KC-10 Extender
Summary
| Category | Military Transport Aircraft |
| Origin country | 🇺🇸 United States |
| Manufacturer | McDonnell Douglas |
| First flight | 1 July 1980 |
| Year introduced | 1981 |
| Number produced | 60 units |
| Average unit price | $96 million |
Technical specifications
| Version: KC-10A | |
|---|---|
| Crew | 4 (Aircraft Commander, copilot, flight engineer, and boom operator) |
| Operational range | 7,100 km (4,412 mi) |
| Maximum speed | 866 km/h (538 mph) |
| Wing area | 367.7 m² (3957.9 sqft) |
| Wingspan | 50.4 m (165.4 ft) |
| Height | 17.7 m (58.1 ft) |
| Length | 55.4 m (181.6 ft) |
| Service ceiling | 13,000 m (42,651 ft) |
| Empty weight | 109,328 kg (241,027 lbs) |
| Max. takeoff weight | 267,619 kg (589,998 lbs) |
| Climb rate | 34.9 m/s (114.5 ft/s) |
| Powerplant | 3 x General Electric F103 (GE CF6-50C2) delivering 78 kN each |
Current operating countries
All operators
Description
The McDonnell Douglas KC-10 Extender was developed under the Advanced Tanker Cargo Aircraft Program (ATCA) to supplement the Boeing KC-135 Stratotanker. Following the 1973 Yom Kippur War, the United States Air Force (USAF) sought a tanker with greater range and payload capabilities after Operation Nickel Grass demonstrated the limitations of existing assets when denied European landing rights. In December 1977, the USAF selected the McDonnell Douglas DC-10 over the Boeing 747 and Lockheed C-5, citing its performance on shorter runways. The KC-10 first flew in July 1980 and performed its first aerial refueling sortie in October 1980. McDonnell Douglas produced 60 aircraft for the USAF between 1981 and 1988.
Based on the civilian DC-10-30CF, the KC-10 retains 88% commonality with the commercial airframe. Modifications for military service included the removal of most windows and lower cargo doors, the addition of military-specific avionics, and an improved cargo-handling system. The aircraft is powered by three General Electric F103 (CF6-50C2) turbofan engines, each providing 52,500 lbf of thrust. Fuel capacity was increased to 356,000 pounds (161,000 kg) through the installation of additional tanks in the baggage compartments below the main deck.
The refueling system features a digital fly-by-wire centerline boom and a hose-and-drogue system. The boom delivers fuel at a rate of 1,100 gallons per minute, while the drogue system operates at 470 gallons per minute. The boom operator is positioned in a rear cockpit with a wide window for visual monitoring. The final 20 aircraft produced also featured wing-mounted hose-and-drogue pods. In cargo configuration, the KC-10 carries up to 170,000 pounds (77,000 kg) of freight or a combination of 75 personnel and 146,000 pounds (66,000 kg) of cargo.
The USAF operated the KC-10 from 1981 to 2024. During Operation El Dorado Canyon in 1986, the aircraft provided refueling for F-111s striking Libya. In the 1990–91 Gulf War, KC-10s and KC-135s conducted 51,700 refueling operations, delivering 125 million gallons of fuel. Subsequent deployments included Operation Allied Force in 1999, where the KC-10 flew 409 missions, and operations in Afghanistan and Iraq. In 2021, the fleet supported the evacuation of 124,000 people during Operation Allies Refuge. The Royal Netherlands Air Force (RNLAF) operated two converted KDC-10s from 1995 to 2021. Upon retirement, the Dutch aircraft were sold to Omega Aerial Refueling Services. The USAF retired its final KC-10 in September 2024.
Main Variants
- KC-10A: The initial military production tanker and cargo variant based on the DC-10-30CF.
- KDC-10: A conversion of civilian DC-10-30CF aircraft for tanker and transport roles, operated by the RNLAF and Omega Aerial Refueling Services.
- KC-10B: A proposed tanker and transport version of the MD-11CF with increased cargo and fuel capacity offered to international customers.