McDonnell Douglas KC-10A Extender (DC-10-30CF) Aircraft Data
The United States Air Force/McDonnell Douglas KC-10A advanced tanker/cargo aircraft is a version of the intercontinental-range DC-10 Series 30CF (convertible freighter), modified to provide increased mobility for U.S. forces in contingency operations by: refueling fighters and simultaneously carrying the fighters' support equipment and support people on overseas deployments. Refueling strategic airlifters (such as the USAF C-5 and C-17) during overseas deployments and resupply missions; and augmenting the U.S. airlift capability.
- Country of Origin: United States
- First Flight: July 12, 1980
- Initial Service Date: March 1981
- No. Built: 60
- No. In Service: 59
- No. of Hardpoints: 0
- Crew: 4
Power:
3 × F103/General Electric CF6-50C2 turbofans at 236 kN
Weapons:
None
Dimensions:
Length: | 55.35 m. |
Wing Span: | 50.41 m. |
Wing Area: | 367.71 m² |
Height: | 17.70 m. |
Empty Weight: | 109,328 kg. |
Max. Weight: | 267,620 kg. |
Max. Payload: | 77,111 kg. |
Internal Fuel: | 155,128 kg. |
Performance:
Max. Speed: | 996 kph |
Cruise Speed: | 910 kph |
Service Ceiling: | 12,800 m. |
Normal Range: | 7,080 km |
Max. Range: | 18,507 km |