeoff weight is 585,000 lb (265,350 kg). |
 | | The USAF originally intended to acquire about 350 units, though this was reduced at the end of the Cold War. |
 | | Specific requirements are that the aircraft must carry 39,000 kg (85,980 lbs) a distance of 6,482 km (3,500 nm) and operate from runways of 4,000 ft. First delivery must be within 18 months and the last no later than 48 months. |
| en.wikipedia.org /wiki/C-17_Globemaster_III (3181 words) |
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